Messages in AirborneWindEnergy group.                       AWES3289to3338 Page 46 of 79.

Group: AirborneWindEnergy Message: 3289 From: Pierre Benhaiem Date: 4/5/2011
Subject: Makani M1 and FlygenKite

Group: AirborneWindEnergy Message: 3290 From: simon_0987 Date: 4/5/2011
Subject: Re: In which countries can you fly your kites legally?

Group: AirborneWindEnergy Message: 3291 From: simon_0987 Date: 4/5/2011
Subject: Hang a windmill in the air, and put the generator on the ground

Group: AirborneWindEnergy Message: 3292 From: Hardensoft International Limited Date: 4/5/2011
Subject: Re: Power Plant Direct Staffing Requirements

Group: AirborneWindEnergy Message: 3293 From: simon_0987 Date: 4/5/2011
Subject: Re: Please Forward to Ben Harder ("Start-ups are devising kites..."

Group: AirborneWindEnergy Message: 3294 From: Pierre BENHAIEM Date: 4/5/2011
Subject: Re: In which countries can you fly your kites legally?

Group: AirborneWindEnergy Message: 3295 From: Joe Faust Date: 4/6/2011
Subject: AWEify

Group: AirborneWindEnergy Message: 3296 From: Joe Faust Date: 4/6/2011
Subject: Welcome David Carmein

Group: AirborneWindEnergy Message: 3297 From: Joe Faust Date: 4/6/2011
Subject: Hermann Oberth

Group: AirborneWindEnergy Message: 3298 From: dave santos Date: 4/6/2011
Subject: Simon's Line Handling Questions

Group: AirborneWindEnergy Message: 3299 From: simon_0987 Date: 4/7/2011
Subject: Re: Simon's Line Handling Questions

Group: AirborneWindEnergy Message: 3300 From: Doug Date: 4/7/2011
Subject: Re: Makani M1

Group: AirborneWindEnergy Message: 3301 From: Theo Schmidt Date: 4/8/2011
Subject: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3302 From: simon_0987 Date: 4/8/2011
Subject: High Plateaus of the World

Group: AirborneWindEnergy Message: 3303 From: Pierre Benhaiem Date: 4/8/2011
Subject: Re: Makani M1

Group: AirborneWindEnergy Message: 3304 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3305 From: Pierre BENHAIEM Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3306 From: dave santos Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3307 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3308 From: Pierre Benhaiem Date: 4/8/2011
Subject: Re: Makani M1

Group: AirborneWindEnergy Message: 3309 From: North, David D. (LARC-E402) Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3310 From: Doug Date: 4/8/2011
Subject: Re: High Plateaus of the World

Group: AirborneWindEnergy Message: 3311 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3312 From: Pierre BENHAIEM Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3313 From: dave santos Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3314 From: Bob Stuart Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

Group: AirborneWindEnergy Message: 3315 From: simon_0987 Date: 4/9/2011
Subject: Re: High Plateaus of the World

Group: AirborneWindEnergy Message: 3316 From: dave santos Date: 4/9/2011
Subject: Re: High Plateaus of the World

Group: AirborneWindEnergy Message: 3317 From: Pierre BENHAIEM Date: 4/9/2011
Subject: Re: Makani M1

Group: AirborneWindEnergy Message: 3318 From: simon_0987 Date: 4/9/2011
Subject: Re: High Plateaus of the World

Group: AirborneWindEnergy Message: 3319 From: Joe Faust Date: 4/9/2011
Subject: Re: AWEA conference wants diversity without AWE, apparently ...

Group: AirborneWindEnergy Message: 3320 From: Joe Faust Date: 4/9/2011
Subject: Re: AWEA conference wants diversity without AWE, apparently ...

Group: AirborneWindEnergy Message: 3321 From: Theo Schmidt Date: 4/10/2011
Subject: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

Group: AirborneWindEnergy Message: 3322 From: Bob Stuart Date: 4/10/2011
Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

Group: AirborneWindEnergy Message: 3323 From: Joe Faust Date: 4/10/2011
Subject: What? What could be conducted via tethers?

Group: AirborneWindEnergy Message: 3324 From: Joe Faust Date: 4/10/2011
Subject: Re: What? What could be conducted via tethers?

Group: AirborneWindEnergy Message: 3325 From: Robert Copcutt Date: 4/10/2011
Subject: Automation of AWE

Group: AirborneWindEnergy Message: 3326 From: Robert Copcutt Date: 4/10/2011
Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

Group: AirborneWindEnergy Message: 3327 From: Pierre BENHAIEM Date: 4/10/2011
Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

Group: AirborneWindEnergy Message: 3328 From: Robert Copcutt Date: 4/10/2011
Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

Group: AirborneWindEnergy Message: 3329 From: dave santos Date: 4/10/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3330 From: simon_0987 Date: 4/10/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3331 From: Robert Copcutt Date: 4/10/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3332 From: dave santos Date: 4/10/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3333 From: Bob Stuart Date: 4/10/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3334 From: christopher carlin Date: 4/11/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3335 From: Robert Copcutt Date: 4/11/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3336 From: Joe Faust Date: 4/11/2011
Subject: Retail product from Pacific Power Sails

Group: AirborneWindEnergy Message: 3337 From: Dave Lang Date: 4/11/2011
Subject: Re: Automation of AWE

Group: AirborneWindEnergy Message: 3338 From: dave santos Date: 4/11/2011
Subject: Re: Automation of AWE




Group: AirborneWindEnergy Message: 3289 From: Pierre Benhaiem Date: 4/5/2011
Subject: Makani M1 and FlygenKite

DaveS and all,

My idea is beginning to see the difference between a mount on a stick under a kite of type parafoil (FlygenKite ) and a mount on a rigid wing (Makani),excepted the specific use of FlygenKite as a cheap model making to load batteries.

Like for precedent messages only losses of output in rapport to Betz limit of rotors aloft are taken into account.So we take a value of 76.548% Betz limit to obtain round numbers for 1 MW with wind speed = 9 m/s.It can be considered that CL/CD of Makani M1 is some value like the double of CL/CD of FlygenKite.Note the following numbers (like for precedent messages) are not the reality but only a hypothesis of working. 

Makani M1:CL/CD = 12; area is 175 m²

FlygenKite:CL/CD = 6; area is 700 m²

Makani M1:advantages could be less area,possibility of high voltage and less losses in the conductive tether because of high kite speed; disadvantages could be the reverse of the medal:problems of safety and also reliability (altitude of work is limited,so an error close to the ground can be a crash) due both to the rigidity and the weight of the wing and its great speed,and also the too high turbine tip speed.

FlygenKite:avantages and disadvantages are inverted.Other advantage:using existing soft wings (of type parafoil).

Of course a more detailed study is needed.For example what are the real aerodynamic losses of the mount of turbines on Makani M1.Indeed during loops such mounts can slow down the kite.Other examples are shown in a recent post from DaveS:losses in conductive tether,generator etc...

PierreB

http://flygenkite.com   

 

Group: AirborneWindEnergy Message: 3290 From: simon_0987 Date: 4/5/2011
Subject: Re: In which countries can you fly your kites legally?
Hi Pierre,

Thank you for your reply :)

Is it easy to get this planning of flight for an experimental tethered kite? And is there a limit to the height and duration? Do you have the name of the French government agency responsible for enforcement?



... on my original post: I guess I'm looking for the aviation authority for every country, so I can ask them. Or for someone who has a general overview of international aviation regulations.




Group: AirborneWindEnergy Message: 3291 From: simon_0987 Date: 4/5/2011
Subject: Hang a windmill in the air, and put the generator on the ground
Hi,

Seeing Dave's drawing on the homepage, I am reminded about my own idea of how to hang a windmill from a kite/balloon: a loop of line wound around a spool attached to the windmill, and going down to the ground and driving a generator (you could also use this in conventional wind-turbines).

Questions:

1. What kind of line (smooth/rough) and spool (threaded/un-threaded) would you use?

2. How much tension would have to be put one the line?

3. How long could you make the line?

4. Why isn't this used in conventional windmills. The generator weighs 50 tons, after all.
Group: AirborneWindEnergy Message: 3292 From: Hardensoft International Limited Date: 4/5/2011
Subject: Re: Power Plant Direct Staffing Requirements
In a world of ever-increasing population, employment will always be necessary and is indeed becoming a considerable deciding factor in government expenditure / policy initiative the world over.
Efficient engagement of humans in profitable employment on any project (including AWE projects) for as long as possible will certainly be most beneficial.


Group: AirborneWindEnergy Message: 3293 From: simon_0987 Date: 4/5/2011
Subject: Re: Please Forward to Ben Harder ("Start-ups are devising kites..."
The contact information is at the bottom of the page?

Harder is the general manager of Health and Science at U.S. News & World Report. <<<

Or you can send your inquiries to "particular staff members" at http://www.usnews.com/usnews/usinfo/infomain.htm
Group: AirborneWindEnergy Message: 3294 From: Pierre BENHAIEM Date: 4/5/2011
Subject: Re: In which countries can you fly your kites legally?

Hello Simon,

"Is it easy to get this planning of flight for an experimental tethered kite?".I think the user has the obligation to submit a planning of flight towards the authority.

PierreB

Aviation authority in France:Direction générale de l'aviation civile (DGAC)






Group: AirborneWindEnergy Message: 3295 From: Joe Faust Date: 4/6/2011
Subject: AWEify

 AWEify           
 Look at a tech matter and wonder if that matter could play a part in energy kite systems or airborne wind energy systems; that wondering is about integrating a subject tech into AWE or AWECS.   Verb: "AWEify" .   Ask about any tech: Can that be AWEified?
 

 

Group: AirborneWindEnergy Message: 3296 From: Joe Faust Date: 4/6/2011
Subject: Welcome David Carmein

Welcome David Carmein

http://energykitesystems.net/Carmein

Best of Lift to you and yours, David,

JoeF

 

Group: AirborneWindEnergy Message: 3297 From: Joe Faust Date: 4/6/2011
Subject: Hermann Oberth

Though he passed, he is returning to AWE  ...
[ ] Welcome any furthering on Hermann Oberth and his kite power station and upper windpower interests!   Here is snapshot of new folder
http://www.energykitesystems.net/Oberth/

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

Home                                           Your notes are welcome: Editor@UpperWindpower.com


Hermann Oberth
and his presentation for "Kite Power Station"
Hermann Julius Oberth

  • Here is a small mystery, a legendary rocket scientist thinking about AWE in 1973.

    Hermann Oberth
    From Wikipedia Oberth page (no reference):
    • The 1973 petroleum crisis inspired Oberth to look into alternative energy sources, including a plan for a wind power station that could utilize the jet stream.

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

      Comment from KiteGen site-
  • [ ]  Find the book
  • [ ]  Search his life
  • [ ]  Edit the wiki when solid reference is found for the AWE
  • [ ]  See how "kite" comes in. Compare the "balloon" notes.
  • [ ]
  • ACTION LOG
    • Sent inquiry to museum images and text concerning Oberth's kite power station.
    • Put Oberth on founders' list
    • Added Oberth item in timeline at wiki of High altitude wind power

Group: AirborneWindEnergy Message: 3298 From: dave santos Date: 4/6/2011
Subject: Simon's Line Handling Questions

Simon posed these...

Questions:

1. What kind of line (smooth/rough) and spool (threaded/un-threaded) would you use?

2. How much tension would have to be put one the line?

3. How long could you make the line?

4. Why isn't this used in conventional windmills. The generator weighs 50 tons, after all.

REPLY: For mechanical power transmission with lines, use the best overall braided kiteline, usually UHMWPE. Its slick, so one can specify a coating like urethane & the extra stiffness of a coating helps line run free in tackle. Capstan spools are unthreaded unless the line action is a short oscillation. A finely etched or sandblasted texture is common on a capstan spool, but holding friction with each line-wrap mounts exponentially, so three wraps handles most any load, with a couple extra wraps for slippery or jumpy conditions. Storage reels are sometimes threaded if they have a level-wind feature.
 
Never put more tension on a line than its working load, use an 8-to-1 safety margin for high duty & high risk, otherwise always have at least a 4-to-1 safety margin, since kites are highly dynamic. Always maintain minimal tension on a line to avoid snarls. An over-running spool is usually tamed with a drag.  Compressed air or water flow is sometimes used to blow lines out of fairlead tubes to maintain minimal tension. 
 
A line can be as long as design load, lift, & aerodrag allow. Flying kites at 10000m is definitely within the capability of UHMWPE, with the required safety factor.
 
The main reasons conventional windmills do not use a line or belt loop to the ground is that the deadweight of the generator aloft is a small factor compared to live wind loads & running a mechanical loop it complicates the weathervaning & tends to reduce reliability & increase maintenence, but its still a design option. For kites, mechanical transmission with lines is the most basic tool to tap high altitude wind.
 
All these issues are mastered by practicing advanced rigging in fields like fishing, sailing, rock-climbing, cranework, & kiting.
 
daveS
Group: AirborneWindEnergy Message: 3299 From: simon_0987 Date: 4/7/2011
Subject: Re: Simon's Line Handling Questions
Thanks :)

You've cleared that up for me.
Group: AirborneWindEnergy Message: 3300 From: Doug Date: 4/7/2011
Subject: Re: Makani M1
Also note:
The Betz coefficient is 59%, but few turbines attain or even approach it. To speak of achieving the Betz coefficient across a whole section of sky is to assume you have near-perfect performance across the entire flight path, with your placement and solidity perfected so that only the absolute minimum of air "leaks" through your system.

A WECS (wind energy conversion system) operating at the Betz theoretical maximum, by definition, must lower the wind speed to 1/2 at the plane of operation (assuming there IS a plane of operation), and the flow exiting the area will be an expanded wake traveling at 1/3 the ambient wind speed.

Good luck achieving anything close to that by flying a kite across a section of sky, especially when your kite itself is not even taking power directly, but with propellers mounted on the kite taking the power.

Also consider the "compound Betz coefficient" that might manifest: the system as a whole has its Betz coefficient, meaning the main wing, acting as what we call a blade, has a Betz coefficient of 59% to try and approach (30% is a high average) but then the propeller has its own Betz coefficient.

I think those guys doing this are courageous to at least be trying instead of just talking, but one concern about the compound effect of a crosswind blade driving a crosswind blade, is this if the aircraft travels at say 6 times the wind speed, necessary to extract anything near the betz coefficient, then in a 40 mph wind, it's going 240 mph. Then the propeller is going mach 2.

In the real world of working turbines, this is at the edge of an overspeed situation when the blades are going this fast. I like to run my turbines this fast but most people don't. They can get a bit noisy.

Now, consider a piggyback propeller: - a whirling blade, riding on the blade. At a 6:1 Tip Speed Ratio, the propeller blade tips will travel at 240 mph x 6 = 1440 mph = Mach 2 !!!

Seems to me that any serious attempt to come anywhere near even a double-digit fraction of energy, approaching say 1/6th of the Betz Coefficient over a wide area of sky would entail high mach numbers and be noisy.

Maboomba.
Doug Selsam

Group: AirborneWindEnergy Message: 3301 From: Theo Schmidt Date: 4/8/2011
Subject: Betz limit [was: Re: [AWECS] Re: Makani M1]
Doug wrote:
I agree. The Betz limit is an important concept but I think of minor
interest for AWE. The constraints are mainly structural, handling and
safety. And we are interested in effectiveness in terms of power
produced in relationship to line force. With a stationary turbine this
would be power produced in relationship to resistance, i.e. torque on
the tower. I expect that line force costs more than tower torque.

Theo Schmidt
Group: AirborneWindEnergy Message: 3302 From: simon_0987 Date: 4/8/2011
Subject: High Plateaus of the World
http://en.wikipedia.org/wiki/High_plateau

Group: AirborneWindEnergy Message: 3303 From: Pierre Benhaiem Date: 4/8/2011
Subject: Re: Makani M1

It is told on Makani website that M1 operates between 200 m and 400 m altitude.Span is 35 m;so the swept area could be 18133.5 m².So with a wind speed of 9 m/s (to obtain the theoretical 1 MW) the power at 100 % Betz limit could be 4700203.2 W. If we do not take into account the (big) other losses the obtained power is about 21 % Betz limit.

Four remarks:

1) The center of the loop is not swept.

2) Knowledge of the output in rapport to Betz limit is yet useful for the knowledge of swept area then space occupation (surface and volume).

3) It is not sure that here the swept area is optimal (perhaps too high for M1 potential,that could explain the low value of % Betz limit, or  for other considerations like a necessary high value of radius of loop because of high kite speed ).Diehl's formula does not take into account Betz limit because it does not take into account the swept area,but it would be possible to make a translation to obtain a rapport between (kite area and kite ratio CL/CD)/(swept area).I think KiteGen already made this calculation.

4) With a less performant flygen (per m² of kite area) like FlygenKite the swept area will be very different than for M1. FlygenKite flying slower the radius can be reduced:it could be a good point to reduce space occupation (this point should be clarified). 

Doug,DaveS and me are right about the necessary limits of speed because of the too high tip speed of the rotor.

PierreB,

http://flygenkite.com  

Group: AirborneWindEnergy Message: 3304 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
Theo,

I would take your Betz limit admonition one step further.

Since our raw source of fuel for AWE is free, considerations as they pertain to "efficiency" can be more or less simply quantified as to whether "Return on Investment" (ROI) and "Cost of Power" (COP) are good enough to warrant competitive energy offerings to the market place, and attract investment. One could conceivably design a system that is only 5% efficient in a "Betz sort of way", and still be successful.

That said, I would further comment that on this forum, there is a huge amount of BS being thrown about regarding the meaning and calculation of so called "Betz limits" (a term that has become used in this forum as virtually a generalized concept applying to everything). I would say that anyone who would contend to understand and speak knowledgeably about such limits on these complex designs should first go through the math and understand how the Betz limit was derived for the simple windmill type system......then before blithely applying it to everything and declaring such things as "double and triple Betz penalties" , should try to derive what a "Betz limit" might look like for the system in question. This will quickly give you a knew appreciation for that of which you speak!

DaveL


At 10:26 AM +0200 4/8/11, Theo Schmidt wrote:
Group: AirborneWindEnergy Message: 3305 From: Pierre BENHAIEM Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
Dave Lang wrote:"...declaring such things as "double and triple Betz penalties"..."
In precedent posts"Double Betz penalties" or similar is an expression for flygen where Betz limit concerns both the rotor aloft and the whole area swept by the kite.It is true that the term "penalty" has a pejorative sense.The "penalty" is not so easy to appreciate:in the case of no regulations,no FAA,no aerial constraints,Betz limit within swept area is not so important.But now our aerial space is limited.

PierreB




Group: AirborneWindEnergy Message: 3306 From: dave santos Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
To Dave Lang,
 
It would help to explain why the Betz Limit based on a rotor solid-disc assumption does not apply in a loose general sense to other shapes like a hollow ring or frontal rectangle. I have seen the Betz Limit principle used in this general sense by leading authors struggling to characterize the limits of non-disc windfarm geometries & it makes considerable sense in those contexts. No one proposed a triple penalty, but you could opine as to whether a small turbine disc on a wing inscribing a larger disc is in fact a Betz "double hit".
 
Betz efficiency is a rough indication of the far more meaningful AWE limitation of Surface Sprawl. The Makani M1 will be severely limited in economic efficiency by the excessive requirement for ground interconnect infrastructure (roads, fences, buried cables, no-go zones, etc.). Despite a big sky, highest airspace utilization is very desirable,
 
daveS
 
 
Group: AirborneWindEnergy Message: 3307 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
I was only alluding to two things....

1. The (conceptually and quantitatively) shaky ground associated with "shooting from the hip" as regards to efficiency of AWE schemes, and the implications thereof.

2. That ROI and COP trumps ALL the details and implications that might be thrown in the mix, such as efficient use of airspace, etc, etc....all of which will show up in the ROI and COP if done rigorously (could one even design an AWE farm without addressing this issue?). These conjectures will ALL "washout to fact" when you do your solid simulations/testing and begin to approach a final design of something that actually works and has potential attraction to investors!

Makani's M1 may have an efficiency of 1% for all I know, but who knows (although Makani may well) until one does the simulations and testing and evaluates TOTAL COST (to determine ROI and COP). I would not sell any AWE scheme short based on a "half-baked assessment of how many Betz limits" they are suffering from...what I am driving at is do the math folks (right).....do the sims....do the tests.

DaveL





At 11:27 AM -0700 4/8/11, dave santos wrote:
Group: AirborneWindEnergy Message: 3308 From: Pierre Benhaiem Date: 4/8/2011
Subject: Re: Makani M1
Correction:"18133.5 m²"; a little less because of vertical projection
of the wing.

Note:you put a small turbine with a generator at the tip of each blade
of a conventional wind turbine.Betz limit concerns the whole
conventional wind turbine,but also concerns each small turbine in
rapport to apparent wind:Betz limit within Betz limit.

It is the same thing for AWECS of type flygen (another thing:it is
interesting that a rotor aloft with a low output produces also a low
drag (it is a point for examen)).Losses due to the rotor aloft (which
Betz limit of the rotor aloft) are the price of the conversion,a little
like losses due to reel-in phase for an AWECS of type reel-in-out.

Other example:an existing huge wind turbine sweeps about 12000 m²:%
output within Betz limit gives a main data for the global power. KiteGen
carousel sweeps about 2 km² and more: % output within Betz limit
gives a main data for the global power.

PierreB

--- In AirborneWindEnergy@yahoogroups.com, "Pierre Benhaiem"
<pierre.benhaiem@... a
%
volume).
high
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because
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35
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Betz
93
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http://www.energykitesystems.net/OrthoKiteBunch/OptimizationOfAManualFly\
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Group: AirborneWindEnergy Message: 3309 From: North, David D. (LARC-E402) Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]

I agree with Dave Lang. The Betz limit sort of loses its relevance with most AWE configurations (flygen or groundgen). Betz developed this law to describe the theoretical maximum amount of energy that could be extracted from a full stream tube of fluid passing within the outer tip diameter of a turbine relative to the total energy passing through it.

 

I suppose you could look at each turbine on a flygen separately and try to estimate the energy in the complex, helical stream tube that passes through each turbine on the flygen, but it seems like it would be very difficult (although not impossible) to model. Using the Betz limit calc with knockdown factors, or “double Betz” is probably an oversimplification of the problem.

 

So again, I agree with Dave L. Build the simulations as best you can (hand calcs all the way up to CFD). Build the test articles. Get data. Recalibrate models (or throw them out and use empirical performance curves from the data). Rinse and repeat.

 

Efficiency does matter (e.g. high L/D, low drag tethers, super efficient turbines/generators, light weight/strong materials, etc.) but In the end ROI (which involves much more than efficiency) will probably be the only figure of merit that matters. The teams that can field marketable systems with decent ROI (better than fossil fuels) will be successful and profit. This is why I was musing before about the really low efficiency Chinese drag system before (don’t slam me Doug S. !). I’m not a big fan of these low efficiency drag systems, but their R&D, DDT&E and materials costs are probably much lower than everybody else’s. And they’ve certainly got low labor costs for sewing enormous square meters of low cost fabric drag buckets.

 

I think the winning AWE solution may be somewhere in the middle between the high-tech (high cost, high efficiency, high performance, composite construction, complex electronic autonomous controls) and the low-tech (low cost ,fabric construction, low L/D, , large(r) surface area, simple (semi-passive?) controls). Kind of hard to visualize something in between the two that combines the best features of both.

 

Kind of got off track from the Betz discussion! But anyhow.

 

Dave North

 

Disclaimer:
The views and opinions expressed herein are my own and do not necessarily state or reflect those of NASA or the United States Government, nor do they represent the official position of NASA.

 

Group: AirborneWindEnergy Message: 3310 From: Doug Date: 4/8/2011
Subject: Re: High Plateaus of the World
Simon:
Oak Hills, California is the gateway to the high desert.
It's a plateau of sorts too.
We get very strong winds here that are funneled through the Cajon Pass.

If you take the 15 Freeway from L.A. to Las Vegas, you'll go by Oak Hills. Oak Hill Road is the first exit at the top of the pass, at 4200 feet elevation. We're a couple miles in at 3600 feet. The desert here looks level, with lots of mountains and lakes surrounding, but a closer look reveals long, flat, gentle slopes.
Anyway, it's like living in the sky.

All you know about Southern California - the perfect weather & the smog, both held in by a wall of mountains - well, beyond that wall of mountains is where we are at.
We had snow last night. Skiing is less than 1/2 hour away and you can see the slopes from here. It's like a piece of Nebraska slapped onto the Golden State. Well except for the skiing. Freezing all winter, then sometime soon it will quickly transition to 120 degree days.

I've been watching the output readings on the inverter for the 10 kW turbine on a 120-foot tower here, making 10, 11, 12 kW and more, just last night. It's making around 6 kW now.

The wind here blows almost all the time and you are already at 3600 feet. So that saves 3600 feet of kite line and all you need are a couple hundred feet to be way way up in the sky!

The edge of the pass is like a "skyscraper" - we look over at storm clouds and fog, all day, every day - just a few miles away, yet the weather seldom makes it here, but instead dissipates before it can get quite to here.

Ya know - clouds form then dissapate without moving though in a stream of fast-moving air. I'm sure you've seen the time-lapse videos of clouds staying in the same place all day while obviously there's a 60 mph wind trying to blow them along...

We watch clouds go by at or just above ground level, like you watch cars go by on the freeway - very fast.

I've got 20 acres with a lot of other clear land around my yard too.
If anyone wants to come here and fly your rig, all are welcome and you can stay here at no charge. Also there are some nice new major hotels within 2 miles.

While I might over-dramatize and complain about the weather a bit, it's closer to home and probably much nicer than the Tibetan Plateau.

We've had a few nice days lately, til global cooling reared its ugly head once again. S'posed to be nice again next week.
Also I'll bet they don't have a Super-Target or an In-And-Out Burger nearby in Tibet.

Maboomba!
Doug Selsam
http://www.selsam.com
Group: AirborneWindEnergy Message: 3311 From: Dave Lang Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
Thanks for the comments DaveN.

Even the Betz limit for the highly idealized stream-tube model has been re-visited with more sophisticated analyses and realistic CFD models and it has been conjectured that for the assumed Betz-model, a more accurate power conversion limit could be as low as 30% efficiency (rather that the oft-quoted 60%)....this is due to flow escaping/diverting around the (idealized stream-tube) rotor geometry (not included in Betz' very elegant but somewhat over-simplified model) and thus avoiding getting robbed of its kinetic energy (thus the loss of efficiency).

If one wants a challenge to stretch their AWE analytical wings, a good exercise is to try to figure out what an equivalent Betz limit would be for a close-hauled sail boat (a sailboat on a full downwind leg is pretty simple to do)....many surprises await, even to the point of having to examine what one means by (the blurry definition of) efficiency - it is the prime baseline ingredient if one wants to express power conversion as a ratio of two quantities :-)?

DaveL



At 2:54 PM -0500 4/8/11, North, David D. (LARC-E402) wrote:
Group: AirborneWindEnergy Message: 3312 From: Pierre BENHAIEM Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
Thanks for the comments DaveN and DaveL.They open my eyes about CFD models and the probably great difficulties to obtain realistic simulations of AWE.

PierreB 




Group: AirborneWindEnergy Message: 3313 From: dave santos Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
I also agree with DaveL that ROI rules but there are so many critical dimensions to a real AWE system that elevating any isolated factor (like Betz performance) above the rest  is a distortion. The double-Betz-hit conjecture is still an interesting question, but in the abstract.
 
A personal beef is how often someone gushes about wind power increasing at the cube of velocity, which is true, but then they presume that they will effectively harvest all this increased power, which is not true. For a variety of reasons, including the  runaway capital cost of chasing top performance, its far safer to estimate one can harvest the increase at the square of velocity. This rule-of-thumb, while incorrect text-book physics, is a properly pessimistic design assumption.
 
DaveN is probably right that the winning early AWE formula will be the sum of many middle-of-the-road trade-offs, a balance of performance & cost. Still, the solution may also involve some very clever inventive leaps unforseeable by any conservative design strategy.
 
 
 
Group: AirborneWindEnergy Message: 3314 From: Bob Stuart Date: 4/8/2011
Subject: Re: Betz limit [was: Re: [AWECS] Re: Makani M1]
I've read comments elsewhere by guys who feel challenged by the Betz limit and want to beat it.  This misses the point on two counts.  One, is that there are seldom any hard physical limits on the section of air available.  The other, more fundamental misunderstanding is that this is not like the problem of increasing efficiency in heat engines, where the limits are not fixed, but subject to improvements in design and materials.  Betz simply warns us about being too greedy, and reducing the flow through our device below the optimum level.

Bob Stuart

On 8-Apr-11, at 5:45 PM, dave santos wrote:


Group: AirborneWindEnergy Message: 3315 From: simon_0987 Date: 4/9/2011
Subject: Re: High Plateaus of the World
Thanks for the invitation :)

It'll be a couple of years before I start testing. When I come to the US, I'll be sure to stop by.

I am actually quite regularly in China ;) , and I would've liked to test there (many plateaus, strong winds over the entire country, sunny, nice food), but I am assuming the government is very restrictive in its control over the airspace.

When I start to test, I will probably contact the aviation authorities of a couple of countries to ask if I can test in the (international) waters off the coast, as I think it will be very difficult to get permission to do the kind of long term (months) testing I would like to do over land.


I started this topic because I noticed no one was talking about this. I still don't know how a plateau/mountain changes the wind over it, but if it doesn't change it much (above the planetary boundary layer), you could set up a test site on the slopes of Mount Everest, for example, at an elevation of 8000 meters, and do your experiment.

If that's too extreme, there might be smaller plateaus/settlements at an elevation of 6000-8000 meters, in China or the other countries surrounding the Himalayas, or the Andes, or somewhere near you.

http://en.wikipedia.org/wiki/List_of_mountain_ranges

http://en.wikipedia.org/wiki/Category:Plateaus
Group: AirborneWindEnergy Message: 3316 From: dave santos Date: 4/9/2011
Subject: Re: High Plateaus of the World
Simon,
 
Many of your questions are covered in the thousands of previous messages on this forum, if not under current discussion. Its a lot of homework, but worthwile to anyone who wants to excell at AWE.
 
The High Plateau/High Altitude R&D question breaks down like this-
 
What are the populations one seeks to serve? Every plateau you mentioned is remote, underpopulated, with no real industry. At most you would serve scattered small native populations with small scale systems. These large high plateaus tend to block or steer a lot of wind around their flanks. The wind that does jump the lip will tend to have large gravity waves for a pattern of gales & lulls. A pinnacle of comparable height is favored. Developing AWE at high altitude thin air can either be an incredible challenge building excellence, or a deep liability contributing to program failure. Places like Everest do not even have a road infrastructure. R&D done by sherpa transport will be fabulously expensive & slow.
 
The AWE field is now incredibly competative, with quite a few savants active. If one is not already hopping out of bed in the morning to do tests, they are falling behind. The sky is a harsh mistress & punishes those who over-reach. Mastering one's art at low altitudes is an essential prelude to mastering high altitude. After all, what vital hypothesis being tested by a high-altitude experiment that science cannot already answer? The key to high altitude is operational excellence based on experience, rather than a missing science experiment.
 
Mastering aviation culture opens up access to the sky. Most energy markets & populations exist in shared airspace. Those who fail to become airworthy in this environment will be grounded, locked out of the main action, a despised menace to aviation. Avoiding aviation regs by fleeing to remote places also cripples R&D if all the aerospace brains are back in civilization. Remote R&D becomes an excercise in long supply lines rather than acculturation to shared airspace. Any great AWE concept that will work at high altitude will also work lower. First-to-market will start low at a modest scale & eat the rest alive. The eventual high-altitude winners will be the toughest survivors of a race where vanity & hubris weeded out the weak.
 
So if you don't get around to wading thru all the old messages, this was a taste of the debates bearing on your issues. Don't be discouraged by the challenges. A good first step is to explain your technical concept as a "theory of operation" so that others can understand what you are attempting & contribute,
 
daveS
 
 
Group: AirborneWindEnergy Message: 3317 From: Pierre BENHAIEM Date: 4/9/2011
Subject: Re: Makani M1
Attachments :
    Interesting paper:reading p.6 and 7 about tether-3 wires:"

    Consider a realistic example of what one might try to build, a 100 kW wind generator with

    a tether length of 1500 feet (circa 450 metres) running 3-phase output at one of 380, 480, or 600

    VAC. The corresponding phase currents at full power and full voltage into a resistive load are

    88.6, 70.2, and 56.1 amperes respectively. In turn, the minimum required cable gauges are 3, 4,

    and 6 AWG respectively, and greater if the reactance of the load cannot be guaranteed to stay

    low. Even with a three-wire delta with no additional grounding lead, the weight of the copper

    alone is 325, 257, or 162 kg for the 1500 ft run. The ohmic losses in the tether at full current are 7

    kW, 5.5 kW, and 5.6 kW respectively, or 5.5 to 7 percent of total production over 1500 ft."

    So for 1MW the weight of the copper alone (waiting for nanotube?) is from 1620 to 3250 kg with a tether length of 450 m.In static use M1 (hypothetical 175 m² and wind = 9 m/s) could lift only 850 kg,FlygenKite (700 m²) could lift 3400 kg (it is not yet enough).What are the repercussions about safety and reliability if lifting tether is only possible during dynamic use?

    After discussions about "to Betz or not to Betz" limit(s),to consider that rough calculations I take is for a very (too) favorable hypothesis,and already requirements seem to be very difficult to satisfy.

    PierreB
    http://flygenkite.com  






      @@attachment@@
    Group: AirborneWindEnergy Message: 3318 From: simon_0987 Date: 4/9/2011
    Subject: Re: High Plateaus of the World
    Thanks for your explanation Dave.

    Actually, the thing I'm working on does allow itself to be tested in lower altitudes, so I will do that first. I'm just thinking about the steps after that.

    Unfortunately I can't say more on what precisely I'm working on. I'm not even convinced it can compete with what other players are developing now.
    Group: AirborneWindEnergy Message: 3319 From: Joe Faust Date: 4/9/2011
    Subject: Re: AWEA conference wants diversity without AWE, apparently ...

    Success. AWE will have an official media press pass at a conventional windpower big conference!   Following three approaches including a helpful bacing letter from AWEIA president prot-tem John Oyebanji, a press-pass first denied twice has been approved:

    Group: AirborneWindEnergy Message: 3320 From: Joe Faust Date: 4/9/2011
    Subject: Re: AWEA conference wants diversity without AWE, apparently ...

    Prior post: program rewrote a redirected link. Here is the absolute URL:

    http://energykitesystems.net/UpperWindpower/index.html

     

    Group: AirborneWindEnergy Message: 3321 From: Theo Schmidt Date: 4/10/2011
    Subject: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]
    Pierre BENHAIEM schrieb:
    ...
    ...
    ...

    I would think that this much copper or whatever is suboptimal. Using
    high-voltage DC might be better if the inverter aloft doesn't weigh too much.
    Then one could use two wires and many kilovolts, saving a lot of material and
    weight in the lines. Of course one also needs a sure method of shorting this out
    in case of accidents. And remember that insulation weighs, too. An interesting
    optimisation problem which I'm sure has been done.

    Theo Schmidt
    Group: AirborneWindEnergy Message: 3322 From: Bob Stuart Date: 4/10/2011
    Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]

    On 10-Apr-11, at 1:58 AM, Theo Schmidt wrote:

    I wondered about using aluminum conductors, but was recently informed on this list that for a combination of conductivity and tether strength, steel is better.  If necessary, considerable line losses can be tolerated.  It may be possible to use a capacitor to use high-frequency AC with only a single conductor, saving the weight of insulation.  

    Bob

    Group: AirborneWindEnergy Message: 3323 From: Joe Faust Date: 4/10/2011
    Subject: What? What could be conducted via tethers?

    Our group has mostly a focus on conducting macro mechanical force or electricity through a KES tether set. 

    What else could be conducted through KES tethers? 
    (Leave development and comparisons to another thread, perhaps.)

    1. Macro mechanical force of the tether (left-right or more generall radial positions of a tether in the imaginary sphere of flight; here the tether is as a lever or a tensed pusher or puller without reel-in or reel-out). Shafts or levers may be operated here. 

    2. Macro mechanical force of the tether via tension for traction or pull/relax for reel-in-reel-out purposes. Here we get power kiting, SkySails, groundgens, play-arm-moving, etc.

    3. High-frequency vibrations of the tether could be mined for signals, communications, state reporting, and even making electricity or heat or pumping, though some uses here won't compete well against other tether uses.

    4. Tethers may be constructed to conduct electricity directly. This might be a single conductor as part of a macro circuit between sky and ground.   Also, a two-wire flygen circuit. Or three-wire. Add the insulation matter discussed.
    5. Gas-conducting tethers have been around for centuries. The purpose of the gas is varied. One of the first uses of gases in a tether was to supply the LTA gas for for large balloons.  Recharging kytoons from grounded gas generators has been described.    However, making gases aloft and sending the product to ground has also been described.

    6. With energy from a working kite aloft, modify chemicals to store electricity; then conduct that reformed chemical to the ground via the tether. Send up one chemical and return the modified chemical; chemical up-and-down tech. Of course, one such player is the charging of chemical-based electrical batteries.

    7. Light. A tether may be dedicated to conducting light or laser.

    8.  Path.  A tether may act as a raw road for climbing and falling. Climbers and returners may be people, animals, carts, cable cars, objects of most any description.  The skyhook may be doing other things even while the tether might be used as a simple roadway. Walk up a tether set. Drive your Ford or Toyota up a tether-way. Let monkeys run up a tether for fun or to fetch things from the aloft living quarters.  Sail messages and toys or supply for the aloft KES human operator (food, medicine, clean clothes, hearing-aid replacement battery, etc.)

    9.  A  kite tether (KT) may conduct one's spirit or inspiration to and from the heavens, may conduct joy or redemptive messages materially or vicariously.

    10. Water conduit. Transport water up or down or up and down a tether for various purposes.

    11. Loop-pulley fan-belt drive transmission of force: Have the tether be a closed loop driven from above to drive a rotating shaft below. Or trade the prime mover for some operation where the ground input is the driver.

    [Open for comprehensive description of what might be conducted by tether sets of  AWECS ro KES] 

    12. ____________________________

    ...

    n#. ____________________________

    What could a tether conduct?

    Group: AirborneWindEnergy Message: 3324 From: Joe Faust Date: 4/10/2011
    Subject: Re: What? What could be conducted via tethers?
    SpiralAirfoil reminded me of what has been covered in our list messages,
    so we add now such to the list.

    ##: Rotating tethers: stiff torque cables, torque-tube as tether,
    unshrouded or shrouded torque tethers, etc. We have at least three
    companies working on this direction. The aloft works drive a rotation
    of the tether about its longitudinal axis. This is the twist/torque
    method of conducting force. Challenges aside, this mode of conducting
    force belongs in the party. In our video set there is shown a working
    system using a flexible cable drive a ground genertor. Another example
    is featured in a photo on our Stakeholders page. Niche uses?

    Other?

    JoeF
    Group: AirborneWindEnergy Message: 3325 From: Robert Copcutt Date: 4/10/2011
    Subject: Automation of AWE
    For those worried about the feasibility of automating AWE systems have a
    look at this video
    http://www.youtube.com/watch?v=3CR5y8qZf0Y

    Quoted from the explanation,
    "This is not human-piloted (please see the overview vid). The
    vehicles/ball are tracked by an overhead motion capture system and
    controlled by a pair of computers."

    overview vid = http://www.youtube.com/watch?v=pcgvWhu8Arc&NR=1

    Once the software to control the flying generators is developed the cost
    of deploying it to other AWE systems will plummet. This is where the
    strength of open-source should come into play, just as the hugely
    complex system that is modern linux has cut the cost of legal computing.

    Robert.
    Group: AirborneWindEnergy Message: 3326 From: Robert Copcutt Date: 4/10/2011
    Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]
    On Sun, 2011-04-10 at 07:26 -0600, Bob Stuart wrote:
    Yes, that was me. The spreadsheet showing the calculations is still
    there. I promised to update it and post an excel version but have been
    too busy with other things to get it done yet. Hopefully soon.

    HF AC down a single line would be inefficient. The way to go is 2 lines
    carrying single phase AC, or preferably DC. Single phase generators tend
    to vibrate too much so 3 phase is better. It only needs a simple
    rectifier to convert to DC and a multi-kilovolt version would weigh very
    little. Inverters are for going the other way.

    Using 2 wires has an important safety benefit because if one breaks the
    other can still be used to pull the airborne generator back to a safe
    place. There is no need to insulate these lines and in fact the
    insulation would just get in the way.

    Something that no one else seems to be considering is using a
    combination of airborne and ground-based generators. The airborne
    generators/motors only need to be powerful enough to get the wing off
    the ground and into the wind. Any more powerful than that and their
    mass, and the mass of the tethers, start to become a problem. The main
    generator will be on the ground driven by the reeling out of the twin
    tethers.

    Another reason for restricting the power of the airborne electrics is
    the tip speed of the blades - as recently discussed by Pierre et al.
    Noise from the blade tips rapidly increases as their speed increases
    (5th to 6th power) so to be a good neighbour the blade rotation rate
    needs to be kept down.

    Quadracopters can be controlled very precisely. Putting more than 4
    generators on a wing would be extravagant. Less than 4 makes control
    difficult.

    Robert.
    Group: AirborneWindEnergy Message: 3327 From: Pierre BENHAIEM Date: 4/10/2011
    Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]
    "Consider a realistic example of what one might try to build, a 100 kW
    Group: AirborneWindEnergy Message: 3328 From: Robert Copcutt Date: 4/10/2011
    Subject: Re: best voltage [was: Re: [AWECS] Makani M1 [1 Attachment]]
    We need to be careful with the rather misleading terminology here.
    "Brushless DC" refers to the whole package including the electronics.
    The motor/generator itself will be 3 phase AC.

    Robert.


    Group: AirborneWindEnergy Message: 3329 From: dave santos Date: 4/10/2011
    Subject: Re: Automation of AWE
    Roger,
     
    No one we know doubts AWE automation will eventually succeed. The debate is over how soon it can earn airworthiness certification, with estimates ranging from 2011, in venture hype, to 2025 & beyond, by career aerospace veterans. The "(worry) about the feasibility of automating AWE" is not based on ignorance of the amazing stunts automation is capable of, but based on the knowledge that such lab rats are not realistic models for full AWE automation.
     
    The neat quadrocopter ping-pong featured clearly won't meet aviation standards for reliability. To their credit, the researchers show a (totally predictable) failure. The lab is a highly structured environment, an essential prerequisite for current automation. The same experiment outdoors, in all lighting & weather, with high-hours, & ordinary windfield chaos, would fail far more. Add tether dynamics as a chaos generator & the multiple chaos sources mean formal hyperchaos. No current example of automation handles hyperchaos. The few simple chaotic controllers that have been developed are not very robust theoretical exercises. Human expert kite-pilots do handle hyperchaos rather well, but after years of practice & they cannot verbally formalize control laws developed as "muscle memory". These were my findings to KiteShip in 2007 & nothing since calls this picture into question.
     
    First-to-market utility-scale AWE will likely be based on supervised automation with a legally required pilot-in-command (PIC) & visual observer (VO) to provide situational judgment & "make saves". Is worth noting that hobby kites do in fact rival the 98.5% availability of wind towers
     
    daveS
     
     
    Group: AirborneWindEnergy Message: 3330 From: simon_0987 Date: 4/10/2011
    Subject: Re: Automation of AWE
    Group: AirborneWindEnergy Message: 3331 From: Robert Copcutt Date: 4/10/2011
    Subject: Re: Automation of AWE
    Dave,

    You got my name wrong which hints that you think I was criticising you.
    That is not the case. Doug made a good point in his post about the space
    tethers saying that it is a popular subject because no one can point a
    finger and say, "why didn't you build it?".

    Fear of failure can be a huge barrier. The rewards for getting AWE
    commercial could be enormous. People are already saying, "if it so good
    why can't we buy one already?".

    I am not sure the level of airworthiness required for passenger carrying
    aircraft will ever be required for AWE. Turbines are already being
    installed offshore. That is a good place for AWE too. No problems with
    fires from burning generators crashing to the ground. Fewer problems
    from the sonic booms when the blade tips exceed the speed of sound and
    more likelihood of getting permission to fly high.

    Google have demonstrated technology that can drive a car better than a
    human. Moore's law is still working and computing power per unit cost is
    still doubling in less than 2 years. Given good software a modern
    standard laptop PC probably already has the power to fly a set of kites
    better than a well trained human.

    The proposal I announced recently talks of starting with a small kite
    flown manually. The plan is automate it step by step. Skysails already
    have their ship hauling kites fully automated. Maybe they will licence
    others to use their software.

    Robert.


    Group: AirborneWindEnergy Message: 3332 From: dave santos Date: 4/10/2011
    Subject: Re: Automation of AWE
    Robert,
     
    Sorry for the "Roger" typo, but i felt no implied criticism from you, nor see how your widely-shared opinion of flight automation could be so badly misconstrued. We both admire the quadrocopter feat, but the logic seems weak that the popularity of the Space Elevator concept is mostly based on current impracticality, not its coolness. Many things, (like, say, chocolate) are far more popular yet practical.  Doug does not account that autonomous AWE is far closer to operational status than a space elevator.
     
    You are correct that the power of a desktop computer in principle should be able to perform adequate flight automation. What folks don't understand about Moore's Law is that it has little bearing on our ability to architect complex software, which advances far slower. This is why our computers still crash & we don't have a HAL9000 artificial intelligence, despite so much available computing power. Similarly, try to find any realistic example of flight automation comparable to the hyped AWE claims that 7/24/365 operation of jumbo aerobatic E-VTOL is near, most especially in a remote, dangerous, hostile (saline), superdynamic marine environment. Formal validation of airworthy "clean-room" software is just one example of the sort of formidable challenges to fill the years that the AWE aerospace vets predict required. Note that Skysails' AWECS is far from "fully automated"; it takes an expert ship crew to judge weather, traffic, & exceptions. Skysails is precisely the sort of supervised partly-automated system folks like me consistently advocate. Its pretty much like the autopilot of an ordinary aircraft: No substitute for a pilot. Software like Skysails' does not find easy reuse outside of its narrow domain. Generally we must rewrite software from scratch until the field matures.
     
    Note that a roughly* comparable standard of airworthyness is demanded of non-passenger transport, to protect populations on the ground & pilots. This is not just a regulatory barrier, no aviation insurer is ready to offer liability coverage for autonomous large aircaft. Imperfect automation quickly destroys the capital "hull" investment as well. Your idea of automating by small steps, starting by small kites, is what everyone working in AWE is already doing. A clear difference in pioneering approach is those AWE systems with inherent flight stability that do not even require manual control, like the classic single-line kite, a marvel of paleo-automation,
     
    Roger ;^)
     
     
     
    * There are in fact passenger related regs, but basic airworthiness is universal to all aircraft & regulated more by gross weight & airspeed.
     

    Group: AirborneWindEnergy Message: 3333 From: Bob Stuart Date: 4/10/2011
    Subject: Re: Automation of AWE
    Someone looking for a location for experimenting might consider Mohave, California.  It is a favourite location for homebuilt aircraft experimentation, so there is tech help around, the air space has minimum restrictions, and the wind is very impressive.

    Bob Stuart

    On 10-Apr-11, at 9:15 PM, dave santos wrote:


    Group: AirborneWindEnergy Message: 3334 From: christopher carlin Date: 4/11/2011
    Subject: Re: Automation of AWE
    As I suggested to our friend from NASA Langley that's where NASA Dryden Flight Research Center is. If you get them interested they can work the airspace problem and work with you in many other ways.


    Regards,

    Chris
    On Apr 11, 2011, at 5:52 AM, Bob Stuart wrote:


    Group: AirborneWindEnergy Message: 3335 From: Robert Copcutt Date: 4/11/2011
    Subject: Re: Automation of AWE
    Dave,

    This business of fear of failure is subtle and deep-rooted. I have been
    studying the mindset of self-made millionaires and looking back on their
    lives it is not easy to see what risks they took. It is easy to be wise
    in retrospect, but before you know the outcome it takes considerable
    courage to invest your time and money in projects your friends are
    laughing at (or simply ignoring). Many are still laughing at AWE and
    nearly everyone else is ignoring it. I still have a sneaking suspicion
    you are using this issue of airworthiness of kites as an excuse to hold
    back.

    We are agreed that developing the software is likely to be the biggest
    job getting AWE automated. However, I thought that was the objective of
    this list - to get a team together to do some open-source development.
    The hardware needs to be developed in places where the manpower, and
    physical resources and money are locally available. However, the
    software can be done anywhere by motivated individuals with computers.
    They could submit their code for testing on real systems and then modify
    it based on the results of real tests. I have discovered 2 other
    enthusiasts here in Cambridge who share my interest in building real
    kites. Are there any programmers on this list interested to contribute
    to the software for it? Are Skysails interested to get involved in an
    open-source software development?

    I do have experience of writing control software and fully appreciate
    how long it takes. My one colleague is a professional in the field of
    computer vision and the other has connections with Kitegen.

    Linux is a success because it is a world-wide effort. The software for
    AWE is a project of similar magnitude and probably even greater value.
    Is it going to be seeded here or elsewhere?

    Robert.


    Group: AirborneWindEnergy Message: 3336 From: Joe Faust Date: 4/11/2011
    Subject: Retail product from Pacific Power Sails

    Retail product from Pacific Power Sails

    Neutral-news instance report:
    Note: lifter and personal power station are extra.
    Generators are kite lifted. Lifter pilot kite trained above the generator-holding kite is a recommendation by the company. Shown seems to be two turbines held in framework in front of the kite's sail.

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

    Product is up for retail sale:

    PacificPowerSail

    100 w at 25 mph wind.

    Discuss:

     

    Group: AirborneWindEnergy Message: 3337 From: Dave Lang Date: 4/11/2011
    Subject: Re: Automation of AWE
    Robert,

    DaveL here (as opposed to DaveS, or DaveN who also inhabit this list :-)),

    It is one thing to develop software, and entirely another to develop h/w.  Open Source software can be developed by reclusive nerds (no pejorative meaning intended -  I likely fit the category) living in their parent's basement, and eating cereal bars, all at the cost of only a cheap computer and their personal TIME.

    On the other hand, H/W, which is what is needed to convincingly demonstrate feasibility and operation, requires: (1) a Central facility, (2) Dedicated folks who inhabit same (ie h/w construction can't effectively be distributed around the world in bits and pieces of "open-source endeavor"), (3) and $$$!  I know that the scheme I am working on (SkyMill) has a firm enough conceptual development at this point to to able to construct and fly a series of progressively larger prototypes that could show  conclusively that it would practical (at some scale) or not.

    I (and my cohorts) have spent enough of our personal time and money on this thing to not be accused of harboring and courting imagined barriers such as (airspace) to avoid being held to the test of ultimate reality and fear of failure - indeed we continue in the face of ongoing and  incessant failure to convince money-folks to smile upon us, sustained by nothing but faith in our concept (maybe ill-founded, who knows for sure).....Just bring us money and we will fly (for better or for worse); I personally would like to put this thing to rest (one way or the other) and get on with my life!

    DaveL




    At 5:20 PM +0100 4/11/11, Robert Copcutt wrote:
    Group: AirborneWindEnergy Message: 3338 From: dave santos Date: 4/11/2011
    Subject: Re: Automation of AWE
    Robert,
     
    Never forget that the software-intensive high-risk high-complexity concepts have attracted over fifty million in R&D investment. Do not expect any small player with an skeptical opinion can negate that. Please do show us how tech failure is avoided, which is what i am also trying to do. Professional pessimism is not fatalism, but a basis for success in a high-risk endeavor. You may be so gifted as a control engineer that my cautions do not apply, so don't take them personally.
     
    Regarding what software to perfect first, my proposal has been to add a layer of minimalist trim-control to inherently stable kite flight for enhanced robustness, but software is not, in my opinion, the biggest priority, given great human pilots, but showing real large scale rigs at work in the sky is. Then the software architects will then know exactly whats worth automating. Sadly, many control engineers are being used to automate doomed platforms, a waste of software dev resources,
     
    daveS