Messages in AirborneWindEnergy group.                          AWES 21701 to 21751 Page 327 of 440.

Group: AirborneWindEnergy Message: 21701 From: dave santos Date: 1/14/2017
Subject: Re: Energy-kite patentee Selsam using potential energy for gliding-k

Group: AirborneWindEnergy Message: 21702 From: Joe Faust Date: 1/14/2017
Subject: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Group: AirborneWindEnergy Message: 21703 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Group: AirborneWindEnergy Message: 21704 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Group: AirborneWindEnergy Message: 21705 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Group: AirborneWindEnergy Message: 21706 From: dave santos Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Group: AirborneWindEnergy Message: 21707 From: dave santos Date: 1/15/2017
Subject: Lattice Waves and Strouhal Number (review)

Group: AirborneWindEnergy Message: 21708 From: dave santos Date: 1/15/2017
Subject: Updating Baptiste Labat's progress in AWE

Group: AirborneWindEnergy Message: 21709 From: joe_f_90032 Date: 1/16/2017
Subject: Re: Lattice Waves and Strouhal Number (review)

Group: AirborneWindEnergy Message: 21710 From: dave santos Date: 1/16/2017
Subject: Dutch team sets record for largest rigid kite ever

Group: AirborneWindEnergy Message: 21711 From: dave santos Date: 1/16/2017
Subject: Giant Kites of the Caribbean; an emergent tradition

Group: AirborneWindEnergy Message: 21712 From: joe_f_90032 Date: 1/16/2017
Subject: Bird Windmill Short Stroke Kite

Group: AirborneWindEnergy Message: 21713 From: dave santos Date: 1/16/2017
Subject: AWE Technological Unemployment, Flight-Automation, and the OSI Model

Group: AirborneWindEnergy Message: 21714 From: dave santos Date: 1/16/2017
Subject: Re: Bird Windmill Short Stroke Kite

Group: AirborneWindEnergy Message: 21715 From: Peter A. Sharp Date: 1/17/2017
Subject: Bird Windmill Short Stroke Kite

Group: AirborneWindEnergy Message: 21716 From: dave santos Date: 1/17/2017
Subject: Re: Bird Windmill Short Stroke Kite

Group: AirborneWindEnergy Message: 21717 From: joe_f_90032 Date: 1/18/2017
Subject: Re: VAWT, HAWT, and AWE compared

Group: AirborneWindEnergy Message: 21718 From: joe_f_90032 Date: 1/18/2017
Subject: Re: Forum headline images

Group: AirborneWindEnergy Message: 21719 From: joe_f_90032 Date: 1/18/2017
Subject: Demir Oral Tethered Airborne Advertising system

Group: AirborneWindEnergy Message: 21720 From: dave santos Date: 1/18/2017
Subject: Re: VAWT, HAWT, and AWE compared

Group: AirborneWindEnergy Message: 21721 From: joe_f_90032 Date: 1/18/2017
Subject: Re: Forum headline images

Group: AirborneWindEnergy Message: 21722 From: joe_f_90032 Date: 1/19/2017
Subject: Kite system used for parachute practice in 1928.

Group: AirborneWindEnergy Message: 21723 From: joe_f_90032 Date: 1/19/2017
Subject: Re: MILLER BERNHARD and his AWES

Group: AirborneWindEnergy Message: 21724 From: joe_f_90032 Date: 1/19/2017
Subject: Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher

Group: AirborneWindEnergy Message: 21725 From: joe_f_90032 Date: 1/19/2017
Subject: SCHEUERMANN BERND

Group: AirborneWindEnergy Message: 21726 From: dave santos Date: 1/19/2017
Subject: Re: Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher

Group: AirborneWindEnergy Message: 21728 From: joe_f_90032 Date: 1/19/2017
Subject: Re: MILLER BERNHARD and his AWES

Group: AirborneWindEnergy Message: 21729 From: dave santos Date: 1/19/2017
Subject: Re: MILLER BERNHARD and his AWES

Group: AirborneWindEnergy Message: 21730 From: joe_f_90032 Date: 1/19/2017
Subject: Estimating the Future

Group: AirborneWindEnergy Message: 21731 From: joe_f_90032 Date: 1/20/2017
Subject: KONSTANTIN HARTMANN

Group: AirborneWindEnergy Message: 21732 From: joe_f_90032 Date: 1/20/2017
Subject: Re: KONSTANTIN HARTMANN

Group: AirborneWindEnergy Message: 21733 From: joe_f_90032 Date: 1/20/2017
Subject: Re: KONSTANTIN HARTMANN

Group: AirborneWindEnergy Message: 21734 From: joe_f_90032 Date: 1/20/2017
Subject: Re: KONSTANTIN HARTMANN

Group: AirborneWindEnergy Message: 21735 From: Peter A. Sharp Date: 1/20/2017
Subject: Re: VAWT, HAWT, and AWE compared

Group: AirborneWindEnergy Message: 21736 From: dave santos Date: 1/20/2017
Subject: Re: VAWT, HAWT, and AWE compared

Group: AirborneWindEnergy Message: 21737 From: dave santos Date: 1/20/2017
Subject: Re: VAWT, HAWT, and AWE compared

Group: AirborneWindEnergy Message: 21738 From: joe_f_90032 Date: 1/20/2017
Subject: Propeller

Group: AirborneWindEnergy Message: 21739 From: joe_f_90032 Date: 1/20/2017
Subject: Nutation

Group: AirborneWindEnergy Message: 21740 From: dave santos Date: 1/20/2017
Subject: Re: Dancing-Arch AWES Concept

Group: AirborneWindEnergy Message: 21741 From: joe_f_90032 Date: 1/20/2017
Subject: Mount turbine on kited tethers?

Group: AirborneWindEnergy Message: 21742 From: joe_f_90032 Date: 1/20/2017
Subject: Re: Mount turbine on kited tethers?

Group: AirborneWindEnergy Message: 21743 From: dave santos Date: 1/20/2017
Subject: Re: Mount turbine on kited tethers?

Group: AirborneWindEnergy Message: 21744 From: dave santos Date: 1/21/2017
Subject: Re: Nutation

Group: AirborneWindEnergy Message: 21745 From: dave santos Date: 1/21/2017
Subject: Kite-Arch Self-launching/landing Video (review)

Group: AirborneWindEnergy Message: 21746 From: Peter A. Sharp Date: 1/22/2017
Subject: Dabiri's COTS VAWTs

Group: AirborneWindEnergy Message: 21747 From: dave santos Date: 1/22/2017
Subject: Re: Dabiri's COTS VAWTs

Group: AirborneWindEnergy Message: 21748 From: dave santos Date: 1/22/2017
Subject: Re: Dabiri's COTS VAWTs

Group: AirborneWindEnergy Message: 21749 From: dave santos Date: 1/22/2017
Subject: "Impossible" demo of sustained vertical flight by a tethered wing

Group: AirborneWindEnergy Message: 21750 From: joe_f_90032 Date: 1/22/2017
Subject: HAWT Kite with Ram Air Drive and Belt Loops

Group: AirborneWindEnergy Message: 21751 From: dave santos Date: 1/23/2017
Subject: Re: HAWT Kite with Ram Air Drive and Belt Loops




Group: AirborneWindEnergy Message: 21701 From: dave santos Date: 1/14/2017
Subject: Re: Energy-kite patentee Selsam using potential energy for gliding-k
Bravo to Doug, for undertaking to master an aviation discipline, which will surely stand him in good stead to continue advancing in AWE practice. The recommendation stands to all AWE developers, to practice some branch of aviation, to learn how to share the sky. Aviation safety culture is an essential part of future AWES operations. Soaring develops a three-dimensional understanding of the upper wind-field. Doug had seemed to falter in his AWE progress, but now he is moving up once again. May he stay safe as he explores the sky to perhaps bring its power down to earth.

High Flight

Oh! I have slipped the surly bonds of Earth
And danced the skies on laughter-silvered wings;
Sunward I've climbed, and joined the tumbling mirth
Of sun-split clouds, — and done a hundred things
You have not dreamed of — wheeled and soared and swung
High in the sunlit silence. Hov'ring there,
I've chased the shouting wind along, and flung
My eager craft through footless halls of air… .
Up, up the long, delirious burning blue
I've topped the wind-swept heights with easy grace
Where never lark, or ever eagle flew — 
And, while with silent, lifting mind I've trod
The high untrespassed sanctity of space,
Put out my hand, and touched the face of God.

— John Gillespie Magee, Jr


On Thursday, January 12, 2017 8:48 AM, "Joe Faust joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
After storing potential energy in his new gliding-kite system
Doug Selsam returns (from decades ago) to gliding-kite system 
exploration ( hang gliding). See his several videos for some
of his flights and those he may be observing: 

It is my guess that his gliding-kite experiences will lead to some heightened
appreciation of FFAWE and other AWE matters. 


Group: AirborneWindEnergy Message: 21702 From: Joe Faust Date: 1/14/2017
Subject: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL
​Some meta notes regarding the Wave Energy Prize (history; done deal; a winner took top prize; second and third prizes were given).  
$1.5 million grand prize
  • ​Seed money was given 
  • Competition occurred.   How did it happen that some of us missed the contest?
  • A first technology gate at 1/50th scale occurred. 
  • Did Poseidon's Kite enter a 1/50th scale model for testing? 
    • How did it do?  
    • Specifications of their 1/50th scale device?  Was it a paravane scheme? Or what?
    • Could kites be involved in sea-wave energy devices in ways that go beyond what Poseidon's Kite team presented?   
    • ​Thomas Bein ​
      Principal Engineer at Maritime Applied Physics Corporation
      ​, 
      Curtis Bay, Maryland
    • ​Some funding awards in Thomas Bein's history: https://sbirsource.com/sbir/people/4191-mr-thomas-bein​       aka Tom Bein  
      [Caution: Discover the distinction between this Thomas Bein and perhaps another in Europe.]



  • What was done by Poseidon's Kite team precisely?
  • See: https://waveenergyprize.org/teams/poseidons-kite    WEC type in the contest by Poseidon's Kite:  "Kinetic Energy Absorbing Kite"

  • Those teams that passed the first gate prepared 1/20th scale devices and competed toward a second technology gate. 
  • Then the top 20 teams surfaced. 
  • Then final competition.   Winner resulted.  

  • The entire contest with substantial prize and method of testing
    might be a model for what could arise one day for AWE.  
    • When will AWE be ready for facing such a contest?
    • How many teams might be expected to enter an AWES prized contest if the prize consisted of $1.5 million USD?  If seeding funds of $125,000 were provided for qualifying teams?  
    • Is DOE up to the deal?  Would some other agent or group of agents be up to the deal? 

  • Start:  https://waveenergyprize.org/​   Study their various pages and envision the contest with an AWES interpretation. 


===============================

POSEIDON’S KITE (EGT1)
​ ​   
An (ETG1) denotes that a Registered Team did not pass Technology Gate 1.

Gambrills, MD

Poseidon’s Kite (ETG1)

Gambrills, MD
Accepted: Wed 01 Jul 2015

=================================================================

It seems like it would be very helpful if Thomas Bein and team gave full presentation of what they entered in approach of the Gate One. 



Group: AirborneWindEnergy Message: 21703 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL
Team Wins $1.5 Million for Wave Energy Device

 



Group: AirborneWindEnergy Message: 21704 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL

Laterally associated with topic
The Pursuit of Wave Energy -- Brian Moffat at Mindshare LA
(notice the chide on Minesto)
The Pursuit of Wave Energy -- Brian Moffat at Mindshare LA

 



Group: AirborneWindEnergy Message: 21705 From: joe_f_90032 Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL
Group: AirborneWindEnergy Message: 21706 From: dave santos Date: 1/14/2017
Subject: Re: Poseidon's Kite AND A POSSIBLE PRIZED-BASED AWE-CONTEST MODEL
Indeed, this wave energy challenge could be a natural prelude for a similar prize by DOE in AWE, however, their record is very poor, having given GoogleX/Makani twice as much via ARPA-E, without any fly-off contest. Its also noted that Cathy Zoi and Fort Felker bolted from DOE into the Makani program, without any revolving-door waiting period. There is also uncertainty over the policies of the Trump administration with regard to energy research, and science generally.

"Poseidon's Kite" and other wave-energy contenders are all kitetoon-like in key respects even if only one team uses the k-word.


On Saturday, January 14, 2017 3:04 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  

Laterally associated with topic
The Pursuit of Wave Energy -- Brian Moffat at Mindshare LA
(notice the chide on Minesto)
The Pursuit of Wave Energy -- Brian Moffat at Mindshare LA
 




Group: AirborneWindEnergy Message: 21707 From: dave santos Date: 1/15/2017
Subject: Lattice Waves and Strouhal Number (review)
Those who have followed the AWES Forum closely over the years are aware of how much we have learned about kite "dancing". Of course gusty wind causes kites to dance in adaptive reaction, but in smooth wind, all kites still dance around their inherent six degrees-of-freedom (DOFs), even if the dancing is hard to see (when the kite seems "pasted to the sky"). Many kites dance strongly, as a design characteristic, and pendulum action is the most common dancing mechanism. Low-complexity open-AWE in particular seeks to amplify and master kite dancing for AWE, for powerful passive pumping without complex control.

The scientific term for inherent kite dancing is harmonic oscillation. A few years ago, the question was posed of whether a giant arch would spontaneously oscillate, and we tried to apply Strouhal Number to predict oscillation [with Baptiste Lebat]. We made the error to take the full arch span as the characteristic Strouhal dimension, and it seemed that oscillation would tend to be weak and slow. This did not explain the Tacoma Narrows Bridge disaster, where strong oscillations famously destroyed the bridge. The correct characteristic dimension was the narrow distance across the arch or bridge, in the direction of flow. This much smaller dimension correctly predicted large energetic oscillations. Stouhal numbers in fact were invented from observing wind causing string to "sing" in wind (aeolian harp effect).

Eiji Ohashi taught us that trains and arches are closely related, and he invented modern kite arches based on trains anchored by both ends. Trains and arches develop one-dimensional lattice waves, and these waves, as energy packets, are phonons, virtual particles classed as bosons, which are collective excitations of the lattice. In the video linked below, which is not too unusual, its easy to see the lattice waves propagating downward, and that the pilot kite on a tether pendant is setting a frequency and amplitude for exciting the waves. Arches that are fully crosswind develop standing waves, and a bit off-axis to the wind they exhibit traveling waves. Classic kitearches and trains are great wave-science demos, but are not optimised for power output. Instead, they use mass and aero dampers to tame the oscillations.

This whole passive lattice-wave approach to AWE is Open-AWE_IP-Cloud, and its lining up nicely as a contender with high-complexity AWE in pending R&D fly-off phases.




Group: AirborneWindEnergy Message: 21708 From: dave santos Date: 1/15/2017
Subject: Updating Baptiste Labat's progress in AWE
Recalling Baptiste in regard to Strouhal Number; it also turns out that he has done a lot of new AWE R&D work in recent years for us to enjoy. Baptiste is one of the best DIY AWE experimenters. Such talented folks accomplish as much or more in AWE than many well-funded academic and venture teams. They represent the bright hope that AWE will ultimately become cheap and simple for popular use, as well as vast industrial scale operations-



Group: AirborneWindEnergy Message: 21709 From: joe_f_90032 Date: 1/16/2017
Subject: Re: Lattice Waves and Strouhal Number (review)
The world's longest kite Weight 500kg


Group: AirborneWindEnergy Message: 21710 From: dave santos Date: 1/16/2017
Subject: Dutch team sets record for largest rigid kite ever
And it wasn't TUDelft :)

About 30m tall, which almost doubles the largest dimension of any sticky kite we have reviewed; remarkable on many counts, including the fact its a cellular box; Bell himself never made made one so large, for all his wealth. The secret to the feat was careful bridling, a quasi 1D overall geometry, and a bit of luck launching...



Coming soon to a browser near you:

"Giant Kites of the Carribean: an emergent tradition"
Group: AirborneWindEnergy Message: 21711 From: dave santos Date: 1/16/2017
Subject: Giant Kites of the Caribbean; an emergent tradition
The traditional small Caribbean three-stick kite in recent years began to grow to monster proportions all across the islands, in part encouraged by an increasing number of online videos, like the examples linked below. One sees a wide range of sophistication in these kites, from basic child versions to extremely refined designs made by specialist masters. 

The finest verions have many subtle features that make them seemingly the most advanced high-wind traditional kite design. We have covered many of these features in old posts, like optional yaw-dampers in the form of streamers around the kites periphery, which look like decoration, but come into their own in high gusty wind.

Given so many documented cases, it can now be said that Caribbean giant kites have attained the status of one of the few bonafide grande kite traditions of the world. Careful study of traditional world-kite videos reveals many operational and design lessons for AWE practice. Surely there are many amazing videos yet to emerge of these genres-











Group: AirborneWindEnergy Message: 21712 From: joe_f_90032 Date: 1/16/2017
Subject: Bird Windmill Short Stroke Kite

Bird Windmill Short Stroke Kite

by Peter A. Sharp 

------------------------------------------up for study and discussion


http://www.energykitesystems.net/SharpKites/BirdWindmillShortStrokeKiteByPeterASharp.jpg


Group: AirborneWindEnergy Message: 21713 From: dave santos Date: 1/16/2017
Subject: AWE Technological Unemployment, Flight-Automation, and the OSI Model
Proposing here that the issue is not that AWE automation will eventually cause "Technological Unemployment" [Wikipedia link below] in early labor-intensive AWE; instead, the issue is that practical AWE automation may only emerge after a very active phase of hands-on evolution has run its course, to develop the operational best-practices sound automation requires. 

To be intensely coding AWE automation prematurely, for sub-optimal "hopeful-monster" prototypes, is to miss a golden age of physical outdoor kite work. A decade ago, KiteLab Portland estimated 25 million kitefarm "dream-jobs" could be created by RAD (Rapid AWE Deployment), for a labor-to-Watt ratio comparable to conventional energy jobs (but with a higher "fun-to-Watt" ratio). Another billion or more folks could use AWE at a personal scale, including kite sports. Utility scale AWE could even be sports-like yachting-in-the-sky, even ordinary child's-play, as a Utopian outcome.

Given our AWES system identification as that of a topological network, under Network Theory, the classic standard OSI Networking Model is hereby invoked. The first layer of AWE automation-architecture logic to encode is a metamaterial Physical Layer, especially the rag-and-string and generator interface. Rigging is the original Stone-Age programming language (literally "hacking"). AWE kite hacking will steal away shut-in coders from their keyboards. That's cool technological unemployment" :)









Group: AirborneWindEnergy Message: 21714 From: dave santos Date: 1/16/2017
Subject: Re: Bird Windmill Short Stroke Kite
Attachments :
    We have a baseline WECS with similar operation; the Prism Flip Kite. KiteLab Ilwaco did many demos with Flip Kites, like grinding coffee and driving small pull-cord chargers. Close observation confirmed that the wing in fact loops closely around a hollow rotation axis, rather than merely spin on its own mid-chord axis. It outputs a sharp short-stroke by carrying its entire mass around the loop. Dynamic soaring's penetration phase depends on sufficient inertial mass, as well as good L/D. 

    KiteLab also found that pilot kites lifting pumping WECS tend to need an elastic buffer section of tether, or their flight is disturbed. The elastic returns the otherwise harmful energy back into the system for harvesting. The pilot kite still does a tiny dance in rhythm with the pumping WECS. Any kite system needs careful tuning of all its major parts to perform its best.

    Inline image



    On Monday, January 16, 2017 12:57 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
    Bird Windmill Short Stroke Kite
    by Peter A. Sharp 
    ------------------------------------------up for study and discussion




      @@attachment@@
    Group: AirborneWindEnergy Message: 21715 From: Peter A. Sharp Date: 1/17/2017
    Subject: Bird Windmill Short Stroke Kite

    Hi DaveS,

    The physics of the Flip Kite is not at all similar to the that of the Bird Windmill Short Stroke Kite in my drawing.

    The Flip Kite and the Koool Kite (closely similar to the Flip Kite) are both closely similar to a kite I built in 1978 that used a Donaldson rotor with a large disc in the middle to increase its stability. Both of those kites vibrate due to blade stall because they are based on the Kramer effect (not the Magnus effect as the Flip Kite makers claim) and have two surfaces (which causes the stall – as opposed to the 3-sided Sharp Rotor which does not stall or vibrate).

    The Bird Windmill works very differently. I can give you a long list of major differences, starting with the fact that the Flip Kite is an entertainment kite, not a power kite. To remind you about how it works, here is a video of a Bird Windmill blade functioning like the blade in my drawing.  https://www.youtube.com/watch?v=UKvRsBgeLQc   [search for “Sharp Cyclo-kite (3)”] I call this a Cyclo-kite for the video. But it is just a Bird Windmill blade (a horizontal orbit) with a vertical orbit. The physics is the same in both cases except for the influence of gravity.

    The Bird Windmill and the Bird Windmill Short Stroke Kite is not like anything that Kite Lab has done. Nothing. Any similarities are quite superficial, such as a vertical, circular motion aligned with the wind. So attempts to understand the Bird Windmill Short Stroke Kite in terms of rotary kites will be highly misleading. They are not analogous in any meaningful way.

    Also note that the blade is already suspended on shock cords, so it is unlikely that an additional shock cord would be required, as you suggest.

    If you ever decide to learn about the Bird Windmill, please keep in mind that I have a long paper on it which I can Email it to you. I recently revised the paper to make it more clear because the physics seems to be difficult for most people to understand.

    PeterS

    http://www.energykitesystems.net/SharpKites/BirdWindmillShortStrokeKiteByPeterASharp.jpg

     

    Group: AirborneWindEnergy Message: 21716 From: dave santos Date: 1/17/2017
    Subject: Re: Bird Windmill Short Stroke Kite
    Hi Peter,

    Are not both turbines crosswind axis, and both backflip the same direction? If so, its not true that these WECS are "not at all similar"; they have the same basic motion and aerodynamics. True, your design has many unsimilar features as well, like two spacer-spars longer than the wing itself, and the added pilot lifter, which impact the overall power to weight negatively (relatively less working wing by mass). Its odd to predict this will be cheaper than less complex designs. 

    "Power kite" is a confusing term as well, if applied to an AWES nothing like standard power kites (LEI, parafoil, and SS). Recall how hard you have tried to communicate your ideas in writing to academia, while your demos speak eloquently for themselves. Your problem has mostly been to apply standard terms in their standard meaning, and power-kite has a very standard meaning (even if all kites are literally "power-kites", that use wind power to fly)

    The shock-cord mounting of the Bird rotor is a particular mystery. The direct effect would be to buffer and isolate the ground PTO, giving weaker smoother pumping strokes. Once again, the ideal comparison would be to build the Bird Windmill AWES at the same weight as the Flip Kite, and fly them off to compare them directly in potential cost and performance, even if you cannot concede any similarities others claim are obvious.

    It would also help us understand you if you distinguish between the science novelty design goal and the practical scalable wind power design goal. You have justified the goal of creating wonderful novelties for personal income without reconciling that with the quest to power the world by upper wind. The two goals are quite a contrast, even if the respective designs have clear similarities. The most-scalable designs can be made to work at small scale, but the least-scalable designs do not work at the largest scales. Its often not clear if you are intentonally restricting yourself to small-scale novelties, as your career so far has gone, or seriously trying to solve the large-scale challenge, as most AWE researchers are,

    daveS




    On Tuesday, January 17, 2017 9:52 AM, "'Peter A. Sharp' sharpencil@sbcglobal.net [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
    Hi DaveS,
    The physics of the Flip Kite is not at all similar to the that of the Bird Windmill Short Stroke Kite in my drawing.
    The Flip Kite and the Koool Kite (closely similar to the Flip Kite) are both closely similar to a kite I built in 1978 that used a Donaldson rotor with a large disc in the middle to increase its stability. Both of those kites vibrate due to blade stall because they are based on the Kramer effect (not the Magnus effect as the Flip Kite makers claim) and have two surfaces (which causes the stall – as opposed to the 3-sided Sharp Rotor which does not stall or vibrate).
    The Bird Windmill works very differently. I can give you a long list of major differences, starting with the fact that the Flip Kite is an entertainment kite, not a power kite. To remind you about how it works, here is a video of a Bird Windmill blade functioning like the blade in my drawing.  https://www.youtube.com/watch?v=UKvRsBgeLQc   [search for “Sharp Cyclo-kite (3)”] I call this a Cyclo-kite for the video. But it is just a Bird Windmill blade (a horizontal orbit) with a vertical orbit. The physics is the same in both cases except for the influence of gravity.
    The Bird Windmill and the Bird Windmill Short Stroke Kite is not like anything that Kite Lab has done. Nothing. Any similarities are quite superficial, such as a vertical, circular motion aligned with the wind. So attempts to understand the Bird Windmill Short Stroke Kite in terms of rotary kites will be highly misleading. They are not analogous in any meaningful way.
    Also note that the blade is already suspended on shock cords, so it is unlikely that an additional shock cord would be required, as you suggest.
    If you ever decide to learn about the Bird Windmill, please keep in mind that I have a long paper on it which I can Email it to you. I recently revised the paper to make it more clear because the physics seems to be difficult for most people to understand.
    PeterS
     


    Group: AirborneWindEnergy Message: 21717 From: joe_f_90032 Date: 1/18/2017
    Subject: Re: VAWT, HAWT, and AWE compared


    Published on Nov 15, 2013

    The Department of Mechanical Engineering's Midwest Mechanics Seminar series welcomes John Dabiri and his presentation, "Bio-Inspired Wind Energy: From Fish Schools and Seagrass to Better Wind Farms."

    Abstract: This talk will describe recent efforts using bio-inspired arrays of counter-rotating vertical-axis wind turbines to reduce the cost, size, and environmental impacts of wind farms. Full-scale field tests of 10-meter tall vertical-axis wind turbines in various counter-rotating configurations have been conducted under natural wind conditions over the past four years. Whereas wind farms consisting of propeller-style, horizontal-axis wind turbines produce 2 to 3 watts of power per square meter of land area, these field tests indicate that power densities an order of magnitude greater can be achieved by arranging vertical-axis wind turbines in layouts inspired by the configurations of schooling fish and seagrass beds. The higher power density is leveraged to achieve meaningful power generation at lower altitudes than required by existing systems. Notably, this improved performance does not require higher individual wind turbine efficiency, only closer wind turbine spacing and a sufficient vertical flux of turbulence kinetic energy from the atmospheric surface layer. The results suggest an alternative approach to wind farming and pose a broad array of interesting, unanswered scientific questions related to the modeling and control of canopy flows.

    ================================================================


    Group: AirborneWindEnergy Message: 21718 From: joe_f_90032 Date: 1/18/2017
    Subject: Re: Forum headline images
     Flygen mounted on kite's tether. This illustration regards a sound generator. 
    Sound device attached to kite string  
    US 4752051 A
    Publication numberUS4752051 A
    Publication typeGrant
    Application numberUS 06/899,301
    Publication dateJun 21, 1988
    Filing dateAug 21, 1986
    Priority dateAug 21, 1986
    Fee statusLapsed
    InventorsWen-Ping Chang
    Original AssigneeChang Wen Ping
    Export CitationBiBTeXEndNoteRefMan
    External Links: USPTOUSPTO AssignmentEspacenet

    Group: AirborneWindEnergy Message: 21719 From: joe_f_90032 Date: 1/18/2017
    Subject: Demir Oral Tethered Airborne Advertising system

    Demir Oral      Tethered Airborne Advertising system


    Group: AirborneWindEnergy Message: 21720 From: dave santos Date: 1/18/2017
    Subject: Re: VAWT, HAWT, and AWE compared
    An interesting VAWT design trend that Dabiri advocates is paired VAWT rotors of complimentary handedness. He seems to have started with trios of VAWTs, but these cannot provide isodirectional optimal orientation. He has set up, on a programmable anchor-grid, fixed pairs that at least address wind optimally, in one orientation. At the same time he is also trying to condense the turbine farm. Its slow tough going to optimize multiple factors at a serious kW scale.

    An interesting analogy from particle physics is to see a single WECS rotor as a fermion, and paired rotors as a boson, with respective qualities. The handedness identical co-directional rotors is the same, but if one twin is flipped, a pair interacts as opposites. Densification is also a BEC property. Many of these physical analogies are mathematically identical, just the scale is very different.


    On Wednesday, January 18, 2017 12:32 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  


    Published on Nov 15, 2013
    The Department of Mechanical Engineering's Midwest Mechanics Seminar series welcomes John Dabiri and his presentation, "Bio-Inspired Wind Energy: From Fish Schools and Seagrass to Better Wind Farms."

    Abstract: This talk will describe recent efforts using bio-inspired arrays of counter-rotating vertical-axis wind turbines to reduce the cost, size, and environmental impacts of wind farms. Full-scale field tests of 10-meter tall vertical-axis wind turbines in various counter-rotating configurations have been conducted under natural wind conditions over the past four years. Whereas wind farms consisting of propeller-style, horizontal-axis wind turbines produce 2 to 3 watts of power per square meter of land area, these field tests indicate that power densities an order of magnitude greater can be achieved by arranging vertical-axis wind turbines in layouts inspired by the configurations of schooling fish and seagrass beds. The higher power density is leveraged to achieve meaningful power generation at lower altitudes than required by existing systems. Notably, this improved performance does not require higher individual wind turbine efficiency, only closer wind turbine spacing and a sufficient vertical flux of turbulence kinetic energy from the atmospheric surface layer. The results suggest an alternative approach to wind farming and pose a broad array of interesting, unanswered scientific questions related to the modeling and control of canopy flows.
    ================================================================



    Group: AirborneWindEnergy Message: 21721 From: joe_f_90032 Date: 1/18/2017
    Subject: Re: Forum headline images

    System and method for umbrella power generation

    which we have seen before at post HERE where discussion of that patent could occur.

    Group: AirborneWindEnergy Message: 21722 From: joe_f_90032 Date: 1/19/2017
    Subject: Kite system used for parachute practice in 1928.

    Cover of Volume XX, Number 25, Aviation, June 21, 1928

    "Kite Balloon Used for Parachute Practice at Lakehurst, N.J."


    Cover photo was while the kite balloon was still closely tethered to the ground. 

    No backstory yet. 




    Group: AirborneWindEnergy Message: 21723 From: joe_f_90032 Date: 1/19/2017
    Subject: Re: MILLER BERNHARD and his AWES
    The English translation of the patent application may contain translation errors. 


    Group: AirborneWindEnergy Message: 21724 From: joe_f_90032 Date: 1/19/2017
    Subject: Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher

    Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher  


    Page bookmarkDE102014105944 (A1)  -  Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher
    Inventor(s):MILLER BERNHARD [DE] +
    Applicant(s):MILLER BERNHARD [DE] +
    Classification:
    - international:F03D9/00F03D9/02
    - cooperative:
    Application number:DE201410105944 20140428 
    Priority number(s):DE201410105944 20140428
    Also published as:


    Group: AirborneWindEnergy Message: 21725 From: joe_f_90032 Date: 1/19/2017
    Subject: SCHEUERMANN BERND

    [Caution: machine translation errors]


    Rope winch power station for energy generation in remote currents e.g. high winds or ocean currents, has current using collectors that are coiled by cable at cable drum similar to stone aged sheet drill  


    Page bookmarkDE102007002989 (A1)  -  Rope winch power station for energy generation in remote currents e.g. high winds or ocean currents, has current using collectors that are coiled by cable at cable drum similar to stone aged sheet drill
    Inventor(s):SCHEUERMANN BERND [DE] +
    Applicant(s):SCHEUERMANN BERND [DE] +
    Classification:
    - international:F03D5/00F03D9/00
    - cooperative:
    Application number:DE20071002989 20070117 
    Priority number(s):DE20071002989 20070117


    Group: AirborneWindEnergy Message: 21726 From: dave santos Date: 1/19/2017
    Subject: Re: Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher
    Bernard Miller has been patenting AWES ideas for a decade, and his 2015 patent depicts airborne iso-lattices of power-kites, which are topologically protected formations. Previous AWE patents did not make the leap to airborne kite networks.

    Fortunately for Open-AWE, this whole conceptual direction has been well explored for almost ten years as public art. For example, fig 5b is identical to fundamental iso-lattice geometries disclosed by KiteLab Group [AWEC2011 and before] with capabilities like circle-towing in calm (reverse-pumping/step-towing variant) is presented in fig 26.

    The implications are as follows. Miller is too late to show priority for fundamental aspects that Open AWE has long documented, but his brilliant patent (if not based on our work!) may still contain novel details of potential utility. Miller provides considerable third-party validation of iso-lattice AWES ideas, which are no longer isolated "fringe" concepts. Hopefully all the players in the iso-lattice concept space can team up. Miller's patent would be a fine addition to kPower's AWE IP Pool (aka Open-AWE_IP-Cloud), and he may welcome working with kPower, which has been exploring these powerful concepts for almost ten years.

    How do we get in contact with Bernard Miller for possible collaboration?


    On Thursday, January 19, 2017 7:21 AM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  

    Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher  


    Page bookmarkDE102014105944 (A1)  -  Vorrichtung zur Stromerzeugung mittels Zugdrachen mit Speicher
    Inventor(s):MILLER BERNHARD [DE] +
    Applicant(s):MILLER BERNHARD [DE] +
    Classification:
    - international:F03D9/00F03D9/02
    - cooperative:
    Application number:DE201410105944 20140428 
    Priority number(s):DE201410105944 20140428
    Also published as:



    Group: AirborneWindEnergy Message: 21728 From: joe_f_90032 Date: 1/19/2017
    Subject: Re: MILLER BERNHARD and his AWES

    [care for "h" in first name: Bernhard]


    Bernhard MILLER


    In the following link under "Documents" tab for at least the document "International Application Status Report"

    there are addresses for him and also for his formal patent agent:  WO/2015/165913 DEVICE FOR CONTROLLING AND STEERING TRACTION KITES OR ROTATING FLYER WHEELS FOR ELECTRICITY GENERATION

     


    Group: AirborneWindEnergy Message: 21729 From: dave santos Date: 1/19/2017
    Subject: Re: MILLER BERNHARD and his AWES
    Thanks Joe,

    A message has been sent to Bernhard's patent agent to explore collaboration possibilities.




    Group: AirborneWindEnergy Message: 21730 From: joe_f_90032 Date: 1/19/2017
    Subject: Estimating the Future

    http://www.openpr.com/news/417428/Airborne-Wind-Turbine-Market-Positive-Long-Term-Growth-Outlook-2024.html

    ===================================

    Significant pay gate for a report is linked above.

    ===================================

    Disclaimer: 

    I have not seen the report. 







    Group: AirborneWindEnergy Message: 21731 From: joe_f_90032 Date: 1/20/2017
    Subject: KONSTANTIN HARTMANN
    Applicants:HARTMANN KONSTANTIN
    Inventors:HARTMANN KONSTANTIN
    Priority Data:4234649 14.10.1992 DE
    Title:(EN) Wind generator - has cable held aloft by hydrogen balloons carrying "wind umbrellas" and towing wagon on ground rails
    (DE) Windkraftzug I


    Clip image: 



    Group: AirborneWindEnergy Message: 21732 From: joe_f_90032 Date: 1/20/2017
    Subject: Re: KONSTANTIN HARTMANN
    Group: AirborneWindEnergy Message: 21733 From: joe_f_90032 Date: 1/20/2017
    Subject: Re: KONSTANTIN HARTMANN

    Clipped image: 




    Group: AirborneWindEnergy Message: 21734 From: joe_f_90032 Date: 1/20/2017
    Subject: Re: KONSTANTIN HARTMANN

    This might help sort some confusion: 

    DE4242065A1 *Dec 14, 1992Oct 7, 1993Konstantin HartmannWind generator - has cable held aloft by hydrogen balloons carrying "wind umbrellas" and towing wagon on ground rails
    DE4300789A1 *Jan 14, 1993Oct 7, 1993Konstantin HartmannWind generator - has cables with wind balloons held aloft by hydrogen cylinders and towing wagon with generators in axles


    Group: AirborneWindEnergy Message: 21735 From: Peter A. Sharp Date: 1/20/2017
    Subject: Re: VAWT, HAWT, and AWE compared

    Hi DaveS,

    You stated:

    " An interesting VAWT design trend that Dabiri advocates is paired VAWT rotors of complimentary handedness. He seems to have started with trios of VAWTs, but these cannot provide isodirectional optimal orientation. He has set up, on a programmable anchor-grid, fixed pairs that at least address wind optimally, in one orientation. At the same time he is also trying to condense the turbine farm. Its slow tough going to optimize multiple factors at a serious kW scale. "

    I agree. So I worked out a simple solution to the directionality problem, and included special advantages that VAWTs have. See  http://www.windpowerengineering.com/featured/business-news-projects/vawts-replace-hawts/ 

    I sent this paper to Dr. Dabiri, but he did not respond. He did respond previously when I sent him my paper on the Bird Windmill. I explained how it could be used to create the kind of wind farm he is researching. He said he would follow my progress. As far as I know, he doesn't understand the Sharp Cycloturbine even though I sent him my long paper on it. Most engineers are biased against passive pitching because previously tested passive-pitch VAWT have been flawed. So they simply refuse to learn about how I fixed those flaws. Whether or not that is also the case for Dr. Dabiri, I don't know. But since he didn't ask me any questions about the Sharp Cycloturbine, my guess is that he rejected it without understanding the problems and how I solved them.

    The basic ideas in my paper could probably be further modified to produce the best wind flows through a wind farm by mounting nearby arrays at different altitudes, and/or by curving each row of VAWTs in some way.

    He does have an economic conflict of interest. He designed and built his own VAWT to use on his wind farms. But, in my opinion, while it may be cheaper than some other VAWT, it’s not nearly as cheap or efficient as the Sharp Cycloturbine promises to be, and it doesn't solve the directionality problem.

    PeterS

    Group: AirborneWindEnergy Message: 21736 From: dave santos Date: 1/20/2017
    Subject: Re: VAWT, HAWT, and AWE compared
    PeterS,

    Dabiri seems to have relied on COTS VAWTs from the start. Recent work in his lab even uses small VAWTs, to speed up research at reduced cost (see link below). I cannot yet find a VAWT his lab has designed, only the hope they might design a better one in the future.

    Its not realistic for Dabiri to be able to validate your claims to have invented a better VAWT. In my aerospace circles, self-trimming designs are fully accepted as aerodynamically superior, and date back to ancient clapper-mills. The problem with self-trimming blades seems to such experts to be simple market economics of mechanical complexity, by capital-cost and reliability; but not at all because university professors active in wind-tech are somehow uniquely ignorant.

    Dabiri's theoretical approach is not to just alternate VAWT handedness in a crosswind array of fixed equal spacing, as your designs on Dvorak's site represent. His spacing pattern is pairs of opposed VAWTs. The best way to convince him you have found a superior ordering is either by clear formal analysis or a well-designed experiment. No one expects he can validate your ideas if he is fully occupied exploring his own ideas. Your best bet is to beat whatever he comes up with, if not formally, then in the wind energy market itself. Like you, Dabiri faces a big challenge just in beating HAWTs, and he risks failing in that foremost. 

    Its small consolation if self-trimming VAWT blades are better, but the VAWT still fails to beat HAWTs, because of its parasitic upwind/downwind cyclic phases. At least VAWTs are accepted as worthy of ongoing research, just in case they can somehow prove to be superior to pure crosswind HAWT cycling.

    daveS







    On Friday, January 20, 2017 11:21 AM, "'Peter A. Sharp' sharpencil@sbcglobal.net [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
    Hi DaveS,
    You stated:
    " An interesting VAWT design trend that Dabiri advocates is paired VAWT rotors of complimentary handedness. He seems to have started with trios of VAWTs, but these cannot provide isodirectional optimal orientation. He has set up, on a programmable anchor-grid, fixed pairs that at least address wind optimally, in one orientation. At the same time he is also trying to condense the turbine farm. Its slow tough going to optimize multiple factors at a serious kW scale. "
    I agree. So I worked out a simple solution to the directionality problem, and included special advantages that VAWTs have. See  http://www.windpowerengineering.com/featured/business-news-projects/vawts-replace-hawts/ 
    I sent this paper to Dr. Dabiri, but he did not respond. He did respond previously when I sent him my paper on the Bird Windmill. I explained how it could be used to create the kind of wind farm he is researching. He said he would follow my progress. As far as I know, he doesn't understand the Sharp Cycloturbine even though I sent him my long paper on it. Most engineers are biased against passive pitching because previously tested passive-pitch VAWT have been flawed. So they simply refuse to learn about how I fixed those flaws. Whether or not that is also the case for Dr. Dabiri, I don't know. But since he didn't ask me any questions about the Sharp Cycloturbine, my guess is that he rejected it without understanding the problems and how I solved them.
    The basic ideas in my paper could probably be further modified to produce the best wind flows through a wind farm by mounting nearby arrays at different altitudes, and/or by curving each row of VAWTs in some way.
    He does have an economic conflict of interest. He designed and built his own VAWT to use on his wind farms. But, in my opinion, while it may be cheaper than some other VAWT, it’s not nearly as cheap or efficient as the Sharp Cycloturbine promises to be, and it doesn't solve the directionality problem.
    PeterS


    Group: AirborneWindEnergy Message: 21737 From: dave santos Date: 1/20/2017
    Subject: Re: VAWT, HAWT, and AWE compared
    To put the AWES turbine comparison problem in its current context, we have a large number of HAWT-principle demos, but nothing on the VAWT side, excepting Magenn and the Portuguese crosswind axis projects. VAWT proponents seem to think a pro-HAWT bias by conventional engineering-science is what prevents the VAWT from gaining acceptance, rather than any possible inherent design deficiency.

    The aerospace prediction is that the highest power-to-mass and maximally KIS WECS will win in an airborne context. KiteLab tested many kite store wind spinners, and found Brasington's Ninja Star turbine to be best. There was hardly any comparable VAWTS to test, for commercial-market reasons unrelated to any academic bias. The "hot air balloon spinner" VAWT exception was very weak, for obvious design shortcomings (see example below).

    If the pro-VAWT community cannot do any better than blame others for the obvious lack of VAWT success, this could be the natural result of a less practical solution. Yes, kites orient to the wind naturally, so the simplest and lightest turbine to fly is a single billet carved into a two-bladed rotor. The Sharp VAWTs tend to look like complex contraptions, but if they can beat the two-bladed rotor (which stops and lies flat in lulls) by power-to-mass, then let someone show such a design.

    If the VAWT community never comes up with a superior AWE solution, due to impractical physics, its not the HAWT community's fault. If mainstream AWE turns out to be based on wings that tack in the crosswind plane, it will be due to superior power-to-mass and practicality over both HAWT and VAWT design limitations. Lets hope VAWT is in the major AWES testing mix, to settle VAWT claims fairly and definitively.









    Group: AirborneWindEnergy Message: 21738 From: joe_f_90032 Date: 1/20/2017
    Subject: Propeller

    The Propeller Explained

    =================================================================


    AWES-involved propeller matters have a home in this topic thread. Such realm embraces AWES turbine or mill  blades driven by wind.

    Group: AirborneWindEnergy Message: 21739 From: joe_f_90032 Date: 1/20/2017
    Subject: Nutation

    Nutation - Wikipedia


    Group: AirborneWindEnergy Message: 21740 From: dave santos Date: 1/20/2017
    Subject: Re: Dancing-Arch AWES Concept
    Preliminary to flying fully-rigged dancing-arches AWES in the next few days, I just tested a small power kite (Prism Stylus 1.8m2 parafoil), in a strong breeze, while holding it near its bridles with leather gloves. As during WSIKF2016, with a staked-out power-kite(5m2 Pansh valved parafoil anchored at its bridle-points), the kite exhibited the same strong spontaneous Dutch-Roll oscillations. I was able to closely modulate the oscillations by varying the span of my arms and "short-line" length, and mimic the action of crosswind cableway motion experiments pending. The trick to controlling wide sweeping of a very short-lined power kite on a cableway may be a pair of pilot tethers run thru pulleys set apart like kitebar ends on the cableway arch line, to passively provide stability and turn input at the intended end-of-travel.

    This bodes well for fully rigged dancing-arch versions to be tested next. This method may be all it takes for parafoil ship kites like SkySails/North-Sails-NZ to pump powerfully at magawatt scale. A reason this method is not obvious is that most kite operations avoid extreme short-line harmonics as a dangerous nuisance. What is normally called "short-line" in power kiting is actually far longer, to avoid higher-frequency harmonics. A wider kite-bar spacing suppresses excess amplitudes, stabilizing the Dutch-Roll orbit. Adding pilot-kite support is a ready dancing-arch option, if needed.

    If you have wind and a small sport parafoil handy, try the hand-held power-kite dancing-arch experiment yourself, as just about the easiest AWES experiment imaginable.


    On Wednesday, January 11, 2017 11:54 AM, dave santos <santos137@yahoo.com
    Group: AirborneWindEnergy Message: 21741 From: joe_f_90032 Date: 1/20/2017
    Subject: Mount turbine on kited tethers?

    Mount the turbine on kited tethers?


    Patent WO2007111517A2 - Fluid power generator 

    Fluid power generator  
    WO 2007111517 A2




    Group: AirborneWindEnergy Message: 21742 From: joe_f_90032 Date: 1/20/2017
    Subject: Re: Mount turbine on kited tethers?


    Publication numberWO2007111517 A2
    Publication typeApplication
    Application numberPCT/NZ2007/000061
    Publication dateOct 4, 2007
    Filing dateMar 23, 2007
    Priority dateMar 24, 2006
    Also published asWO2007111517A3
    InventorsPeter Boyd-WilsonPaul Binner
    ApplicantPacer Turbines Limited
    Export CitationBiBTeXEndNoteRefMan
    External Links: PatentscopeEspacenet



    Group: AirborneWindEnergy Message: 21743 From: dave santos Date: 1/20/2017
    Subject: Re: Mount turbine on kited tethers?
    This concept of a Savonius turbine on a yacht backstay has many disadvantages- excess windage, low efficiency, difficult access, excess rig mass-aloft destabilization. It does not seem any more promising as a kite-based flygen, and mostly duplicates Fry & Hise's prior art.


    On Friday, January 20, 2017 8:39 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  

    Publication numberWO2007111517 A2
    Publication typeApplication
    Application numberPCT/NZ2007/000061
    Publication dateOct 4, 2007
    Filing dateMar 23, 2007
    Priority dateMar 24, 2006
    Also published asWO2007111517A3
    InventorsPeter Boyd-WilsonPaul Binner
    ApplicantPacer Turbines Limited
    Export CitationBiBTeXEndNoteRefMan
    External Links: PatentscopeEspacenet




    Group: AirborneWindEnergy Message: 21744 From: dave santos Date: 1/21/2017
    Subject: Re: Nutation
    Nutation is "wobble". Perturbations of ideal nutation occur by all sorts of extraneous influences, along with chaotic transitions. In AWES, nutation motions are aeroelastic in six degrees-of-freedom (rotational pitch, roll, and yaw interacting with translational heave, surge, and sway).

    Two example cases-

    Place an aircraft model with sensitive position encoding in a wind tunnel. A three-camera set-up of sufficient resolution can track all motions in realtime (videogrammetry). 

    Or just fly a kite and watch it nutate in 6D. A kite's dance is nutation.


    On Friday, January 20, 2017 4:46 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  



    Group: AirborneWindEnergy Message: 21745 From: dave santos Date: 1/21/2017
    Subject: Kite-Arch Self-launching/landing Video (review)
    As active-automation-dependent AWE ventures struggle and fail over the years, its worth keeping in mind that many classic kites self-launch/land. This is a familiar kite arch video to us, but its still our best reference for arch self-launch/land. Note the multiple launch-land cycles, without fuss. High kite density in fluky turbulence is seen tamed by the arch's inherent topological stability, which we increasingly understand in terms of the fundamental mathematical physics. Compare this Open-AWE basis to AWE kitefarm concepts of single kites on single lines dependent on active control theory, which have not shown practical reliability-

    Group: AirborneWindEnergy Message: 21746 From: Peter A. Sharp Date: 1/22/2017
    Subject: Dabiri's COTS VAWTs

    Hi DaveS,

    I didn't say that I expect Dr. Dabiri to “validate” the Sharp Cycloturbine. I want him to understand it because it is well suited to his purposes. Please avoid pejorative paraphrasing.

    I showed you my paper that explains, among other things, that VAWT are inherently more efficient than HAWT. Astonishingly, you then reassert the false claim that VAWT are less efficient than HAWT because the blades move upwind. That's nonsense made up by people who don't understand VAWT. It's an old troll's tale that probably originated when some naïve person noted that drag type VAWT experience drag on the blade moving upwind which reduces efficiency, and then he uncritically assumed that lift-type VAWT are also subject to the same drag. That's false physics. I’ve warned you that there is a lot of false information about VAWT on the Internet, and I’ve given you examples. Please apply your skepticism to your own assumptions, as any researcher should. If you still insist that you are right, then show me your evidence in vector form. You can’t.

    The advancing side of a VAWT produces much more lift and thrust than the retreating side. Yet if your false physics were correct, the opposite would be true.

    Here is a simplified explanation: For a VAWT with a TSR of 3, and ignoring the effect of wind shadow from the upwind blade pass, the average TSR on the advancing side is 3.5, and on the retreating side the average TSR is 2.5. Lift is proportional to the square of the apparent wind speed. So the ratio of the advancing side to the retreating side, in terms of blade lift, is 12.25 to 6.25. In other words, the advancing blades produce almost twice as much lift and thrust. Also, the blades of lift-type VAWT have high lift to drag ratios. So when they are heading directly into the wind, with no angle of attack, they produce only minimal drag. The claim that VAWT are inefficient because the blades move upwind is just negative propaganda kept alive by people who -- if they are not simply ignorant -- wish to denigrate VAWT.

    The Windspire wind turbine used by Dabiri was basically crap and they duly went out of business. My guess is that Dr. Dabiri used what was most convenient to use at the time -- in terms of cost and close spacing. The flaws in the Windspire were that it used a very large cantilever with inadequate strength (some broke their foundations in high winds), it was too close to the ground, and it was a fixed-blade VAWT operating at a TSR which was too low to be efficient, plus the blade chords were too short to be efficient at that TSR. As a result, it spun too slowly for its direct-drive generator, which raised the cost of the generator.

    I saw an image of a wind turbine Dr. Dabiri designed, or had designed, and I think that he used some of them for his test site in Alaska. If I find that reference, I'll send it to you. Here is a reference mentioning new designs from CalTech that they planned to test in Alaska:

     https://www.caltech.edu/news/caltechs-unique-wind-projects-move-forward-39703 

    I just found a video that shows a brief shot of a small VAWT he will be using in Alaska, but I’m not sure if this one was designed at CalTech. This is where I saw the VAWT I referred to:

    https://www.youtube.com/watch?v=FNUSphVmnuE  

    And here is his 2015 updated lecture that includes images of those new VAWT:

    https://www.youtube.com/watch?v=pAGAcGoyP8Q 

    I particularly like this 2012 Dabiri lecture because it make the concepts especially clear:

    https://www.youtube.com/watch?v=Bc4GRaAyE9c&t=54s  

              Whats is “COTS”?  He doesn’t use that acronym. Are you coining an acronym without identifying it?

    A tall, stacked Sharp Cycloturbine could be suspended from an overhead cable. Many of them could be suspended from the same cable. So they could be used just like the Dabiri used the Windspires, but they would be more powerful and produce even less turbulence (because accurate pitch control reduces turbulence). Then Sharp Cycloturbines could be combined into arrays to further increase their efficiency and to further reduce their turbulence. And the arrays can orient to the wind, so new patterns are possible to enhance wind flow across a wind farm. The arrays can be very tall or very wide. If very wide they can be suspended at different elevations to take best advantage of the wind energy flowing above them, as usual, and also below them by means of leaving gaps between the vertical layers of the arrays. Of course, that means more analysis and testing, but it promises to improve on what Dr. Dabiri is currently doing. It could potentially make wind farms using small-scale VAWT much cheaper than wind farms using large-scale HAWT. But Dr. Dabiri has to complete his present project because it is already funded from grants. So even if there is a better idea, he can’t switch to it in mid-stream. That is a flaw inherent in academic grants: if they discover something better along the way, they can’t follow that lead until they complete the project they are working on.

    Your comments seem to assume that if I reveal a new insight in my paper -- that VAWT are inherently more efficient than HAWT if appropriately configured -- it couldn't be true if everybody doesn't already know it. But new ideas are new because people don't already know about them. Lots of people have good ideas that people don’t listen to. It took 25 years of promoting submarines for people to take the concept of a submarine seriously.

    You make a dubious claim that the lowest weight per unit of power predicts the lowest cost of power. That is a good rule of thumb because weight and cost are fairly closely correlated, but it is not a law of physics. There are usually exceptions to rules of thumb. Often, achieving extreme lightness can be very expensive when exotic materials or processes are required . For HAWT, three blades, although heavier than two blades, cost less in the long run because they are more reliable due to better balance when yawing. For VAWT, three blades are better than two blades because, although heavier, three blades smooth out rotor drag pulses that can cause fatigue problems for the rotor as a whole. Consider a car without shock absorbers. It would be lighter. But it would be far less reliable. So it is important to consider new kite ideas in terms of whether they might also be exceptions to the weight-cost rule. Some probably will be. The weight of the ground station must be considered as well, and some will be much heavier than others.

    The KISS rule of thumb when applied to VAWT assumes, uncritically, that any additional moving parts, such as blades that pitch, means that reliability will be reduced and costs will be increased. The people who make that claim are thinking about conventional blade-pitching systems where that rule of thumb does apply in most cases. But if you study VAWT and the Sharp Cycloturbine, you will learn why the Sharp VAWT promises to be cheaper, more reliable, more efficient, and able to capture much more wind energy than is even predicted by its higher efficiency (because it can capture much more energy from wind gusts). The blades of the Sharp VAWT are more durable because they are protected by the shock absorbing effect of using cord bearings and free pitching. Turbulence does not stress the blades nearly as much as for rigidly mounted blades. And V-blades greatly reduce bending stresses. The pitch control should be more accurate than other mechanical systems and it costs almost nothing and has almost nothing to wear out. So the Sharp Cycloturbine is one of the exceptions to that complexity-reliability rule of thumb if one assumes that blade pitching adds complexity.

    But then, if one looks even more closely, in the case of the Sharp Cycloturbine the blade-pitching actually reduces complexity if you consider the various kinds of complexity, such as the machines and processes required to produce it, the complexity of the overspeed control and self-starting devices, the need for more parts and more specialized parts, versatility, ease of shipping, etc. So from that perspective, the Sharp Cycloturbine actually conforms to the complexity-reliability rule of thumb because it is so easy to make using relatively few, common, inexpensive materials and parts.

    PeterS

     

     

     

    Group: AirborneWindEnergy Message: 21747 From: dave santos Date: 1/22/2017
    Subject: Re: Dabiri's COTS VAWTs
    PeterS,

    You have reported struggling to make your case for the Sharp rotor, birdmill, etc, to academia. Its intended to be helpful, not perjorative, to try to identify the problem. Either you are wrongly misunderstood or mistaken about supposed advantages. No one is offended that you claim to be misunderstood, it just keeps VAWT technical questions your raise open, on your behalf.

    Dr. Dabiri and the rest of us in WECS research would be able assess your VAWT claims if you either pose them clearly enough or demo them suitably. For example, make a small-scale working AWES prototype (that is not supported by a pole). As you know, there are hundreds of AWE videos by dozens of parties, and these count far more than written claims on the AWES Forum that are misunderstood.

    The key metric for you to ace is high mass-to-weight, and your build-complexity will be fairly evident. Good baseline comparisons can be with HAWT foam blade designs, like old KiteLab prototypes. Be patient for experimental AWE confirmation, rather than expect your extraordinary claims by themselves to convince anyone. Dabiri himself makes no AWE claims at all, since its just not his field. 

    If AWE is your field, prepare to flyoff against all other contenders.  Lets all let the data decide in due time whose claims stand. You are most welcome, win or lose; and sorry for any offense that misunderstanding you causes,

    daveS




    On Sunday, January 22, 2017 1:14 PM, "'Peter A. Sharp' sharpencil@sbcglobal.net [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
    Hi DaveS,
    I didn't say that I expect Dr. Dabiri to “validate” the Sharp Cycloturbine. I want him to understand it because it is well suited to his purposes. Please avoid pejorative paraphrasing.
    I showed you my paper that explains, among other things, that VAWT are inherently more efficient than HAWT. Astonishingly, you then reassert the false claim that VAWT are less efficient than HAWT because the blades move upwind. That's nonsense made up by people who don't understand VAWT. It's an old troll's tale that probably originated when some naïve person noted that drag type VAWT experience drag on the blade moving upwind which reduces efficiency, and then he uncritically assumed that lift-type VAWT are also subject to the same drag. That's false physics. I’ve warned you that there is a lot of false information about VAWT on the Internet, and I’ve given you examples. Please apply your skepticism to your own assumptions, as any researcher should. If you still insist that you are right, then show me your evidence in vector form. You can’t.
    The advancing side of a VAWT produces much more lift and thrust than the retreating side. Yet if your false physics were correct, the opposite would be true.
    Here is a simplified explanation: For a VAWT with a TSR of 3, and ignoring the effect of wind shadow from the upwind blade pass, the average TSR on the advancing side is 3.5, and on the retreating side the average TSR is 2.5. Lift is proportional to the square of the apparent wind speed. So the ratio of the advancing side to the retreating side, in terms of blade lift, is 12.25 to 6.25. In other words, the advancing blades produce almost twice as much lift and thrust. Also, the blades of lift-type VAWT have high lift to drag ratios. So when they are heading directly into the wind, with no angle of attack, they produce only minimal drag. The claim that VAWT are inefficient because the blades move upwind is just negative propaganda kept alive by people who -- if they are not simply ignorant -- wish to denigrate VAWT.
    The Windspire wind turbine used by Dabiri was basically crap and they duly went out of business. My guess is that Dr. Dabiri used what was most convenient to use at the time -- in terms of cost and close spacing. The flaws in the Windspire were that it used a very large cantilever with inadequate strength (some broke their foundations in high winds), it was too close to the ground, and it was a fixed-blade VAWT operating at a TSR which was too low to be efficient, plus the blade chords were too short to be efficient at that TSR. As a result, it spun too slowly for its direct-drive generator, which raised the cost of the generator.
    I saw an image of a wind turbine Dr. Dabiri designed, or had designed, and I think that he used some of them for his test site in Alaska. If I find that reference, I'll send it to you. Here is a reference mentioning new designs from CalTech that they planned to test in Alaska:
    I just found a video that shows a brief shot of a small VAWT he will be using in Alaska, but I’m not sure if this one was designed at CalTech. This is where I saw the VAWT I referred to:
    And here is his 2015 updated lecture that includes images of those new VAWT:
    I particularly like this 2012 Dabiri lecture because it make the concepts especially clear:
              Whats is “COTS”?  He doesn’t use that acronym. Are you coining an acronym without identifying it?
    A tall, stacked Sharp Cycloturbine could be suspended from an overhead cable. Many of them could be suspended from the same cable. So they could be used just like the Dabiri used the Windspires, but they would be more powerful and produce even less turbulence (because accurate pitch control reduces turbulence). Then Sharp Cycloturbines could be combined into arrays to further increase their efficiency and to further reduce their turbulence. And the arrays can orient to the wind, so new patterns are possible to enhance wind flow across a wind farm. The arrays can be very tall or very wide. If very wide they can be suspended at different elevations to take best advantage of the wind energy flowing above them, as usual, and also below them by means of leaving gaps between the vertical layers of the arrays. Of course, that means more analysis and testing, but it promises to improve on what Dr. Dabiri is currently doing. It could potentially make wind farms using small-scale VAWT much cheaper than wind farms using large-scale HAWT. But Dr. Dabiri has to complete his present project because it is already funded from grants. So even if there is a better idea, he can’t switch to it in mid-stream. That is a flaw inherent in academic grants: if they discover something better along the way, they can’t follow that lead until they complete the project they are working on.
    Your comments seem to assume that if I reveal a new insight in my paper -- that VAWT are inherently more efficient than HAWT if appropriately configured -- it couldn't be true if everybody doesn't already know it. But new ideas are new because people don't already know about them. Lots of people have good ideas that people don’t listen to. It took 25 years of promoting submarines for people to take the concept of a submarine seriously.
    You make a dubious claim that the lowest weight per unit of power predicts the lowest cost of power. That is a good rule of thumb because weight and cost are fairly closely correlated, but it is not a law of physics. There are usually exceptions to rules of thumb. Often, achieving extreme lightness can be very expensive when exotic materials or processes are required . For HAWT, three blades, although heavier than two blades, cost less in the long run because they are more reliable due to better balance when yawing. For VAWT, three blades are better than two blades because, although heavier, three blades smooth out rotor drag pulses that can cause fatigue problems for the rotor as a whole. Consider a car without shock absorbers. It would be lighter. But it would be far less reliable. So it is important to consider new kite ideas in terms of whether they might also be exceptions to the weight-cost rule. Some probably will be. The weight of the ground station must be considered as well, and some will be much heavier than others.
    The KISS rule of thumb when applied to VAWT assumes, uncritically, that any additional moving parts, such as blades that pitch, means that reliability will be reduced and costs will be increased. The people who make that claim are thinking about conventional blade-pitching systems where that rule of thumb does apply in most cases. But if you study VAWT and the Sharp Cycloturbine, you will learn why the Sharp VAWT promises to be cheaper, more reliable, more efficient, and able to capture much more wind energy than is even predicted by its higher efficiency (because it can capture much more energy from wind gusts). The blades of the Sharp VAWT are more durable because they are protected by the shock absorbing effect of using cord bearings and free pitching. Turbulence does not stress the blades nearly as much as for rigidly mounted blades. And V-blades greatly reduce bending stresses. The pitch control should be more accurate than other mechanical systems and it costs almost nothing and has almost nothing to wear out. So the Sharp Cycloturbine is one of the exceptions to that complexity-reliability rule of thumb if one assumes that blade pitching adds complexity.
    But then, if one looks even more closely, in the case of the Sharp Cycloturbine the blade-pitching actually reduces complexity if you consider the various kinds of complexity, such as the machines and processes required to produce it, the complexity of the overspeed control and self-starting devices, the need for more parts and more specialized parts, versatility, ease of shipping, etc. So from that perspective, the Sharp Cycloturbine actually conforms to the complexity-reliability rule of thumb because it is so easy to make using relatively few, common, inexpensive materials and parts.
    PeterS
     
     
     


    Group: AirborneWindEnergy Message: 21748 From: dave santos Date: 1/22/2017
    Subject: Re: Dabiri's COTS VAWTs
    Correction-

    High POWER-to-weight was intended as a "key metric" for an AWES (not "mass-to-weight")

    Sorry for the careless error.


    On Sunday, January 22, 2017 4:20 PM, dave santos <santos137@yahoo.com  
    Hi DaveS,
    I didn't say that I expect Dr. Dabiri to “validate” the Sharp Cycloturbine. I want him to understand it because it is well suited to his purposes. Please avoid pejorative paraphrasing.
    I showed you my paper that explains, among other things, that VAWT are inherently more efficient than HAWT. Astonishingly, you then reassert the false claim that VAWT are less efficient than HAWT because the blades move upwind. That's nonsense made up by people who don't understand VAWT. It's an old troll's tale that probably originated when some naïve person noted that drag type VAWT experience drag on the blade moving upwind which reduces efficiency, and then he uncritically assumed that lift-type VAWT are also subject to the same drag. That's false physics. I’ve warned you that there is a lot of false information about VAWT on the Internet, and I’ve given you examples. Please apply your skepticism to your own assumptions, as any researcher should. If you still insist that you are right, then show me your evidence in vector form. You can’t.
    The advancing side of a VAWT produces much more lift and thrust than the retreating side. Yet if your false physics were correct, the opposite would be true.
    Here is a simplified explanation: For a VAWT with a TSR of 3, and ignoring the effect of wind shadow from the upwind blade pass, the average TSR on the advancing side is 3.5, and on the retreating side the average TSR is 2.5. Lift is proportional to the square of the apparent wind speed. So the ratio of the advancing side to the retreating side, in terms of blade lift, is 12.25 to 6.25. In other words, the advancing blades produce almost twice as much lift and thrust. Also, the blades of lift-type VAWT have high lift to drag ratios. So when they are heading directly into the wind, with no angle of attack, they produce only minimal drag. The claim that VAWT are inefficient because the blades move upwind is just negative propaganda kept alive by people who -- if they are not simply ignorant -- wish to denigrate VAWT.
    The Windspire wind turbine used by Dabiri was basically crap and they duly went out of business. My guess is that Dr. Dabiri used what was most convenient to use at the time -- in terms of cost and close spacing. The flaws in the Windspire were that it used a very large cantilever with inadequate strength (some broke their foundations in high winds), it was too close to the ground, and it was a fixed-blade VAWT operating at a TSR which was too low to be efficient, plus the blade chords were too short to be efficient at that TSR. As a result, it spun too slowly for its direct-drive generator, which raised the cost of the generator.
    I saw an image of a wind turbine Dr. Dabiri designed, or had designed, and I think that he used some of them for his test site in Alaska. If I find that reference, I'll send it to you. Here is a reference mentioning new designs from CalTech that they planned to test in Alaska:
    I just found a video that shows a brief shot of a small VAWT he will be using in Alaska, but I’m not sure if this one was designed at CalTech. This is where I saw the VAWT I referred to:
    And here is his 2015 updated lecture that includes images of those new VAWT:
    I particularly like this 2012 Dabiri lecture because it make the concepts especially clear:
              Whats is “COTS”?  He doesn’t use that acronym. Are you coining an acronym without identifying it?
    A tall, stacked Sharp Cycloturbine could be suspended from an overhead cable. Many of them could be suspended from the same cable. So they could be used just like the Dabiri used the Windspires, but they would be more powerful and produce even less turbulence (because accurate pitch control reduces turbulence). Then Sharp Cycloturbines could be combined into arrays to further increase their efficiency and to further reduce their turbulence. And the arrays can orient to the wind, so new patterns are possible to enhance wind flow across a wind farm. The arrays can be very tall or very wide. If very wide they can be suspended at different elevations to take best advantage of the wind energy flowing above them, as usual, and also below them by means of leaving gaps between the vertical layers of the arrays. Of course, that means more analysis and testing, but it promises to improve on what Dr. Dabiri is currently doing. It could potentially make wind farms using small-scale VAWT much cheaper than wind farms using large-scale HAWT. But Dr. Dabiri has to complete his present project because it is already funded from grants. So even if there is a better idea, he can’t switch to it in mid-stream. That is a flaw inherent in academic grants: if they discover something better along the way, they can’t follow that lead until they complete the project they are working on.
    Your comments seem to assume that if I reveal a new insight in my paper -- that VAWT are inherently more efficient than HAWT if appropriately configured -- it couldn't be true if everybody doesn't already know it. But new ideas are new because people don't already know about them. Lots of people have good ideas that people don’t listen to. It took 25 years of promoting submarines for people to take the concept of a submarine seriously.
    You make a dubious claim that the lowest weight per unit of power predicts the lowest cost of power. That is a good rule of thumb because weight and cost are fairly closely correlated, but it is not a law of physics. There are usually exceptions to rules of thumb. Often, achieving extreme lightness can be very expensive when exotic materials or processes are required . For HAWT, three blades, although heavier than two blades, cost less in the long run because they are more reliable due to better balance when yawing. For VAWT, three blades are better than two blades because, although heavier, three blades smooth out rotor drag pulses that can cause fatigue problems for the rotor as a whole. Consider a car without shock absorbers. It would be lighter. But it would be far less reliable. So it is important to consider new kite ideas in terms of whether they might also be exceptions to the weight-cost rule. Some probably will be. The weight of the ground station must be considered as well, and some will be much heavier than others.
    The KISS rule of thumb when applied to VAWT assumes, uncritically, that any additional moving parts, such as blades that pitch, means that reliability will be reduced and costs will be increased. The people who make that claim are thinking about conventional blade-pitching systems where that rule of thumb does apply in most cases. But if you study VAWT and the Sharp Cycloturbine, you will learn why the Sharp VAWT promises to be cheaper, more reliable, more efficient, and able to capture much more wind energy than is even predicted by its higher efficiency (because it can capture much more energy from wind gusts). The blades of the Sharp VAWT are more durable because they are protected by the shock absorbing effect of using cord bearings and free pitching. Turbulence does not stress the blades nearly as much as for rigidly mounted blades. And V-blades greatly reduce bending stresses. The pitch control should be more accurate than other mechanical systems and it costs almost nothing and has almost nothing to wear out. So the Sharp Cycloturbine is one of the exceptions to that complexity-reliability rule of thumb if one assumes that blade pitching adds complexity.
    But then, if one looks even more closely, in the case of the Sharp Cycloturbine the blade-pitching actually reduces complexity if you consider the various kinds of complexity, such as the machines and processes required to produce it, the complexity of the overspeed control and self-starting devices, the need for more parts and more specialized parts, versatility, ease of shipping, etc. So from that perspective, the Sharp Cycloturbine actually conforms to the complexity-reliability rule of thumb because it is so easy to make using relatively few, common, inexpensive materials and parts.
    PeterS
     
     
     




    Group: AirborneWindEnergy Message: 21749 From: dave santos Date: 1/22/2017
    Subject: "Impossible" demo of sustained vertical flight by a tethered wing
    At the Windless Kite Festival today, Eeideken Award winner and former AKA President, John Barresi demoed a new kite trick he calls the Tornado, where he sustained an indoor Rev kite spinning directly above him. There had been a longstanding question of whether such a trick was even possible.

    The Rev is tugged up by hand and set by the kite-handles with helical-pitch, and the flyer twirls in place about 4m underneath, with leading arm outstretched. Its like a single link of torque-ladder driving a single-bladed rotor. This is only known to work with the indoor Rev, which just needs a bit of torque to sustain itself like a helicopter.

    Video was taken, and should be viewable online soon.
    Group: AirborneWindEnergy Message: 21750 From: joe_f_90032 Date: 1/22/2017
    Subject: HAWT Kite with Ram Air Drive and Belt Loops

    HAWT Kite with Ram Air Drive and Belt Loops

    Hi JoeF,

    Please post the attached drawing for me. Much thanks.

    This sketch is just a first approximation. This design is potentially cheaper than any other design, so far, in terms of the cost of the energy. The final design would keep the central shaft close to horizontal. The proportions would probably be modified from what I show here, but the basic configuration would be the same. Note that if a ram air turbine is pushed through air at 6 times the wind speed, it can produce as much power as 216 turbines of the same size but facing only the true wind. So this design is far simpler and cheaper than using stacked rotors on a torque-transmitting tether. The ram air rotors also spin 5 to 6 times as fast as stacked rotors, which is much better suited to direct drive generators. Ram air turbines imply that stacked, horizontal-axis rotors would be uncompetitive for commercial applications.

    The blade’s pitch axis is just a little ahead of the blade’s center of lift, so that will cause the blade to try to face into its apparent wind. But the T-Rule centrifugal force tries to keep the blade facing in the direction of its path. The two forces appose each other and reach a balance, which is the pitch angle of the blade. The pitch angle determines the angle of attack.

    In the final version of the kite, the belt loops from the ram air rotors would probably run down the inside of each blade’s main tube (which is coincident with the pitching axis of the blade).

    Small floats could be added to enable the kite, and it’s pilot kite, to launch from the surface of a body of water, thus eliminating the need for a launch and retrieval tower, which would otherwise be a major expense. An actual blade might be made in sections with each section controlling its own pitch angle, which would be the equivalent of blade twist.

    The diameter of the large rotor could be further increased withoug adding much weight. Merely move the original blade radially outward. That makes the inward end of the original blade more efficient because it would move at a higher tip speed ratio (since it would be out at a larger percentage of the large rotor’s radius). The shafts supporting the blades can be streamlined.

    With the large blades fully feathered, the large rotor would have very low drag in high wind speeds, yet the ram air rotors would continue to operate since they would be facing the true wind. Hurricane wind speeds would be in about the same range as their normal apparent wind speed.

    The pilot kite would need to have enough rigidity to allow it to fly in hurricane wind speeds. If it did, then the kite system would not need to be retracted and stowed prior to hurricanes.

    An alternative: The parts of the HAWT Kite could be submerged in sea water without damage, and the large blades would simply pitch in response to crashing waves, so the HAWT Kite and a soft pilot kite could rest on the sea surface during storms. The soft kite could be made so that would descend to the sea surface when the wind speed became too high. These solutions could eliminate the need for a tower for launch and retrieval, and eliminate most of those complications and costs. If that proved possible, it would greatly lower the cost of AWES, at least at sea.

    The goal here is to do what the Makani kite can do, but do it for a small fraction of the cost – by greatly simplifying. Any electronics or electrical components, if needed, are kept at ground level, or near sea level. This kite requires no computerized controls once it is launched. There are no electrical cords to the kite, which eliminates that cost and source of wear. The tether does not need to move at high speed across the wind as must the Makani tether, so that reduction of drag should increase the efficiency. The kite will be much lighter and far simpler than the Makani. Yet the ram air rotors will move through the air just as fast and could capture just as much wind energy. Energy from the kite can be transmitted to the ground very cheaply by using a high speed loop belt. No transmission is required for the ground generator, yet the generator can be quite small and operate at a very high rpm, so it will be relatively low-cost. And only one generic generator will be required, not the many specialized generators required by the Makani kite. The gear ratio can be chosen to best match the ground mounted generator.

    Pitch control: The T-Rule states that if a T-shaped object is spun in a circle using a string or rod tied to the bottom of the T, with the central bar of the T lying on a radius of the circle, the top bar of the T will try to lie flat in the plane of rotation due to centrifugal force acting on it, thus creating a centrifugal spring which can be used for blade pitch control. In this case, that means that the blades will try to lie flat in their plane of rotation when revolving.

    In this case, the blade and the ram air rotor shaft create a T shape. Additional weight can be added to the ends of the ram air rotor shafts to increase their resistance to pitching, and/or their length can be increased to increase their moment arm length. That creates a spring that can balance the aerodynamic lift on the blade which tries to make the blade face into its apparent wind. The two forces reach a balance, which is the pitch angle of the blade. The pitch of the blade determines the angle of attack of the blade. So T-Rule pitching can keep the blades from stalling once they are properly balanced. Centrifugal force and aerodynamic lift rise and fall at the same general rate: by the square of the blade speed. So a centrifugal spring can be used to balance aerodynamic lift at all tip speed ratios. I demonstrated T-Rule pitch control of a single blade on a string back in about 1978. I did a recent test with a small model in front of a fan to verify the concept. It works.

    PeterS

    http://www.energykitesystems.net/SharpKites/HAWTKiteWithRamAirDrive.jpg



    Group: AirborneWindEnergy Message: 21751 From: dave santos Date: 1/23/2017
    Subject: Re: HAWT Kite with Ram Air Drive and Belt Loops
    Its problematic to propose any AWES design to "do what the Makani kite can do", without specifying which model (M600 seems grounded by scaling over-reach). 

    A more helpful description of PeterS's design is that its a "turbine on a wing" (like Makani, but [Loyd] is the best reference) driving a "groundgen" by a torque-tube. The torque-tube transmission is challenged by a lack real-world similarity cases. The only identified industrial torque tubes of considerable power and length are oil-well drilling tubes, which are massive thick-wall steel tubes supported from kinking damage by the well shaft.

    Its also problematic to apply either HAWT or VAWT to a diagonal axial-shaft design. To the degree that an axis reaches upper wind, its vertical, and to the degree it fails to reach high, its horizontal.

    Once again, PeterS is not clearly defining the practical scale of his AWES concept (toy-scale? Wing7 scale? M600 scale?). It does not seem designed with scaling laws in mind, if M600 scale is intended, which would require a torque tube almost 2000ft long. Even Wing7 scale would require a torque tube hundreds-of-feet long. There are no COTS tubes known that could be flown practically, with resistance to damage, low-mass, low-cost, etc.

    At least Wing7 exists to compare to an equivalent torque-tube AWES concept, if the required tube can be shown to exist.


    On Sunday, January 22, 2017 8:11 PM, "joefaust333@gmail.com [AirborneWindEnergy]" <AirborneWindEnergy@yahoogroups.com  
    HAWT Kite with Ram Air Drive and Belt Loops
    Hi JoeF,
    Please post the attached drawing for me. Much thanks.
    This sketch is just a first approximation. This design is potentially cheaper than any other design, so far, in terms of the cost of the energy. The final design would keep the central shaft close to horizontal. The proportions would probably be modified from what I show here, but the basic configuration would be the same. Note that if a ram air turbine is pushed through air at 6 times the wind speed, it can produce as much power as 216 turbines of the same size but facing only the true wind. So this design is far simpler and cheaper than using stacked rotors on a torque-transmitting tether. The ram air rotors also spin 5 to 6 times as fast as stacked rotors, which is much better suited to direct drive generators. Ram air turbines imply that stacked, horizontal-axis rotors would be uncompetitive for commercial applications.
    The blade’s pitch axis is just a little ahead of the blade’s center of lift, so that will cause the blade to try to face into its apparent wind. But the T-Rule centrifugal force tries to keep the blade facing in the direction of its path. The two forces appose each other and reach a balance, which is the pitch angle of the blade. The pitch angle determines the angle of attack.
    In the final version of the kite, the belt loops from the ram air rotors would probably run down the inside of each blade’s main tube (which is coincident with the pitching axis of the blade).
    Small floats could be added to enable the kite, and it’s pilot kite, to launch from the surface of a body of water, thus eliminating the need for a launch and retrieval tower, which would otherwise be a major expense. An actual blade might be made in sections with each section controlling its own pitch angle, which would be the equivalent of blade twist.
    The diameter of the large rotor could be further increased withoug adding much weight. Merely move the original blade radially outward. That makes the inward end of the original blade more efficient because it would move at a higher tip speed ratio (since it would be out at a larger percentage of the large rotor’s radius). The shafts supporting the blades can be streamlined.
    With the large blades fully feathered, the large rotor would have very low drag in high wind speeds, yet the ram air rotors would continue to operate since they would be facing the true wind. Hurricane wind speeds would be in about the same range as their normal apparent wind speed.
    The pilot kite would need to have enough rigidity to allow it to fly in hurricane wind speeds. If it did, then the kite system would not need to be retracted and stowed prior to hurricanes.
    An alternative: The parts of the HAWT Kite could be submerged in sea water without damage, and the large blades would simply pitch in response to crashing waves, so the HAWT Kite and a soft pilot kite could rest on the sea surface during storms. The soft kite could be made so that would descend to the sea surface when the wind speed became too high. These solutions could eliminate the need for a tower for launch and retrieval, and eliminate most of those complications and costs. If that proved possible, it would greatly lower the cost of AWES, at least at sea.
    The goal here is to do what the Makani kite can do, but do it for a small fraction of the cost – by greatly simplifying. Any electronics or electrical components, if needed, are kept at ground level, or near sea level. This kite requires no computerized controls once it is launched. There are no electrical cords to the kite, which eliminates that cost and source of wear. The tether does not need to move at high speed across the wind as must the Makani tether, so that reduction of drag should increase the efficiency. The kite will be much lighter and far simpler than the Makani. Yet the ram air rotors will move through the air just as fast and could capture just as much wind energy. Energy from the kite can be transmitted to the ground very cheaply by using a high speed loop belt. No transmission is required for the ground generator, yet the generator can be quite small and operate at a very high rpm, so it will be relatively low-cost. And only one generic generator will be required, not the many specialized generators required by the Makani kite. The gear ratio can be chosen to best match the ground mounted generator.
    Pitch control: The T-Rule states that if a T-shaped object is spun in a circle using a string or rod tied to the bottom of the T, with the central bar of the T lying on a radius of the circle, the top bar of the T will try to lie flat in the plane of rotation due to centrifugal force acting on it, thus creating a centrifugal spring which can be used for blade pitch control. In this case, that means that the blades will try to lie flat in their plane of rotation when revolving.
    In this case, the blade and the ram air rotor shaft create a T shape. Additional weight can be added to the ends of the ram air rotor shafts to increase their resistance to pitching, and/or their length can be increased to increase their moment arm length. That creates a spring that can balance the aerodynamic lift on the blade which tries to make the blade face into its apparent wind. The two forces reach a balance, which is the pitch angle of the blade. The pitch of the blade determines the angle of attack of the blade. So T-Rule pitching can keep the blades from stalling once they are properly balanced. Centrifugal force and aerodynamic lift rise and fall at the same general rate: by the square of the blade speed. So a centrifugal spring can be used to balance aerodynamic lift at all tip speed ratios. I demonstrated T-Rule pitch control of a single blade on a string back in about 1978. I did a recent test with a small model in front of a fan to verify the concept. It works.
    PeterS