Messages in DSUTWP group. Page 1 of 1.

Group: DSUTWP Message: 1 From: Joe Faust Date: 8/16/2013
Subject: Welcome all
Group: DSUTWP Message: 2 From: Joe Faust Date: 8/16/2013
Subject: How to store the gained energy from DSUTWP plants?
Group: DSUTWP Message: 3 From: Joe Faust Date: 8/16/2013
Subject: RATs
Group: DSUTWP Message: 4 From: Joe Faust Date: 8/16/2013
Subject: Model unmanned sailplanes doing dynamic soaring
Group: DSUTWP Message: 5 From: Joe Faust Date: 8/16/2013
Subject: Dynamic Soaring Bibliography
Group: DSUTWP Message: 6 From: Joe Faust Date: 8/16/2013
Subject: Re: Dynamic Soaring Bibliography || L. Hargrave in 1899
Group: DSUTWP Message: 7 From: Joe Faust Date: 8/17/2013
Subject: Re: How to store the gained energy from DSUTWP plants?
Group: DSUTWP Message: 8 From: Joe Faust Date: 8/17/2013
Subject: Re: Dynamic Soaring Bibliography || Raptor Force
Group: DSUTWP Message: 9 From: Joe Faust Date: 8/17/2013
Subject: Study of Cesare Marchetti
Group: DSUTWP Message: 10 From: Joe Faust Date: 8/17/2013
Subject: Liquid air
Group: DSUTWP Message: 11 From: Joe Faust Date: 8/17/2013
Subject: Liquid-Air Bibliography
Group: DSUTWP Message: 12 From: Joe Faust Date: 8/17/2013
Subject: Re: Study of Cesare Marchetti
Group: DSUTWP Message: 13 From: dbmurr@ymail.com Date: 8/17/2013
Subject: possible DSUTWP platforms for study
Group: DSUTWP Message: 14 From: dbmurr@ymail.com Date: 8/19/2013
Subject: Re: Study of Cesare Marchetti
Group: DSUTWP Message: 15 From: Joe Faust Date: 8/19/2013
Subject: Tethered-FFAWE is distinct from FFAWE-IFO WPP or other untethered en
Group: DSUTWP Message: 16 From: dbmurr@ymail.com Date: 8/19/2013
Subject: Re: Tethered-FFAWE is distinct from FFAWE-IFO WPP or other untethere
Group: DSUTWP Message: 17 From: Joe Faust Date: 8/19/2013
Subject: Not dependent on gliding packets of liquid air
Group: DSUTWP Message: 18 From: Joe Faust Date: 8/19/2013
Subject: Group definition changing
Group: DSUTWP Message: 19 From: Joe Faust Date: 8/20/2013
Subject: Almost orbital, solar-powered drone
Group: DSUTWP Message: 20 From: Joe Faust Date: 8/21/2013
Subject: Darin Selby and gliders making liquid air
Group: DSUTWP Message: 21 From: Gabor Dobos Date: 8/24/2013
Subject: Re: [AWES] Liquid air in AWES?
Group: DSUTWP Message: 22 From: Joe Faust Date: 8/24/2013
Subject: Taras Kiceniuk, Jr.
Group: DSUTWP Message: 23 From: Joe Faust Date: 8/24/2013
Subject: The DS explorations of Steve Seibel
Group: DSUTWP Message: 24 From: Joe Faust Date: 8/24/2013
Subject: Re: The DS explorations of Steve Seibel
Group: DSUTWP Message: 25 From: dobosg1 Date: 8/25/2013
Subject: Re: The DS explorations of Steve Seibel
Group: DSUTWP Message: 26 From: dobosg1 Date: 8/25/2013
Subject: Re: Not dependent on gliding packets of liquid air
Group: DSUTWP Message: 27 From: dobosg1 Date: 8/25/2013
Subject: Re: Darin Selby and gliders making liquid air
Group: DSUTWP Message: 28 From: David Lang Date: 8/26/2013
Subject: Re: [AWES] Liquid air in AWES?
Group: DSUTWP Message: 29 From: Joe Faust Date: 8/26/2013
Subject: LA gasification for driving turbines
Group: DSUTWP Message: 30 From: Joe Faust Date: 8/26/2013
Subject: Re: LA gasification for driving turbines
Group: DSUTWP Message: 31 From: Joe Faust Date: 8/26/2013
Subject: LA applications
Group: DSUTWP Message: 32 From: Joe Faust Date: 8/26/2013
Subject: Re: LA applications
Group: DSUTWP Message: 33 From: Gabor Dobos Date: 8/27/2013
Subject: Re: LA applications
Group: DSUTWP Message: 34 From: Joe Faust Date: 8/28/2013
Subject: Onboard Superconductivitgy
Group: DSUTWP Message: 37 From: joe_f_90032 Date: 9/1/2013
Subject: LTAUTRS
Group: DSUTWP Message: 38 From: joe_f_90032 Date: 9/1/2013
Subject: Re: LTAUTRS | LTA structuring
Group: DSUTWP Message: 39 From: Gabor Dobos Date: 9/2/2013
Subject: Re: LTAUTRS | LTA structuring
Group: DSUTWP Message: 40 From: Gabor Dobos Date: 9/2/2013
Subject: Re: [AWES] Liquid air in AWES?
Group: DSUTWP Message: 41 From: Gabor Dobos Date: 9/13/2013
Subject: My poster on AWEC2013
Group: DSUTWP Message: 42 From: joe_f_90032 Date: 9/26/2013
Subject: Expand WPP's mined energy consumers
Group: DSUTWP Message: 43 From: Gabor Dobos Date: 10/1/2013
Subject: Re: Expand WPP's mined energy consumers
Group: DSUTWP Message: 44 From: joe_f_90032 Date: 10/2/2013
Subject: Aloft consumers
Group: DSUTWP Message: 45 From: joe_f_90032 Date: 10/19/2013
Subject: Update on AWEC2013 by Gabor Dobos
Group: DSUTWP Message: 46 From: joe_f_90032 Date: 10/29/2013
Subject: Update: AWEC2013, Part 2
Group: DSUTWP Message: 47 From: Gabor Dobos Date: 12/25/2013
Subject: Fw: LTA: The rise and fall?
Group: DSUTWP Message: 48 From: Gabor Dobos Date: 1/5/2014
Subject: IFO: the proof of concept
Group: DSUTWP Message: 49 From: joe_f_90032 Date: 1/14/2014
Subject: CARDOSO PAULO ALEXANDRE TEIXEIRA E SILVA
Group: DSUTWP Message: 50 From: joe_f_90032 Date: 2/21/2014
Subject: Tether up, then release to untethered phase. Then drive on board gen



Group: DSUTWP Message: 1 From: Joe Faust Date: 8/16/2013
Subject: Welcome all
Welcome all who aim to advance wind power by use of sailplanes using dynamic soaring. 
We begin with an invitation to study the patent application of Gábor Dobos

Owner, Chemotronik Kft,   

WO 2010/106382 A3
at 

~JoeF
Group: DSUTWP Message: 2 From: Joe Faust Date: 8/16/2013
Subject: How to store the gained energy from DSUTWP plants?
How to store the gained energy from DSUTWP plants?



Group: DSUTWP Message: 3 From: Joe Faust Date: 8/16/2013
Subject: RATs
Ram-air turbine on aircraft may be one source of tech for fitting sailplane for energy production. 

In that light, e.g., 
Ducted ram air generator assembly
US 20130048780 A1
Publication numberUS20130048780 A1
Publication typeApplication
Application numberUS 13/215,129
Publication dateFeb 28, 2013
Filing dateAug 22, 2011
Priority dateAug 22, 2011
InventorsMike Mehdi Masoudipour5 More »
Original AssigneeHoneywell International Inc.
External Links: USPTOUSPTO AssignmentEspacenet
Group: DSUTWP Message: 4 From: Joe Faust Date: 8/16/2013
Subject: Model unmanned sailplanes doing dynamic soaring
Model unmanned sailplanes doing dynamic soaring
without generating energy for third-party use may be instructive. There is a world speed record in the model world for DS of a craft. 

www.DSkinetic.com

Yes:  468 mph 

Now we might get these guys to put a RAT on the aircraft and charge a battery!
[[Welcome to DBMurr ... new member!]]
Group: DSUTWP Message: 5 From: Joe Faust Date: 8/16/2013
Subject: Dynamic Soaring Bibliography
All members are encourage to post links in this topic thread that face dynamic soaring matters. Thanks, All. 
=========================================================================

Start: 

General:  DynamicSoaringINTERNET  

Annotations of linked items would enhance this tool. Thanks. 
Then, if an item seems to be a center of study with special interest, the item
could break out to a topic thread on its own. 

Group: DSUTWP Message: 6 From: Joe Faust Date: 8/16/2013
Subject: Re: Dynamic Soaring Bibliography || L. Hargrave in 1899
http://www.ctie.monash.edu.au/hargrave/rs_soaring.html
Soaring Birds are Dependent on Wave-Power
by L. Hargrave
1899


Group: DSUTWP Message: 7 From: Joe Faust Date: 8/17/2013
Subject: Re: How to store the gained energy from DSUTWP plants?
Brainstorm over storing energy from dynamically soaring a sailplane: 

  • Let a RAT torque rubber bands and thus store some energy in the twisted rubber. 
  • Let a RAT drive an electric generator that charges a chemical-based battery. 
  • Let a RAT increase the energy in a flywheel. 
  • Let a RAT drive an air compressor to compress air into cavities/containers. 
  • Let a RAT drive a set of devices that produce liquid air stored in insulated containers. 
  • Let the dynamic soaring increase the kinetic energy of the sailplane. 
  • Let the dynamic soaring increase the potential energy of the sailplane. 
What else?   All are welcome ...
Group: DSUTWP Message: 8 From: Joe Faust Date: 8/17/2013
Subject: Re: Dynamic Soaring Bibliography || Raptor Force
Notes about  physicist Lord Rayleigh.
Comments by Bowers regarding gust soaring. 

Raptor Force 
Thermal vs. Dynamic Soaring

Group: DSUTWP Message: 9 From: Joe Faust Date: 8/17/2013
Subject: Study of Cesare Marchetti
Transport and Storage of Energy  by Cesare Marchetti,
November 1975


Open study of his terms, notions, and predictions. 
An how such matters may affect a wind power plant that uses sailplanes in dynamic soaring may be discussed. 



Group: DSUTWP Message: 10 From: Joe Faust Date: 8/17/2013
Subject: Liquid air
How might liquid air play in a Dobos IFO  or DSUTWP plant (WPP) ? 
We read his works and begin to see how liquid air may be one solution for storing and transporting gains during dynamic-soaring flight of energy-productive sailplanes.    Just how would the liquid air system work?   

Fly the aircraft. Mine part of the dynamic soaring for driving a liquid-air production plant in the sailplane. In various ways get packets of liquid air to exterior receivers. The receivers would let the liquid air be a source for doing practical works.    The feedstock for the liquid air is the air in which the sailplane flies; very handy! The sailplane's liquid-air manufacturing plant never has to carry the feedstock for what would store energy; this contrast with charging chemical storage batteries where the sailplane would carry the chemical batteries before charging and after charging. Similarly, if the sailplane's energy mining were to form starches, then the feedstock chemicals for the starches would have to be carried.   Liquid air uses the air that surrounds the sailplane; just grab some of that air and liquefy it. 

So, how during flight of a dynamically-soaring sailplane produce liquid air?  Dobos rehearses how we need not worry so much about mass of parts, as mass may be used to drive more robust dynamic soaring.    So, use known methods to convert gaseous air into liquid air. 

Will there be reason to separate the to liquid nitrogen and liquid oxygen in the flying system?   Might we use atmospheric moisture to get hydrogen to combine with air's oxygen to power the flying system during climb to altitude or during loss of dynamic-soaring conditions? 

What about the containers for gliding packets of liquid air to reception stations?  Will aerogel play in the structure of the containers? The containers would let gaseous air be released back into the atmosphere. Containers would glide to receiving stations. 

Some of the energy mined might be used to transport a fresh supply of liquid-air containers up to the working sailplane; the sailplane would receive  fresh supply of the containers without having to return to ground stations. 



Group: DSUTWP Message: 11 From: Joe Faust Date: 8/17/2013
Subject: Liquid-Air Bibliography
Group: DSUTWP Message: 12 From: Joe Faust Date: 8/17/2013
Subject: Re: Study of Cesare Marchetti
 Cesare Marchetti is excited about liquid air relative to balancing the heat in cities: 

"If the compressed gas (or my negotiated compromise, liquid 
air) is carried on shore, and used to run the city, all thermal 
balances will be zero: no heat anywhere!"

In the atmosphere, the working IFO  making liquid air will have its heat story to be told by a careful physicist.  The liquid air used from the process to drive a city on soil  will follow the story just quoted.   Gabor, do you want to explain this matter?     Thanks.


Group: DSUTWP Message: 13 From: dbmurr@ymail.com Date: 8/17/2013
Subject: possible DSUTWP platforms for study
Joe,
thank you for this new forum opportunity that studies airborne energy extraction devices that are not tethered to the ground. For me,I believe it worthwhile to develop this type of system first, for many reasons. I will try to convey all these reasons to this group over time, as they are varied & some of the ideas need more study. 

Over the past months I have had the pleasure, and have been personally enlightened through conversations with Gabor Dobos & Wayne German. I have been studying possible solutions for the specific requirements for the individual projects they each are interested in. Back in July I saw what AgustaWestland was working on, and thought their "Project Zero" aircraft was a possible candidate for Gabor's IFO needs. And back in June, Wayne and I emailed each other about Frederick To's great work in the early 80's on "Phoenix", an inflatable man-powered aircraft. I have followed Frederick To's career through to more of his work in the 90's on inflatable aircraft with Andreas Reinhard's company 'Prospective Concepts'. 

'Prospective Concepts' has, in the last few years, spun into several companies. Andreas Reinhard's new R&D company is called "iii solutions" (note: you require 'flash' to search this site). There are many extremely innovative projects shown, but for this forum post I want to point to three in particular. The first (more for Wayne), an insulated aerostat (search 'CURRENT PROJECTS' & see 'Hot-airships'). The second (more for Gabor), the 'HAPS STINGRAY' (search 'CURRENT PROJECTS' & see 'Highflying platforms'). I am assuming this DSUTWP group will discuss any type of FFAWE device (see AWES post #9679 for possible definitions), because this third "iii solutions" project is really pushing boundaries. See the 'HAPS Stratokite' (search 'CURRENT PROJECTS' & see 'Highflying platforms'). I'm encouraged by this 'Stratokite' project because it reminds me of a concept I was working on in 2001, tethered groupings of what we now call FFAWE devices. Here is a 'Wayback Machine' image capture of the "cross-tethered Flyboats" from one of my first 'on-line' archives. 

Hoping for future dynamic lift developments from all.
db murray

Group: DSUTWP Message: 14 From: dbmurr@ymail.com Date: 8/19/2013
Subject: Re: Study of Cesare Marchetti
This is a link to the Cesare Marchetti Web Archive. Many more of his publications are shown here on-line as PDF documents

--- In DSUTWP@yahoogroups.com, "Joe Faust" wrote:
Group: DSUTWP Message: 15 From: Joe Faust Date: 8/19/2013
Subject: Tethered-FFAWE is distinct from FFAWE-IFO WPP or other untethered en
Tethered-FFAWE is distinct from untethered FFAWE-IFO WPP. 
The T-FFAWE is a true kite system facing the dynamic challenges of kite systems. 
UT-FFAWE as IFO WPP is not a kite system. 
Both T- and UT-FFAWE systems have options to send energy packets or product to receiver stations in ways that may be similar; so, there is common interests. Other common interests regard the use of airspace without tethers to the ground, unless the T-FFAWE decides in operation to make contact with ground or water directly which is an important option for T-FFAWES.   
       The kite dynamics of T-FFAWES are steady foci for the group AirborneWindEnergy.     It is a bit unfortunate that the name of the AirborneWindEnergy is not KiteEnergy (though we have rights on a group that is not used of such name).   However, it is pleasant to have the hereon group focus on UT-FFAWE matters with top focus. 

      This forum is public, so post only ideas that are out of stealth mode. Some nations allow patenting within a grace period of reveals; some do not; consult with your patent attorney to help you decide what to post and what not to post. 

      Dobos has stated a believe that UT-FFAWE will have a win over T-AWE and even T-FFAWE  in the fullness of time, perhaps even sooner ... perhaps 15 years from now, if serious effort is made by enough people in the right places.      I personally believe T-FFAWE will win over UT-FFAWE, but am still a student and could change beliefs later.   Right now, I still believe Non-FFAWE energy kite systems will stay dominant once they are mature; but being yet a student, such believe may change.   Because of my beliefs and personal drive for open source, I will not be privy to the private correspondence of some participants. Whatever I post openly will be under a commons license.     But I am a serious student of UT-FFAWE and aim to have implementations occur so that gems are not lost to the world. 

~ JoeF
Group: DSUTWP Message: 16 From: dbmurr@ymail.com Date: 8/19/2013
Subject: Re: Tethered-FFAWE is distinct from FFAWE-IFO WPP or other untethere
Joe,
I would argue that the wording of this forum's definition be altered to allow for more scope, because short tethers would act like hinged joints in a structural frame, and longer tethers connecting FFAWE devices could also function in similar way to how the Dobos IFO's are described. 

I find this statement too limiting for future economies of scale for this type of energy production; "This forum is about soaring systems that do not use tethers to the ground, do not use tethers to other aircraft, and do not use tethers between wings of an integrated flight system. Incidental use of tethers for launching or docking or release of packets, etc. are potential included. But no tethers for the main flight operations."

Without the above stated limiting definition, I would like to explore ideas, like the ones below, in future DSUTWP posts. 

On the AWES forum Dave Santos & others have discussed scaling laws. With this in mind, a Dobos IFO built to a large scale many use modified tethers as wings for dynamic soaring. Or if built to a very large scale, short tethers would function like connective tissues between the bones in a bird's skeletal structure. 

In the Dobos patent abstract there is this line; "The liquid-air containers are made of flexible, double-walled plastic foil, and can be forwarded to the ground station by means of remote controlled or GPS-Guided Parafoils.". I can see future IFOsystems operating along with large scale 'flying' collection stations, as this type could better serve the needs of the smaller collection units due to the probable wide ranging daily migration that a system would experience in very active weather systems. These large flying collection platforms could stay permanently aloft through energy gained from the dynamic wave action of such a system. The short connective tethers would facilitate the flexibility required  in such a large system. Hydrogen production on these large scale platforms would aid with persistence aloft as well as provide a second medium for the storage & sale of energy. It is also possible that the large scale flying platform is the device used for energy collection & medium production, and the smaller scale IFOs are the delivery method to the users on the ground. 

I realize there may be some overlap with the AWES forum because of this, but for now this DSUTWP forum should keep an open mind on the best configuration for an "IFO". 
db murray

--- In DSUTWP@yahoogroups.com, "Joe Faust" wrote:
Group: DSUTWP Message: 17 From: Joe Faust Date: 8/19/2013
Subject: Not dependent on gliding packets of liquid air
I envision that delivery of liquid-air packets need not be totally dependent on gliding.  Rather, some of the liquid air in the delivery process could be used to power the delivery packet to further receiving stations.   

~ JoeF
Group: DSUTWP Message: 18 From: Joe Faust Date: 8/19/2013
Subject: Group definition changing
Good DBMur,  
     How about this new install: 

Mining the atmosphere for energy using aircraft mostly in dynamic soaring mode without conventional kiting tethering to the ground is the focus of this public discussion group. Complete systems or wind-power plants will have energy-storage challenges as energy is captured and ultimately used aloft or elsewhere. Transporting the energy from the the flight system to reception systems form part of the focus here. Exploring energy-storage schemes fit for such DSUTWP plants is of high interest here. Structural and system lofted tethers may place roles.
=====================================

Feel free to tweak it. 
Notice that the new generality permits intermittent powering of the "aircraft" as needed for operations. 

~ JoeF
Group: DSUTWP Message: 19 From: Joe Faust Date: 8/20/2013
Subject: Almost orbital, solar-powered drone
The notes in the article seem to have items that speak to project evolution:

Almost orbital, solar-powered drone 

offered as "atmospheric satellite" 

Titan's Solara, first commercial solar drone, can fly five years without landing.

by Sean Gallagher - Aug 18 2013, 12:00pm PDT

Group: DSUTWP Message: 20 From: Joe Faust Date: 8/21/2013
Subject: Darin Selby and gliders making liquid air
This topic thread invites a study of Darin Selby on liquid air and gliders. 
What was his timeline on reveal text?   What was he saying? Darin, are you there? Thanks. 

In an interview : "I consider myself a kind of 'H.I.P.P.I.E. inventor'
(i.e. Highly Intelligent Person Pursuing Interesting Endeavors).
"

Start: 

Teasing study clips: 
 "Liquid air (-321F) is made either by thermoacoustic refrigeration technology, or by ADR (adiabatic demagnetization refrigeration) as the glider descends from being lifted to 5 miles."  ~ Darin Selby
and
"The symbiosis between the spinning airship and glider could produce a traveling method coast-to-coast of economy lifters, which require gliders to pay with liquid air they make to get lifted up to 5 miles."  ~ Darin Selby

He also has notes  for study on 
and on

Hopefully Darin Selby will join in the discussion. 

Best, 
JoeF

Group: DSUTWP Message: 21 From: Gabor Dobos Date: 8/24/2013
Subject: Re: [AWES] Liquid air in AWES?

Hi David,

Let's begin with the answer:

The heat of evaporation (that is needed to convert liquid air into gaseous form to perform useful work) may come from everywhere. You may apply e.g. heating with a fire or the like.  But our preferred solution  is of course using the heat content of our surroundings to evaporate liquid air in a restricted volume and in this way pressurize it.
 
 The concrete solution depends on the properties of the concrete device as well as on our own decision. The concrete source of heat may be the ambient air, the water of a river, a lake, or the sea, waste heat of a traditional heat power plant, the underground heat-collecting pipes of a heat-pump, etc.


I can say that you see the essence of the process correctly, and the analogy with water is also correct. Your rationale is not breaking down. You just forgot to mention the last step, namely that water vapor must condensate to supply energy by freeing up the condensation heat. Without condensation no heat develops. This process occurs if the water vapor contacts a solid or liquid surface or a gas that is cooler than the temperature of the water vapor. In this case some water vapor will condensate to liquid water and at the same time the condensation heat is released and warms up the above mentioned solid or liquid surface or gas. This heating up process ends if the temperature of the cooler matter reaches the temperature of the water vapor.

As you know, liquid air can be stored at atmospheric pressure while its temperature is equal to its boiling point at the same (ambient) pressure. Just to come closer to a real process, imagine a Dewar flask that has a heat isolating wall. Let this flask contain some liquid air. This is a usual arrangement for storing liquid air and at the same time it is a ready to use experimental setup to answer your question.

In short: due to the insufficient heat isolation, some heat flows continuously trough the wall of the Dewar flask and evaporates some liquid air. That is the explanation of the continuous loss of liquid air, and yes, it is the energy that you are seeking.

Since the temperature of the liquid air is exactly equal to the boiling point of it at the ambient pressure, some liquid air begins to boil and will be evaporated immediately.  The quantity of the evaporated liquid air is in close relation to the heat reaching the liquid air through the wall of the flask. The following equation is valid:

q = m·ΔHv

where
q = heat energy
m = mass
ΔHv = heat of vaporization   

Putting the liquid air into a ballon, we can blow up the ballon  by heating it from te outside with the ambient air.. This simple experiment shows that mechanical work can be made by the liquid air ddue to thee
                                                                                                                                                                                                                                         

This simple qualitative picture is very useful.
Are you satisfied with the answer? Any other qu
estion?


Regards,  Gabor



Group: DSUTWP Message: 22 From: Joe Faust Date: 8/24/2013
Subject: Taras Kiceniuk, Jr.
""I would like to help promote the development of aircraft that is fun to fly and safe," and Kiceniuk said he has "set a personal benchmark" for aviation's newest technology, the electric motor glider, that provides a "blend of the different aspects of flight." Motor gliding is seeing increasing popularity in Europe, but regenerative gliding requires heavy battery power that draws energy from the air from the propeller and stores it for later use."
See full article:  

Group: DSUTWP Message: 23 From: Joe Faust Date: 8/24/2013
Subject: The DS explorations of Steve Seibel
Steve has delighted in examining dynamic soaring (DS).  This topic thread might walk through his DS adventure. 
See his various notes linked off
Group: DSUTWP Message: 24 From: Joe Faust Date: 8/24/2013
Subject: Re: The DS explorations of Steve Seibel
Steve gives a link set: 

Dynamic soaring links: a widespread, steady, updraft or downdraft or headwind or tailwind or crosswind has no effect whatsoever on the force vectors generated by an aircraft flying at a given airspeed in a given direction. However, transient gusts or gradients or shears do affect the force vectors generated by an aircraft flying in a given airspeed in a given direction. "Dynamic soaring" is the exploitation of gusts or gradients to extract energy from the atmosphere. In some cases, an aircraft or bird using "dynamic soaring" techniques can stay aloft indefinitely in unpowered flight even while flying in an airmass that is entirely devoid of updrafts. (For a bit more theory, see www.aeroexperiments.org/dynamicsoaring.shtml.)

Dynamic soaring "type 1": RC model gliders dynamic soaring on the lee side of a hill:

"Dynamic Soaring--the challenge" by Klaus Weiss--a practical article on the lee-side-of-the-hill form of dynamic soaring practiced by RC glider pilots

"Dynamic Soaring (DS) -- the hottest development in R/C soaring in many years!"--another practical article on the lee-side-of-the-hill form of dynamic soaring practiced by RC glider pilots

"How and why does dynamic soaring work?" by Mark Drela--a brief technical article on the lee-side-of-the-hill form of dynamic soaring practiced by RC glider pilots

"Dynamic Soaring on Back Side of Hill"--an illustration for the above article

"Dynamic Soaring"--another brief article, with some technical notes, on the lee-side-of-the-hill form of dynamic soaring practiced by RC glider pilots

"Dynamic Soaring Observations" from NorCal slope soaring--practical tips on dynamic-soaring RC models on the lee side of the hill

"Dynamic Soaring"--More practical tips on dynamic-soaring RC models on the lee side of the hill, along with downloadable video clips

Sample clip from "Lift ticket"--video illustrating RC gliders dynamic-soaring on the back side of the hill

Video clip from North Country Flying Machines illustrating an RC glider dynamic-soaring on the back side of the hill

"Dynamic Soaring video clips"--many more video clips from North County Flying Machines of RC gliders soaring on the back side of the hill (also includes some other types of soaring, not always clear from titles what is being depicted)

First page from "Preliminary Dynamic Soaring Research using a Radio Control Glider" by James Parle--a very technical exploration of dynamic soaring on the lee side of a hill. For more see this link

Dynamic soaring "type 2": using heading changes and "zoom climbs" for "cross-country" travel within the wind gradient over flat ground or over the ocean, as practiced by the albatross :

"Dynamic Soaring"--a simple article, with an animated illustration, about the form of dynamic soaring practiced by the albatross

"How Flies the Albatross: the flight mechanics of dynamic soaring" by J. Phillip Barnes--a fascinating, in-depth article about the form of dynamic soaring practiced by the albatross

An exploratory analysis of dynamic soaring: trajectories in shear layers" by Misty Davies -- a very technical exploration of the form of dynamic soaring practiced by the albatross

Dynamic soaring "type 3": various ways to use transient gusts, and to use the transition between still air and lift or sink, far from the earth's surface, such as are now being explored by full-scale sailplane pilots:

"Dynamic Soaring and Sailplane Energetics" by Taras Kiceniuk--an article introducing the basic principles of soaring without lift

"Calculations on Soaring Sink" by Taras Kiceniuk--an in-depth article on extracting energy from the transitions between still air and sinking air

"Dynamic Soaring of Sink Pockets" by Taras Kiceniuk--an illustration for the above article

"Vector diagram of dynamic soaring: showing how a glider can get energy from a downward gust" by Taras Kiceniuk--an illustration for the above article

"Side gust soaring" by Taras Kiceniuk--an illustration showing how a glider can extract energy from a sideways gust

Dynamic soaring "type 4": combining various ways to use transient gusts and transitions between still air and lift or sink, with a knowledge of fine-scale meteorology:

"Understanding Microlift" from September 6 2002 OZ report--notes from G. Osaba

More notes on putting various types of "dynamic soaring" into practice in full-scale sailplanes:

Extracts from "For Pilots" discussion group: #1

Or in spacecraft...

More dynamic soaring links:

Autonomous dynamic soaring platform for distributed mobile sensor arrays" by Mark B.E. Boslough -- a very technical exploration of various types of dynamic soaring, including the technique used by the albatross and the technique used by RC glider pilots on the lee side of hills

(End of dynamic soaring links)


Steve Seibel of  http://www.aeroexperiments.org   gathered the above set of links.        

Group: DSUTWP Message: 25 From: dobosg1 Date: 8/25/2013
Subject: Re: The DS explorations of Steve Seibel

Hi JoeF,

I am very glad to see the results of your mining the literature.

Well, I have spent several years studying the literature of DSing, among others, the papers of Mark Drella, Kiceniuk Barnes, Sachs and a long line of other authors. I think my patent application contains enough citations from the literature to evaluate the state of the art. Therefore it wasn't  a surprise for me that a downward gustes are also useful for gaining energy with DS:


"Vector diagram of dynamic soaring: showing how a glider can get energy from a downward gust" by Taras Kiceniuk--an illustration for the above article "


But I know, it is not a simple thing to decide where to begin? I would propose the following site:

DSing step by step  

You willl find here a very simple though experiment, calculating a full DSing cycle step by step, together with clear explanations.


Returning to your links, it was a very large surprise for me that renowned members of the community (do not forget we are talking about the AWES !) have essential difficulties with understanding dynamic soaring. The following quotes are more than enough to prove this:  (Without mentioning any names)

"raise the question "once the tether is abandoned, then what besides wind gradient and gravity serves to effectively hold this flying device into the "teeth of wind"?
" My short comment: apart from wind gradient and gravity, only inertial mass is needed... and NOTHING  ELSE (apart from  the necessary knowledge).

try harvesting energy in a uniform 200 kt jet stream with this scheme…..all you end up doing is being swept across the countryside)
My comment: I will NOT try it. I'd like to bring this comment to Doug's attention. This test would be totally pointless. DSing isn't possible in uniform wind. One has to know not only WHAT TO DO, but also WHAT NOT TO DO. But even if you meant 200kt wind gradients, I will not do this experiment, but for the opposite reason: for those skilled in the art it is obvious that it works. (by the way, the unit of wind gradient is not kt but kt/m or kt/foot or inverse seconds, 1/s )

My intuitive assessment of tetherless (ie. non-externally-equilibrated wind force) energy harvesting envisions that reverse-effective forces (ie. d'Alambert forces) are all you have at your disposal to "stand your ground against the wind" (ie. in order to force relative wind to persist at useful levels

Just a short comment: I ask you to forget d'Alambert mechanics! Without enough practice its application can be misleading, like in this case... Newton's mechanics are perfectly  adequate  to discuss DS.

I agree with  the opinion of DaveL:
"If we intend to be serious purveyors of AWE, we must believably quantify the amount of energy we imply that we can harvest."

Because of this, we must be careful not to spread misconceptions or false speculations like the above ones ourselves.
The links you cited are very useful and I am happy to see them indeed. I hope your own results in mining the literature will promote the aim of other fellows too, to study the opportunities ensured by DS, since it maybe useful not only in untethered AWES.  

By the way, the same problem what I wrote about is more significant in the case of liquid air energy storage. But it is another issue.. 

Lift!

Gabor

Group: DSUTWP Message: 26 From: dobosg1 Date: 8/25/2013
Subject: Re: Not dependent on gliding packets of liquid air
Of course, you are right. The means of forwarding liquid air to the ground may be also self-driving tools: see my patent application 11.page 25 It depends only on economics what does it cost to fly larger distances, or how long may be the distance between two adjacent ground stations. It has to be calculated how large circle around the ground station is optimal? It depends on several factors, e.g.: the glide number of the "ferry", whether it has a drive system/motor, the surface relief, the surface winds, etc. I have calculated several possible scenarios. --- E.g.: one of them was State Kansas. Why Kansas? It has a very simple but very serious reason. I listened to the radio and even that time was on the Kansas City, a concert record of the Beatles....

Gabor

PS.: I am glad to see that others are thinking like me. Originally I have thought that these details are the tasks of the future. and others will have new ideas which will complete my ideas. I welcome all new and creative details


Group: DSUTWP Message: 27 From: dobosg1 Date: 8/25/2013
Subject: Re: Darin Selby and gliders making liquid air
JoeF,

I wonder what you can find on the net. I am waiting to hearing from Darin.

Good luck!

Gabor

Group: DSUTWP Message: 28 From: David Lang Date: 8/26/2013
Subject: Re: [AWES] Liquid air in AWES?
Gabor,

Thank you very much for the response. It was helpful.

I would bring attention to two interesting quantifications of this engineering challenge of employing Liquid Air (LA) for energy storage.

1. The rate at which energy can be "retrieved" from LA (power retrieval capability), and

2. The Ratio of "energy that can be retrieved" from LA vs "energy expended to produce the LA" (ie. end-to-end efficiency ETEE).

Elaboration…

item 1: We know that if LA energy RETRIEVAL RATE demands are LOW, then we could rely on a gasification heat source as simple as just letting the LA gasify under the influence of un-augmented ambient heat sources (which would likely represent a low power-retrieval potential, producing a rate of energy-retrieval of little value for industrial-scale storage. However, far more complex heat-exchangers and capable heat sources would be needed to augment the energy-release mechanism to produce significant power retrieval. Are such achievable for practical, cost effective power retrieval?

item 2: It seems one could easily test the ETEE by measuring the simple energy-use of the electric-powered compression system proposed for such as an energy-glider, then taking the resulting LA and submitting it to the energy retrieval process machine (that, presumably results once again in electrical energy) to see what energy would be yielded back.

I bring up these subjects since it seems that for energy gliders to be practical using the LA scheme as the energy-harvest  repository, then said LA storage system must prove worthy (in both design weight and efficiency), else the energy glider will be forced to rely on some other airborne energy transmission scheme (that must pass similar scrutiny), or stand in danger of being impractical. These LA energy-storage assessments can be made even without the full knowledge of the extent of raw energy harvest a glider might be expected to produce (ie. predicted via time-domain simulation of a typical glider/system and maneuver design).

Regards

DaveL





Group: DSUTWP Message: 29 From: Joe Faust Date: 8/26/2013
Subject: LA gasification for driving turbines
LA may be gasified at rates from very slow to near flash. Arrangements  for gasification vary in cost. Each final purpose would need to be engineered for effectiveness and safety.    Expert engineers may be required for any certain project.      So much for the general comments.     This topic thread over time welcomes discussion over the gasification of LA in total systems involving energy hang gliders, energy gliders, or energy sailplanes; that is the full wind-power plant is respected as an object for integrated design.     

Starting: 
The following note is a brainstorm share: 
Consider a large-area black-iron top to a  pressure container. Let the sun heat the black iron. Let the heat produced feed enclosed LA that was harvested from IFOs (Dobos' identified flying object) and delivered to the conversion site.  Let the solar heat gasify the LA and let the obtained pressure drive an electric turbine.   I have no numbers over this share. 
Group: DSUTWP Message: 30 From: Joe Faust Date: 8/26/2013
Subject: Re: LA gasification for driving turbines
http://en.wikipedia.org/wiki/Thermal_energy_storage

Included in "thermal" is the holding of water ice, liquid air (LA), and many other cold gases or liquids. 


Group: DSUTWP Message: 31 From: Joe Faust Date: 8/26/2013
Subject: LA applications
For some motivation toward having DSUTWP systems use liquid air as a generated storage means, this topic thread invites the telling of possible applications for LA. 

Begin: 
LA harvested from use of DSUTWP plants (DSUTWPP or just WPP, if understood in this forum; or IFOs) might be used to do three things in one process: 
        1. Cool a home or refrigeration box. 
        2. Use the gas pressure to drive an electric turbine. 
        3. Inflate a low-pressurized inflatable structure with the exit air. 

There are no doubt hundreds and more applications for LA. Having the applications up and available may play a part in some final effective builds. 
What else, then?

  • Distilling to obtain liquid nitrogen and also liquid oxygen. Then the special uses of those productes. 
  • Inflate the wing of an inflatable aircraft, perhaps the aerial delivery craft from the aerial harvesting IFO. 
  • Drive work tools. 
  • Aerate certain industrial products. 
  • Freeze damp soil during special engineering projects. 
  • Freeze water to ice. Distribute the water ice when the ice reaches more handy temperatures. 
  • ?
  • ?
  • ?
Group: DSUTWP Message: 32 From: Joe Faust Date: 8/26/2013
Subject: Re: LA applications
  • http://www.dearmanengine.com/cms/liquid-air/
    • Run small demonstrator engine
    • Run handy workbench scale engine
    • Run a car
  • http://www.dearmanengine.com/cms/applications/    mentions the following: 
    • forklifts
    • golf carts
    • tools
    • bikes
    • trucks
    • buses
    • underground mining equipment
    • waterways material handling machines
    • port machinery
  • Mentioned in a post in AWES group:  creating ballast for a sailplane or hang glider. Then when not wanting the ballast consider using the gasification for powering the glider or sailplane or some instrument or process on board. 
  • Look for applications of LOX      ?
  • Look for applications for liquid nitrogen
  • Look for applications for argon gas
  • Drive turbines to make electricity for small or large loads.   See the thousands of applications for electricity. 
  • ?
Group: DSUTWP Message: 33 From: Gabor Dobos Date: 8/27/2013
Subject: Re: LA applications
Yes, JoeF,

these all are very important and useful opprotunities. But probably, the most important one is missing. Namely the "onboard" superconducting technology, that can be applied everywher wher liquid air is applied. It is a distinct topic, and ought to write abouot it a separate paper, . I would like to mention just one application, namely the     motor-generator.  As you know, the rotor of our wind power plant is a bi-functional device, from two points of view. On the one hand, if the propeller is powered by the electric motor of the aircraft, it produces thrust for the plane during takeoff. After reaching an appropriate wind shear, the software switches the propulsion off, and begins harvesting energy. In this case, the relative wind rotates the prop and it functions as a windmill. This means that it rotates the shaft of the motor, which starts to function as a generator and produces electricity.

 The main attribute of this motor-generator is its large power to weight ratio. The limit of today’s technical state puts this at 10 kW/kg i, but a superconducting device cooled with liquid nitrogen may reach even 20 kW/kg. There is extensive researchii in this field and a predicted value of 25-40 kW/kg in the case of motors and about 40-80 kW/kg in the case of generators may be found in the literature. We are near to, but within the limits of reality if using 8 kW/kg in our calculations of IFO.  Imagine: a generator of 1 kg weight is capable to produce 80 kW power. Imegine: the mmotor of your car weights no more than 1 kilogram!  Of course there are also several other possibilities of application.

Gabor




Group: DSUTWP Message: 34 From: Joe Faust Date: 8/28/2013
Subject: Onboard Superconductivitgy
Upon the focused notice from Gabor Dobos, and with agreement, the LA application onboard DSUTWP flying devices  with respect to opportunities of  "Onboard Superconductivity" receives now a topic thread with special focus.  
============================================

Study, discussion, related papers, links, etc. are invited for DSUTWP flying devices and the role that superconductivity may play in practical systems. 
Group: DSUTWP Message: 37 From: joe_f_90032 Date: 9/1/2013
Subject: LTAUTRS

 This topic regards LTA untethered receiving stations (LTAUTRS). Thanks to the nudges from DBMurr!      We have elsewhere already some start on ground-based receiving stations (GBRS); and, of course, ground-based receiving stations may or may not coordinate with airborne LTA receiving stations, depending on niche system design.  


Noting now that LTAUTRS may be small in size or large or very large; size will be determined by missions.  DBMurr has shared some about very large LTAUTRS (VL-LTAUTRS) with some notice about the design of the skin of the macro craft involved where the skin might be solar-energy collector that might produce hydrogen from water moisture even while the LTAUTRS receives liquid-air packets from such as IFOs. 

Airborne factories and life units and operating drones, etc. might recharge from LTAUTRS.    The LTAUTRS would be like central hubs or filling stations. 
Group: DSUTWP Message: 38 From: joe_f_90032 Date: 9/1/2013
Subject: Re: LTAUTRS | LTA structuring

DMurr directed some attention to a researcher that has made some progress on vacuum balloons:: 


Microfabricating the First-Ever Lighter-Than-Air Solid Structure by Dr. Gavrilin





Group: DSUTWP Message: 39 From: Gabor Dobos Date: 9/2/2013
Subject: Re: LTAUTRS | LTA structuring
Very interesting! In the link there is given a contact for licensing opportunities:


Group: DSUTWP Message: 40 From: Gabor Dobos Date: 9/2/2013
Subject: Re: [AWES] Liquid air in AWES?
DaveL,
thank you for your kind response. I didn't forget it, but currently I havn't enough time (a day is no longer than 25 hours....)  I will answer soon.
Regards,
Gabor



Group: DSUTWP Message: 41 From: Gabor Dobos Date: 9/13/2013
Subject: My poster on AWEC2013
Dear Friends,

please find attached my poster published on the AWEC2013 in Berlin.

Regards,

Gabor
  @@attachment@@
Group: DSUTWP Message: 42 From: joe_f_90032 Date: 9/26/2013
Subject: Expand WPP's mined energy consumers
This note is about expanding "WPP" into a realm that DOES NOT need to send energy to the ground.    Expandingly, let WPP generate energy for supply of other aircraft; there is no need to require that energy packets be sent to the ground for consumers. The consumers may be other aircraft.  Let a DSUWPP have a choice of where the gained energy will be spent; the gained energy may be spent in itself beyond its mere self-flight, say for manufacturing purposes or utility for passenger resort, or sent to other aircraft for energy spending, or spent on the ground.  Let us not constrain DSUWPP to just ground consumers.


JoeF
Group: DSUTWP Message: 43 From: Gabor Dobos Date: 10/1/2013
Subject: Re: Expand WPP's mined energy consumers
Congratulations JoeF.  It is really a great idea!

I propose to further think on the most general wording. Writing my patent application, I needed to mark off my solution only from J. P. Barnes's "regenerative soaring". (You can find the details in the published application.) I suppose one can find more general wording than that of mine.

Good luck,

Gabor  

PS.: I am afraid, there is today not enough demand on midair refueling of aircrafts, but it is only a guess. Maybe, the demand is given, "only" the infrastructure is missing.




Group: DSUTWP Message: 44 From: joe_f_90032 Date: 10/2/2013
Subject: Aloft consumers
This topic thread invites study of "aloft consumers" of energy gained from DSUTWP


1. Aviation has not yet had systems making energy packets  aloft for aloft consumption, except in the self-sustaining soaring and regenerative soaring and minor battery-recharge arena.   What may occur is a whole new set of opportunities that would unfold as capability for supplying aloft-produced energy advanced. 

2. Living in the skies is a project that has crawled only slowly. Advanced schemes of living in the skies consider various energy-production schemes. DSUTWP could be one avenue of energy supply for living quarters that do not return to the ground. 

3. Let DSUTWP production give energy packets to SkyPalace (SP); or let fetching agents (FA) from SP go out to fetch energy packets (EPs) left in the sky by working DSUTWP units.   The FA might run double-duty by supplying DSUTWP workers with empty envelopes for use in further packaging energy.   SP would receive from FA the filled EPs. FA would go out and give DSUTWP workers empty EPs and then fetch filled EPs that were left in the sky for fetch. Part of the economy of the operations would involve equipotential operations, i.e., avoid FA from going to low altitudes, but rather aim to have FA operate near a single altitude for its duties. 

4. SP could be small or large. Activity in SP may vary from uninhabited special-duty operations to mammoth inhabited operations.  Resort living, manufacturing, retreat place, conference space, school, city, headquarters, ...

5.  Have aircraft that very rarely come to the ground, if ever. Let mother aircraft let out passengers in gliders along a route. Let mother aircraft stay at altitude. Let new incoming passengers be lofted along the way by mini-lifters; mother ship would have FA to bring in the mini-lifted passenger capsules. Mother aircraft keeps going and going and going ... receiving energy from various means as well as from DSUWP workers. The materials of the mini-lifters would supply format materials for the release-of-passenger gliders.   Mother aircraft could receive products from SP that recycled materials and manufactured items and grew or manufactured food.    Mother transport aircraft could move people and objects  from one SP to another.
Group: DSUTWP Message: 45 From: joe_f_90032 Date: 10/19/2013
Subject: Update on AWEC2013 by Gabor Dobos
  • Group: Friends of DG's Flying Wind Power Plant
  • Subject: AWEC2013

Dear Friends,

Please find my poster presented at the AWEC2013 Airborne Wind Energy Conference in Berlin at the following link: http://uploadingit.com/file/ gcrzgrhfskkngxlz/IFO_awec2013_ poster_Dobos.pdf . The website of the conference: www.awec2013.de. The „Book of Abstracts” can be downloaded from: http://www.awec2013.de/index. php?page=speaker#abstracts . (for our IFO, see: p. 62.)

It was very interesting to see that even though several types of airborne devices are proposed to harvest energy from high altitude winds, all have a common feature, namely the tether, that connects the device to a ground station. While listening to the presentations and reading the abstracts, my father comes to mind. He was a handyman, and was always tinkering with something. He could have become a phenomenal engineer, had his circumstances made it possible. He has, as fathers usually do, built kites of several types for me. I enjoyed playing around with kites, and I like to see them fly even today., e.g.: at

http://vimeo.com/74443367/ download?t=1381616303&v= 189628928&s= f9fe1bd0f9a710f0abe21b387c07d4 df 

But I remember very clearly that we always had difficulties with the tether. Altogether, we spent much more time with the tether than with all the other parts of the kite or with flying it. This is probably the origin of my aversion to the tether. Of course, one can say that these were problems of a toy. They would be right. But probably, the central task of even today's kites is the construction of tethering and related issues. It was interesting to see that a lot of presentations at the conference also dealt with these problems. Though the scientific-industrial background seems to be significant and persuasive, the results are just starting to approach a desired technical standard and reliability. This is not only my guess, but also the opinion of experts: “Kite-power systems ... need an accurate control system ... to cover the main dynamic behavior of all system components: the kite, the tether and the ground station. To the best knowledge of the authors, no system model was published until now that covers the dynamics of all three system components.” (see: Dynamic Kite-Power System Modeling. Uwe Fechner, Rolf van der Vlugt, Roland Schmehl, Delft University of Technology, Book of Abstracts p. 42.)

In comparison to the sophisticated glider/UAV/drone constructions and their guidance systems of today, it seems that these untethered autonomous devices have an advantage of several years in respect to kites. I am convinced even more than I was before the conference that untethered flying devices like our IFOs will be the winners in this race of technologies. But there are also several other reasons for why I think so.* First of all, our IFOs are not tethered to the ground and therefore their activity radius isn’t restricted by the length of the tether. IFOs need not wait for good winds, they can follow them. This way, one of the important drawbacks of other wind power harvesting devices, namely the low capacity factor, caused by the fluctuation of the winds can be eliminated. This action alone results in duplication of the harvested energy.

Another key topic of the conference was energy storage.

Prof. Chul Park's liquid hydrogen producing parafoil-pulled ships represent a very interesting complex approach to the problems (Book of Abstracts p.33.) Since our posters were second neighbors, we have met up right at the beginning of the conference, and we had interesting discussions about economy, cryotechnology and ways of energy storage. Later on, he introduced me to Prof. Michael Sterner, who proposes to convert the produced hydrogen to methane, “which is fully compatible with today's natural gas infrastructure.” (Book of Abstracts p. 34.) 

To be continued.

Gabor 

Group: DSUTWP Message: 46 From: joe_f_90032 Date: 10/29/2013
Subject: Update: AWEC2013, Part 2
AWEC2013, part 2.

Speaking of hydrogen and energy storage, please allow me to mention a Hungarian breakthrough in hydrogen-storage. Prof . Ferenc Joó (University of Debrecen in Hungary) and his coworkers solved the catalytic hydrogenation of carbon dioxide under mild reaction conditions, see : 

Joó F.: Breakthroughs in Hydrogen Storage - Formic Acid as a Sustainable Storage Material for Hydrogen. CHEMSUSCHEM: CHEMISTRY & SUSTAINABILITY, ENERGY & MATERIALS 1:(10) pp. 805-808. (2008)

Joó, F. (2010) Activation of Carbon Dioxide, in Physical Inorganic Chemistry: Reactions, Processes, and Applications (ed A. Bakac), John Wiley & Sons, Inc., Hoboken, NJ, USA. doi: 10.1002/978047060

Papp, G., Csorba, J., Laurenczy, G. and Joó, F. (2011), A Charge/Discharge Device for Chemical Hydrogen Storage and Generation . Angew. Chem. Int. Ed., 50: 10433¨C10435. doi: 10.1002/anie.201104951 

The above results open a new path of chemical energy storage, and at the same time act against global warming by fixing CO2 in the form of a low molecular weight organic compound (formic acid) produced by catalytic hydrogenation. On the one hand, the reversibility of the reaction ensures a simple mode of hydrogen-storage, and on the other hand formic acid is a bestseller basic compound in the chemical industry. This is an example that basic research may have a direct contact to, and can answer the problems of the real world.

My invention regards to a possible first step in this line, namely the primary energy storage in form of liquid air on-board an energy harvesting glider (see: WO 2010/106382 A3 and Hungarian patent registration number 227 468). One of the main advantages of it is the outstanding efficiency of the retrieval of the stored energy from liquid air (LA). The process proceeds in a heat engine that has a cold heat sink cooled with LA. While evaporating, LA maintains the cold heat sink temperature at the boiling point of liquid air, 79 K. The evaporated and in this way pressurized LA drives the engine (in the simplest case). The warm heat sink of the engine can harvest the energy of several heat sources. It is interesting to see the Carnot-efficiencies of the engine depending on the temperature of the warm heat sink (TH) as follows:

1. TH = 273 K = 0 Centigrade, 
Heat source e.g. the ambient air or a river or the sea
Carnot efficiency = 71 %

2. TH = 373 K = 100 Centigrade, 
Heat source e.g. waste heat (cooling water) of a conventional steam power plant
Carnot efficiency = 79 %

3. TH = 800 K = 523 Centigrade, 
Heat source the boiler-wall temperature of a typical steam power plant, but cooled with LA
Carnot efficiency = 90 %

As a reference for a typical steam power plant operating between TH=800 K (boiler) and TL=300 K(cooling tower), the maximum achievable Carnot-efficiency is 62.5%. 

The latter is the state of the art today. To improve efficiency by enhancing the warm heat sink temperature careful further research of structural materials is needed. It is a slow and continuous development. But lowering the cold heat sink temperature to 79 K results in prompt and significant enhancement of efficiency. Though it is “only” a theoretical possibility, approaching 90% Carnot-efficiency in a heat-engine may justify to start revising our thinking of heat energy being a “low- grade” one . 

Today LA energy storage seams to be one of the promising opportunities. Take a look please also at the following links: 
http://youtu.be/19cGYcsk2sM%20 http://www.liquidair.org.uk/ . (Thanks to our member, Joe Faust for mining a lot of literature data to the topic.)

The above mentioned examples show that the research of energy storage has very promising results. I mean, not only batteries and supercapacitors are the possible winners of this race of technologies but also the above mentioned ones.

Best regards,

Gábor
 
Group: DSUTWP Message: 47 From: Gabor Dobos Date: 12/25/2013
Subject: Fw: LTA: The rise and fall?


On Tuesday, December 24, 2013 11:50 AM, Gabor Dobos <dobosg1@yahoo.com
Group: DSUTWP Message: 48 From: Gabor Dobos Date: 1/5/2014
Subject: IFO: the proof of concept
Gentlemen,

it is time to respond to your posts below. Take a look please at the following two links:
This is the proof of concept of my energy harvesting gliders ("IFO") that you wanted to see.

"Re-GENERATION SYSTEM:
Our electric re-gen systems provides battery charging during non-powered flight/gliding. This system can also be used with our folding prop to force the motor to stop so the prop can fold. "
http://www.electraflyer.com/price_list.php

The following link contains a photo of the aircraft:
http://www.planeandpilotmag.com/pilot-talk/more-pilot-talk/light-sport-chronicles-profiles-in-vision-randall-fishman.html

I have received some further details from the company about the solution and how it functions. It can be integrated into our preliminary plan, though of course a further development is needed.
There is nothing unforeseeable. As I told before

The larger part of the whole system can be developed and constructed this way, using "off-the-shelf" components. Other parts of the system need further research work.


DaveS, yes, dreams are dreams. But don't forget: toda la vida es sueno, and I dare to dream great, though sometimes it is un frenesi, sometimes una illusion, sometimes una ficción. But now (and for some time now) it is the reality.

Doug, just one question: are you serious? I am.

Gabor

-----------------------------------------------------------------------

PS.: Your cited posts:



On 2013-08-23 17:18, Doug wrote:

On 2013-09-04 17:44, dougselsam@yahoo.com wrote:

Group: DSUTWP Message: 49 From: joe_f_90032 Date: 1/14/2014
Subject: CARDOSO PAULO ALEXANDRE TEIXEIRA E SILVA


CARDOSO PAULO ALEXANDRE TEIXEIRA E SILVA
from Portugal
Does he address some of our concerns?
Group: DSUTWP Message: 50 From: joe_f_90032 Date: 2/21/2014
Subject: Tether up, then release to untethered phase. Then drive on board gen
Not directly Gabor IFO, but: 

Use ground as anchor to a kited wing. Fly the wing under tether to a great altitude; such converts the wind energy into potential energy in the wing. Then upon reaching desired altitude release from tether and glide and soar and dynamically soar until reaching ground; have on board RATs and batteries to be charged. Finally land with charged batteries. Exchange the batteries for to-be-charged batteries; then hook into the tether for another kited lift to altitude; release again and charge batteries again. Repeat this cycle over and over again. Launch hundreds of wings under tether and then enter the untethered mode for the generation mode. Use that potential energy to drive the RATs to charge the batteries.       This system is mechanically not new. The emphasis for production line has some freshness.  This can be done today with model sailplanes, manned hang gliders, manned sailplanes.    ~ JoeF   
PS: In a way, hang glider pilots get a "charge" after tow release; they land fully charged up (adrenaline) from the untethered gliding, soaring, and some dynamic soaring. Their "batteries" are recharged; they use their recreational heightened energy to go through the work week.