Messages in AirborneWindEnergy group.                             AWES5808to5857 Page 14 of 440.

Group: AirborneWindEnergy Message: 5808 From: dave santos Date: 3/14/2012
Subject: Re: Forging ahead despite ignorance, lack of help

Group: AirborneWindEnergy Message: 5809 From: Phils Date: 3/14/2012
Subject: Re: Forging ahead despite ignorance, lack of help

Group: AirborneWindEnergy Message: 5810 From: dave santos Date: 3/14/2012
Subject: Altaeros seeks AE Intern for Windtunnel Studies

Group: AirborneWindEnergy Message: 5811 From: Joe Faust Date: 3/14/2012
Subject: #400

Group: AirborneWindEnergy Message: 5812 From: Joe Faust Date: 3/14/2012
Subject: Is there a mention in EnergyKiteSystems.net on ______ ?

Group: AirborneWindEnergy Message: 5813 From: Doug Date: 3/15/2012
Subject: Re: Forging ahead despite ignorance, lack of help

Group: AirborneWindEnergy Message: 5814 From: Joe Faust Date: 3/15/2012
Subject: Exploring carbon stiffening for the KiteGen kite?

Group: AirborneWindEnergy Message: 5815 From: blturner3 Date: 3/16/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?

Group: AirborneWindEnergy Message: 5816 From: dave santos Date: 3/16/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?

Group: AirborneWindEnergy Message: 5817 From: roderickjosephread Date: 3/16/2012
Subject: Re: Makani Seeks Two Engineers

Group: AirborneWindEnergy Message: 5818 From: dave santos Date: 3/16/2012
Subject: Kickstarter

Group: AirborneWindEnergy Message: 5819 From: harry valentine Date: 3/16/2012
Subject: Re: Kickstarter - AWE in Article

Group: AirborneWindEnergy Message: 5820 From: Robert Copcutt Date: 3/16/2012
Subject: Re: Makani Seeks Two Engineers

Group: AirborneWindEnergy Message: 5821 From: blturner3 Date: 3/17/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?

Group: AirborneWindEnergy Message: 5822 From: blturner3 Date: 3/17/2012
Subject: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5823 From: harry valentine Date: 3/17/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5824 From: Doug Date: 3/17/2012
Subject: Re: Makani Seeks Two Engineers

Group: AirborneWindEnergy Message: 5825 From: dave santos Date: 3/17/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5826 From: Joe Faust Date: 3/17/2012
Subject: "Gliding kite" (paraglider big) served 10 skydivers at once

Group: AirborneWindEnergy Message: 5827 From: dave santos Date: 3/17/2012
Subject: Correction and Addendum //Re: [AWES] Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5828 From: mmarchitti Date: 3/18/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5829 From: Robert Copcutt Date: 3/18/2012
Subject: NASA on kite physics

Group: AirborneWindEnergy Message: 5830 From: Doug Date: 3/19/2012
Subject: Re: Flygen vs Groundgen / squaregen vs roundgen

Group: AirborneWindEnergy Message: 5831 From: Joe Faust Date: 3/19/2012
Subject: Energy and signal in 1902 by Trainor

Group: AirborneWindEnergy Message: 5832 From: dave santos Date: 3/19/2012
Subject: Re: Energy and signal in 1902 by Trainor

Group: AirborneWindEnergy Message: 5833 From: blturner3 Date: 3/19/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5834 From: Pierre BENHAIEM Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5835 From: Doug Date: 3/20/2012
Subject: Re: Energy and signal in 1902 by Trainor

Group: AirborneWindEnergy Message: 5836 From: Doug Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5837 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5838 From: blturner3 Date: 3/20/2012
Subject: Re: Flygen vs Groundgen - wire weight

Group: AirborneWindEnergy Message: 5839 From: blturner3 Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5840 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen - wire weight

Group: AirborneWindEnergy Message: 5841 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5842 From: dave santos Date: 3/20/2012
Subject: Displacing fuel and slashing costs- Wind Powered Aviation

Group: AirborneWindEnergy Message: 5843 From: Joe Faust Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5844 From: Joe Faust Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5845 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5846 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5847 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Makani Seeks Two Engineers

Group: AirborneWindEnergy Message: 5848 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen - wire weight

Group: AirborneWindEnergy Message: 5849 From: Joe Faust Date: 3/21/2012
Subject: Startram

Group: AirborneWindEnergy Message: 5850 From: blturner3 Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5851 From: dave santos Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5852 From: Dave Lang Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5853 From: dave santos Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5854 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5855 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

Group: AirborneWindEnergy Message: 5856 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Startram

Group: AirborneWindEnergy Message: 5857 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen




Group: AirborneWindEnergy Message: 5808 From: dave santos Date: 3/14/2012
Subject: Re: Forging ahead despite ignorance, lack of help
Phil,
 
Nobody has solved hydrogen problems (explosivity with even small amounts of air contamination, highest leakage rate with ozone layer depletion, high chemical reactivity, etc). No one has solved LTA storm survival, except by a hangar or deflation requirement. No one has beaten the standard streamlined blimp design for general performance (static and dynamic Lift v. Drag) although some kytoons have desirable capability.
 
We also know how to keep kites up in calm by pumping the line, especially by phased circular or step-tow tugs, and we can land them reliably in no wind by reeling them in under control. LTA for holding up idle AWES equipment during calm periods does not contribute much value.
 
Of course hundreds of such issues were well explored in the prior 5000 Forum messages, not to mention Joe Faust's volumes of AWE content, but data-mining a mountain is not easy   :)
 
daveS
 
PS You have added a corollary observation to the LTA topic- that the cheapest maximal-volume round balloon is good enough for assisted launch in low wind, even if very unsuited for any high-wind role.  KiteLab has used single party balloons as the initial pilot-lift basis for staged launch of kite arrays: In principle no more LTA than that is really needed for vast kite farm operations.

 
    
Group: AirborneWindEnergy Message: 5809 From: Phils Date: 3/14/2012
Subject: Re: Forging ahead despite ignorance, lack of help
It's Ground already covered. Ok, I'll dabble in another direction. It's windy today here ,Think I'll go fly my kites 8)
Group: AirborneWindEnergy Message: 5810 From: dave santos Date: 3/14/2012
Subject: Altaeros seeks AE Intern for Windtunnel Studies
Given engineering trade-offs, LTA-based AWES is not easy to envision as a dominant AWES technology, but it will likely enjoy nice niche markets. Altaeros seeks an intern to conduct windtunnel studies (link below) of its ducted HAWT. How does one test long-tether flight interactions all over the kite window in a small tunnel? Does a small rigid model really predict the flight dynamics of a sagging soft envelope? What if the tunnel work and CFD, buy omitting such dimensions, agree on a critically misleading model?
 
The cool image looks like a real prototype in recent testing. This LTA concept must at some point compete against the "KiteLab Reference Model" of a COTS aerostat with a suspended caged COTS HAWT equipped with landing gear; to settle open questions of lowest capital and O&M costs; also ideal gas volumetrics, minimal leakage, best payload ratio, etc.. Altaeros is in the cat-seat to evaluate LTA AWES conceptual contenders by direct comparative testing, to act on such results first with minimal uncertainty, but the overwhelming psychological pressure will be to gamble all on The Tube, scaling it a bit larger* than what comparative concept testing would afford.
 
Altaeros intends large crosslinked array formations for utility-scale farm operations; an "MIT vote" for aerial latticework principles.
 
* looks identical at all scales in photos
Group: AirborneWindEnergy Message: 5811 From: Joe Faust Date: 3/14/2012
Subject: #400
[[All development teams are invited to send link to their sites, videos, and documents.  editor@upperwindpower.com   ]]

Our video collection just reached "400" in count.   There is matter in the 400th that may be discussed in group. 

UNLVEngineering-High Altitude Wind Turbine.mp4   
 Dan Byrd & Casey Griffith.     Advisor: Dr. Darrel Pepper
Group: AirborneWindEnergy Message: 5812 From: Joe Faust Date: 3/14/2012
Subject: Is there a mention in EnergyKiteSystems.net on ______ ?


Bookmark the page reached:

And then after one space put a keyword or special phrase (force phrase by enclosing in quotation marks, if wanted) in the page's top search-query field; click the search button.   Google will find choices for you.   If you do not find what you want, give me a notice for partnering with you on the search; we would like to cover AWES well.  Thanks.

JoeF


Group: AirborneWindEnergy Message: 5813 From: Doug Date: 3/15/2012
Subject: Re: Forging ahead despite ignorance, lack of help
Don't you have something a little better than blue tarps at the world kite museum? (affordable though...) We're not talking about lifting several tons here. I can take steps to make a lightweight generator. Often in wind energy you try to make certain components heavier, rather than lighter, on the principle of "The 3 Little Pigs" which is a scientific theory only taught at the highest levels of academia, but I think I have some room to lighten a generator significantly and it should last days, months or more.
What kite options do we have to lift something between, say 50 and 100 lbs, that will stay up when the wind gets a bit light? What about lifting say 20 or 30 lbs?
:)
Doug S.

Group: AirborneWindEnergy Message: 5814 From: Joe Faust Date: 3/15/2012
Subject: Exploring carbon stiffening for the KiteGen kite?
Group: AirborneWindEnergy Message: 5815 From: blturner3 Date: 3/16/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?
Now, thats what I'm talking about. IMHO, a simi-rigid wing is the way to go. Carbon fiber is not needed for the ribs as they are illustrating. The loads on the ribs are relatively small. What is still missing is a stiffening spar along the leading edge to push the wing from from a pure catenary to a straighter line. That would be a good place to use carbon fiber. This change would increase the ratio of swept area vs wetted surface. This is like the spar in the flexifoil kite.

Another optimization that I don't see is that the outboard ribs should not be placed straight front to back. The airflow in that region travels at an angle approaching the overall wing angle of attack. ... Wait, I just did the math on that. A 15:1 LD ratio is only about 4 degrees. Too small to see in that drawing. So maybe they are doing it. And actually 4 degrees could be too small to mess with. 7:1 is closer to 8 degrees and would be worth messing with.

I also don't see any attempt to deal with the differing pressures from the forward to the rearward parts of the airfoil. The only good idea I have seen for that is to use EPP foam to add stiffness. I think Dave Lang was working on that. It's kinda heavy and not perfect.

Brian

Group: AirborneWindEnergy Message: 5816 From: dave santos Date: 3/16/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?
The urgent problem KiteGen has is achieving reliable low-drag retraction by pulling in on one wing tip. This must work flawlessly thousands of times in a row, but they are likely currently unable to do more than a few cycles before fouling. Their hope seems to be that this new carbon skeleton kite will lay flat to retract more stably.
 
Any conventional power kite tends to roll and foul itself in the KiteGen retract mode, especially LEIs with a built-in C-arch geometry. Normal ram-air parafoils dragged sideways lose pressure in a messy way (squirting air laterally), which does not help with stability, and then they have to reinflate, which can easily hang-up. Valved parafoils might work OK, but you would still need the leading wingtip to be a flyable pod "aircraft" able to resist roll disturbance. Another limitation on the KiteGen retract mode is that multi-line bridles are not practical, so they are stuck with a two line C-Kite.
 
This is the sort problem high-dollar commercial ventures have a hard time publicly admitting, but they must privately warn investors, or face criminal legal jeopardy. This is why you have to sign NDAs with most "elite" VC's, ti hide weakness, not so much because they have a secret-sauce recipe to protect. Massimo claimed to have some eight or so launch and retract methods as "Plan Bs", but he is running thru them (the blowers were a bust, a quadrocopter test was rumored, and the ungainly stem may end up as the snout of a "White Elephant"). The gamble on early scale-up is bold, but very unforgiving.
 
A secondary goal of KiteGen's carbon battened kite is to get a thinner foil section for higher performance, but such performance makes control challenges even more acute. A spanwise carbon spar does not make for a better large kite due to cubic-mass scaling penalty. You get a wing like a hang-glider, but due to the added weight, and higher minimum speed, you have to claw harder in light air, on the edge of falling out of the sky, just to stay up. The 1970's Flexifoil has a leading edge spar, but it obviously never scaled, and is one of the hardest kites to fly ever sold. The lighter C-Kite can hold its own operationally, as well as being cheaper and more robust, so it has thrived more. The latest ram-air race kites are so hot, with more progress to come, that carbon-based contenders may never quite catch up.
 
Adding carbon weight and cost to a large AWE kite is easily self-defeating. Airbeams, and especially ram-air, are dominant structural principles by inherent advantages. One can add thin carbon whiskers to inflated structure, just as sled kites are made, and get "tensairity" synergism, but the small-whisker format represents the effective scaling ceiling. Battens are also an effective use of small spar structure, to damp out membrane flutter, and that is the function of the ribs in the KiteGen carbon kite concept. They may get in new trouble if the carbon kite glide speed exceeds the reel-in speed.
 
Note to Brian: AoA is not by itself much of a predictor. At very low Re a high AoA can even be the highest L/D. AoA varies all along a highly engineered wing due to changes in foil section and washout. Some foils even operate at essentially zero AoA by just a curved upper surface. Virtually all aircraft vary AoA in flight, using high AoA to develop max lift at higher drag or to slow down. The wing root chord is often used for AoA measurement, but this only weakly predicts overall L/D. An optimized wingtip often even has a decided negative AoA to help cancel the induced drag of excessive wingtip votex generation. 
    
Group: AirborneWindEnergy Message: 5817 From: roderickjosephread Date: 3/16/2012
Subject: Re: Makani Seeks Two Engineers
I'm going to stand by my kickstarter project funding idea.

Single projects such as one prototype, can have tiny funding requests. 
If you want to make a statement to google, use facebook to advertise it.
Heck why not apeal to facebook to fund it... they have servers to fuel, a visage to keep and a reputation for providing crowdsharing tech.  
We can come together as a crowd and make excellent solutions custom designed to specific environments.
Dave S recently offered to lift Doug Selsams' generators ... awesome If I can help too I'd love to. 

Lets pick a first target project in a set environment... 
Everyone who's up for providing some expertise SAY SO in the kickstarter fundraising video... 
Set a go price. 
Allow people, institutions, governments, whoever, to sponsor the venture to whatever value they feel.

are you up for it?

Your only paperwork is offerings and thanks to sponsors.
If somebody happens to want to offer $2billion for an IP protected system. Well that's fine for a single years work. As long as we're publicly making something awesome. We have already shared the crucial component ideas....

It can only help spread the idea we all believe in.

We don't have to over hype what it can do.... kinetic sculptures find funding... we can make beautiful art with electricity as a useful by-product.

I have been planning asking $2660.33 for my first flexi pipe mounted, tail lifted daisy structure.

Group: AirborneWindEnergy Message: 5818 From: dave santos Date: 3/16/2012
Subject: Kickstarter
Rod,
 
By all means do try the KickStarter/FaceBook paths, but don't ever give up on Google someday funding another grander round of R&D, on a broader better balanced basis. Its just that you seemed to imply Kickstarter was a way to forget Google, in responding to a "Makani Hiring" post with the Kickstarter suggestion.
 
Its your call whether to try to raise small funds for your personal scheme, or to go way bigger and represent the global open-source R&D movement, with a broad blessing from our community. I tend towards the latter community option as both safer, and a potentially more explosive success (if also slower and more work). The video you mention would be a knock-out if it densely montaged dozens of our prototypes. You can budget your R&D expenses to be first-in-line. Do not be afraid to go for the bigger bucks; AWE is  far hotter than the iphone cradle idea that raised over a million.
 
Good Luck either way, we will root for you!
 
daveS
 
PS I have not heard from Doug, but if he does not want to fly his HAWT to 500ft, any similar sized commercial unit would do for the demo.

  
Group: AirborneWindEnergy Message: 5819 From: harry valentine Date: 3/16/2012
Subject: Re: Kickstarter - AWE in Article
I've mentioned Airborne wind energy in my article at http://www.energypulse.net 

Harry


To: AirborneWindEnergy@yahoogroups.com
From: santos137@yahoo.com
Date: Fri, 16 Mar 2012 15:33:09 -0700
Subject: [AWES] Kickstarter

 

Rod,
 
By all means do try the KickStarter/FaceBook paths, but don't ever give up on Google someday funding another grander round of R&D, on a broader better balanced basis. Its just that you seemed to imply Kickstarter was a way to forget Google, in responding to a "Makani Hiring" post with the Kickstarter suggestion.
 
Its your call whether to try to raise small funds for your personal scheme, or to go way bigger and represent the global open-source R&D movement, with a broad blessing from our community. I tend towards the latter community option as both safer, and a potentially more explosive success (if also slower and more work). The video you mention would be a knock-out if it densely montaged dozens of our prototypes. You can budget your R&D expenses to be first-in-line. Do not be afraid to go for the bigger bucks; AWE is  far hotter than the iphone cradle idea that raised over a million.
 
Good Luck either way, we will root for you!
 
daveS
 
PS I have not heard from Doug, but if he does not want to fly his HAWT to 500ft, any similar sized commercial unit would do for the demo.

  

Group: AirborneWindEnergy Message: 5820 From: Robert Copcutt Date: 3/16/2012
Subject: Re: Makani Seeks Two Engineers
Rod,

In Visventis we have considered Kickstarter and competing schemes a
couple of times. Although I think there is certainly potential with
these sorts of fund raising processes the consensus is that Visventis
can manage for the moment on our own funds.

The problem is that there is a danger of shooting ourselves in the foot.
If anyone in the AWE community raises money through a big publicity
drive and the idea fails the whole community suffers a setback from the
negative publicity.

When I first got interested in wind power I was introduced to someone in
my community who had patented a vertical axis turbine design. There was
pressure to collaborate. He had built a toy sized model that span, but
there was no generator attached. I made my own model using old CDs and
an old floppy disc drive motor. Really crude and the parts bill was
almost zero. However, it was sufficient to prove that the design was
seriously flawed.

The message about keeping early prototypes as small as possible is
absolutely critical. Some large turbines have been built using cable
supported blades which I suspect resemble the design you are proposing.
They failed because if the wind changed direction too quickly they could
not keep all the cables in even tension.

Robert.


Group: AirborneWindEnergy Message: 5821 From: blturner3 Date: 3/17/2012
Subject: Re: Exploring carbon stiffening for the KiteGen kite?
I don't know what a LEI is. If you will pardon the criticism, this list often uses jargon level initials without explanation. That substantially lowers the readability for new users.

Yes, AoA does only weakly predict overall L/D but that was enough for the illustration. Because having airflow across bumps caused by ribs wether it's inflated or just flight pressures leads to an airfoil cross section that is less than ideal. So the ribs would ideally run with the local airflow over the wing. What I can't tell you is if that is worth the trouble. My gut tells me yes because it is mostly a one time expense.

I don't see stabilizing the sideslip as any more of a challenge than any other reel in method I have seen. The only possibly unsolvable problem is the added cost of the high speed reel in motors that still are efficient generators. You can't leave optimal generator design by much before the cost is huge in lost efficiency. Then you have to add a second reel in motor that costs money.

The kite forms that have emerged as best for their various applications is not an automatic prediction of them being best for AWE. AWE can tolerate slower turns than kite surfing. The oversized sidewalls of a C kite provide maneuverability that I don't think AWE needs at the cost of more wetted surface and other forms of drag. Inflated, thin wall spars are a maintenance point for a 24/7 machine. Part of that dreaded complexity but not a showstopper.

I think you are excessively concerned about low wind performance. When you do groundgen you can launch different kites for different conditions. Also because of the positive effects of scale up.

Carbon, used properly, does not add weight and can easily pay for it's cost. Makani and others tends to use it everywhere much like the proverbial kid with a hammer. I used to do this till I went back over some of my designs and realized it.

Composite compression load structures are much heavier than air based compression structures or pure tension structures. Yes "tensairity" is a good thing, but it's not the only thing.

Cool to here KiteGen though of a quadcopter for launch. I personally think that would work.

Brian

Group: AirborneWindEnergy Message: 5822 From: blturner3 Date: 3/17/2012
Subject: Flygen vs Groundgen
I could not find a thread on flygen vs groundgen so I decided to start one.
Flygen:
Makani
Joby
Magen

Groundgen:
About everyone else.

There are also a number of concepts that are not currently represented in
Flygen pluses:
Near continuous power output.
little mechanical losses
More likely to have severed tether flyability
powered launch option

Flygen minuses:
Expensive lightweight generators that are still heavy to lift.
Need the added weight and cost of props.
Electrical losses in the tether
May require transformers on the kite
heavier tether.
Larger diameter tether
Launch is more critical with heavier kites

Groundgen pluses:
Cheaper generators with not weight restrictions
Can use Different kites for different conditions
Can use Multikite tethers
Lighter kites present less of an impact danger
Lower cut-in windspeed
Can easily use soft-wing kites

Groundgen minuses:
intermittent power production
fatigue of tether
mechanical losses in tether and tether handling
different kites for different conditions
normally requires tether for controlled flight
More difficult to launch high performance hard-wings

That is just the off the top of my head issues. Next step would be to quantify the pluses and minuses.

I will start by countering Robert.

By the time you have enough windspeed to compete with coal the efficiency cost of lifting the generator is less than the lost generation time of reel-in. Sorry I don't have time to do the math on this, but I think the math would prove the point.

The launch is less than .5% of the total time in flight. Efficiency here is not an issue. I see no reason to believe that there is more weight and cost for launching a flygen vs a groundgen. That is because you have to be able to launch during no-wind at ground conditions in order to tap the added availability at height. So you always need a launch mechanism. (At least in the cheaper than coal systems) IMHO towed launch is the baseline for this and towed launch is essentially the same for groundgen and flygen.

Brian

Group: AirborneWindEnergy Message: 5823 From: harry valentine Date: 3/17/2012
Subject: Re: Flygen vs Groundgen
Hi Brian,

Good summary.

The main purpose of AWE technology is to gain access to winds that blow at higher velocity and that blow more consistently than winds at low elevation (as is the elevation of the hub of a tower-mounted wind turbine). There are towers now extending up to 100 to 120-metres above ground, with potential to reach 150-metres in some geographic locations .  .   .  .  . such as in a valley, where cables secured into valley walls will provide additional structural support to the towers (terrain-enhanced wind power). 

AWE technology can access winds that blow at a higher rate of availability at elevations above 300-metres. Ground-gen technology could definitely access winds that blow at elevations of 1000-metres and possibly much higher. 

Fly-gen technology encounters its own set of unique challenges .  .  .  . there may be a need for multiple balloons or kites along the tether, to carry the weight of the tether system. 

Terrain-enhanced and terrain-enabled high-elevation wind power is very possible and can access winds that blow through valleys at higher elevations above the valley floor, than the hub-height of tower-mounted wind turbines.

In a subsidy-free environment, there will likely be potential for terrain enhanced and terrain-enabled wind power to gain a customer base.
Development and market acceptance of ground-gen technology will likely follow. In the long-term future, fly-gen technology would likely find market application in some regions.

Harry


To: AirborneWindEnergy@yahoogroups.com
From: yahoo2@turnersystems.com
Date: Sat, 17 Mar 2012 16:14:16 +0000
Subject: [AWES] Flygen vs Groundgen

 


I could not find a thread on flygen vs groundgen so I decided to start one.
Flygen:
Makani
Joby
Magen

Groundgen:
About everyone else.

There are also a number of concepts that are not currently represented in
Flygen pluses:
Near continuous power output.
little mechanical losses
More likely to have severed tether flyability
powered launch option

Flygen minuses:
Expensive lightweight generators that are still heavy to lift.
Need the added weight and cost of props.
Electrical losses in the tether
May require transformers on the kite
heavier tether.
Larger diameter tether
Launch is more critical with heavier kites

Groundgen pluses:
Cheaper generators with not weight restrictions
Can use Different kites for different conditions
Can use Multikite tethers
Lighter kites present less of an impact danger
Lower cut-in windspeed
Can easily use soft-wing kites

Groundgen minuses:
intermittent power production
fatigue of tether
mechanical losses in tether and tether handling
different kites for different conditions
normally requires tether for controlled flight
More difficult to launch high performance hard-wings

That is just the off the top of my head issues. Next step would be to quantify the pluses and minuses.

I will start by countering Robert.

By the time you have enough windspeed to compete with coal the efficiency cost of lifting the generator is less than the lost generation time of reel-in. Sorry I don't have time to do the math on this, but I think the math would prove the point.

The launch is less than .5% of the total time in flight. Efficiency here is not an issue. I see no reason to believe that there is more weight and cost for launching a flygen vs a groundgen. That is because you have to be able to launch during no-wind at ground conditions in order to tap the added availability at height. So you always need a launch mechanism. (At least in the cheaper than coal systems) IMHO towed launch is the baseline for this and towed launch is essentially the same for groundgen and flygen.

Brian


Group: AirborneWindEnergy Message: 5824 From: Doug Date: 3/17/2012
Subject: Re: Makani Seeks Two Engineers
Robert:
Congratulations that you saw the writing on the wall and did not remain in denial of reality forever. I saw those CD spinners on YouTube and thought "here we go again for the thousandth time"...

I think the worst aspect of these crackpot designs that start with zero knowledge and go downhill from there is this:

Coming in, they strongly state overwhelming superiority over known technology in press releases. Often these announcements are completely dismissive of turbines that can power 1000 homes simultaneously, while their prototype, usually vertical-axis, usually drag-based, as you relate, has not even been connected to a generator at all! Hey let me tell you these vertical axis machines perform FANTASTIC as long as you never take that critical step of connecting it to a (gasp!) generator...

Anyway these newbie will kick and scream and call all sorts of names if anyone with any experience with wind energy tries to give them a heads-up. They create all sorts of controversy and get really angry and also get the people they are bothering angry, and the whole time they talk talk talk about how great they are and how superior their drag-based idea is. And how stupid they think working "GE turbines" are, since they don't know any other brand names to cite. They always cite GE and never any other brand. Well, we DID say they are idiots...

Then their idea fails. It fails a few times, over maybe a couple of years. And guess what?
The perpetrators, purveyors, promoters, NEVER come back and apologize. They never return with a statement like "Well I guess I was wrong and the people making turbines based on 3000 years of experience were right after all - sorry I bragged so much - I guess I didn't know what I was talking about".
Nope, that is one thing you will never hear.
Or how about
"Sorry we wasted so much money - I guess we were idiots"
or maybe
"Sorry we lied - didn't understand how bad we were lying at the time, but you told us and we didn't listen and now we can see that everything we said was in reality a complete lie".

It would be nice to see some of these (clearly in retrospect) hucksters admit that they were wrong, just once. We need a few more Robert Copcutts who can admit that they chased a false trail.

I think I must have heard a thousand, by now, of the incoming bragging statements, and not once have we had the "exit interview" of why any of these superior ideas somehow (gee ya think?) didn't pan out.

Today we have horrendous winds and rain. The hundreds of 10 kW turbines powering the homes in this area are all sideways in self-protection mode, but still bouncing off full-power as they cycle in and out of furling. Ah prolly nobody knows what I am talking about now...
Seeya!

Doug S.

Group: AirborneWindEnergy Message: 5825 From: dave santos Date: 3/17/2012
Subject: Re: Flygen vs Groundgen
Brian,
 
This issue has been a top topic on the forum: Safety under existing aviation regulations (and the underlying physical basis for the regs), and therefore liability insurability, seems like the early decisive utility-scale factor in favor of GroundGens. Small Flygens avoid excessive cubic-mass scaling penalties and do not invoke high-consequence safety concerns like large Flygens do. The safety concerns are quantified into aviation regulations that place strict requirements on aircraft based on mass and velocity. Thus a flygen of a given mass generates less power-to-weight than a bare kite, and its larger free-fall terminal-velocity creates a more substantial hazard. Many such quantifiables are highly success-predictive of GroundGens in the short term.
 
You missed a long list of FlyGen players like Altaeros, Sky Windpower, Honeywell, and many small AWECS developers. KiteLab Group embraces both Flygens and Groundgens, depending on scale and operational needs, and forsees that giant superconducting generators could in fact someday, decades from now, be lifted by large array formations, mainly for reasons of farm self-mobility (ferrying) or even for high operational independence from the surface (airborne architecture).
 
The reason for the Cult of Lowest Mass-Aloft is not just for low wind generation; weight is simply toxic to a good kite, the lightest practical kite wins operationally by many virtues, especially by better general flight performance and especially critical flight stability. In special conditions where more mass is desired, water-ballast is an option (just as high-performance gliders take on water ballast at times).
 
You seem to think long reeling cycles, and therefore "intermittent power production" is an inherent flaw to ground gens. In fact, on this Forum, its well known that high-frequency short-stroke pumping and continuous-loop rope-driving are quite practical. Long-cycle reeling is mostly just an early historic phase, much as early biplanes were, and the tether fatigue problems of reeling will mostly go away. On the other hand, composite conductive/strucutural cables have severe inherent problems that simple tethers avoid.
 
It would be nice if someone formally explained and proved what is widely believed, that groundgens are generally superior, but this involves a fundamental quantum physics comparison of tug v. electrical efficiency. There is ongoing informal study behind the scenes, with help from Dr. Jeremy Rutman and Dave Lang, with some exciting results due soon,
 
daveS
 
 
PS Ribbed wings are so bad as you suggest, usually provided the ribs run streamwise. Ribs can even act as part of a turbulation mechanism to maintain attached flow in turbulent conditions. One sees ribbed wings everywhere in nature, from insects to birds and bats and fish fins. Its wonderful to see how stone-age aerodynamicists figured out how to use *transverse* ribs as turbulators on items like throwing sticks, enhancing performance. Modern toys like Frisbees and Aerobies rely on ribs in just this way. Ribs is therefore just a tool in our wing-design toolkit.
 
Yes, there are lots of acronyms used in professional aviation, and engineering generally, to keep communication concise, and they do require learning them to serve as aids. The AWE Forum is billed as a professional-level venue, so acronyms come with the territory. LEI stands for "Leading Edge Inflatable" (Kite), the technology invented by the Legaignoux brothers enabling kitesurfing to become popular by a kite that will not sink or take on water.
 
 

 
    
Group: AirborneWindEnergy Message: 5826 From: Joe Faust Date: 3/17/2012
Subject: "Gliding kite" (paraglider big) served 10 skydivers at once
Sent: Saturday, March 17, 2012 3:31 PM
Subject: "Gliding kite" (paraglider big) served 10 skydivers at once

Big paraglider with 10 passengers


Aluminum ladder rig beneath pilot in command (PIC) was a COTS choice. 
(Note: Someone had to drive to altitude; probably oil was used to get the skydivers and PIC to mountain launch. One day kite energy will be used to give the launch lift.)

Group: AirborneWindEnergy Message: 5827 From: dave santos Date: 3/17/2012
Subject: Correction and Addendum //Re: [AWES] Flygen vs Groundgen
Whoops, regarding ribbed wings, i meant to write that "ribbed wings are NOT so bad" as suggested.
 
Also forgot to add High Voltage risk to the rehashing of inherent FlyGen disadvantages, and also note the many expensive high mass power electronic components that are in addition to generator mass (transformer and power MOSFET bricks, conductive tether, etc.).
 
There are many other smaller disadvantages, and also advantages, mentioned in the old posts; we did a pretty good job thinking this topic through, but there will still be new angles to find and ponder.
 
Power-to-weight was proposed as a major predictor of FlyGen v. Groundgen outcome.
 
-------------------------------
 
Hi Dave,
Was a "not" meant in the PS intro sentence?
"PS Ribbed wings are so bad as you suggest, usually provided the ribs run streamwise"

JoeF

Group: AirborneWindEnergy Message: 5828 From: mmarchitti Date: 3/18/2012
Subject: Re: Flygen vs Groundgen
Several GroundGen minuses are not really minuses

-The intermittent power production can be tolerated by the electric grid. In any case you can provide the ground gen plant with an energy buffer by the use for example of the supercapacitor, http://www.youtube.com/watch?v=v1vLQ1XYdOk

- There is of course a fatigue on the tether, but it can be accountend for, by appropriate testing, as in this test rig, http://fuoripista.webs.com/Immag0006.jpg

-The mechanical losses in the cable are really minor

-You do not have to use different kites

-I do not see a minus in the use of the tether to control the kites

-The launch is really a challenge, and this should stimulate technitian to find solutions and optimise the control in such a delicate phase.


Group: AirborneWindEnergy Message: 5829 From: Robert Copcutt Date: 3/18/2012
Subject: NASA on kite physics
This NASA page is a good introduction to kite physics. I have not seen
it mentioned in this group before.
http://www.grc.nasa.gov/WWW/k-12/airplane/shortk.html
Group: AirborneWindEnergy Message: 5830 From: Doug Date: 3/19/2012
Subject: Re: Flygen vs Groundgen / squaregen vs roundgen
If you are not producing steady power - at least as steady as the wind itself, then you have not reached the point of basic adequacy for a wind energy system. Or any other system. Name another power system that is intermittent. Achieving steady-state power was accomplished 3000 years ago. Look at the laddermill for an example of a drag-based system that would give steady-state performance if anyone bothered to build it, which they have not (perhaps because laddermill itself might suggest further refinement to a SuperTurbine(R)?). Go back to the drawing board - you don't have it yet!
:)
Yes the grid can tolerate intermittent power - especially if enough intermittent systems are averaged. What cannot tolerate intermittent operation are:
1) Your budget, since you cannot afford a generator, let alone a whole multi-million dollar system, working half the time - think about it. If you have a competitor who can use the same material to generate steady-state power they will out-compete you 2:1!
2) Your machinery, since machinery loves steady-state operation for reliablity and longevity.

PS
Most Irish people have never heard of Irish Spring soap, or Lucky Charms cereal! Now that is a travesty!
:)
"Always after me Lucky Charms!"
"But I like it too!"...

Group: AirborneWindEnergy Message: 5831 From: Joe Faust Date: 3/19/2012
Subject: Energy and signal in 1902 by Trainor
Patent US 701106 Filed Feb 14, 1902 by Hughie J. Trainor for Kite.   This AWES converts part of the wind's energy to vibrations that are sent through the tether to a ground converter of the vibrations into the vibration of a diaphragm that makes sound for the hearing enjoyment of a person on the ground. 

AWES status signal-prints?  Characteristic patterns in vibrations may tell a smart signal-receiving program about the health and status of elements in the wing set of a working kite system.  Fingerprints (vibration prints) of normal, abnormal, failures, etc.?    How far could this be taken?

JoeF
Group: AirborneWindEnergy Message: 5832 From: dave santos Date: 3/19/2012
Subject: Re: Energy and signal in 1902 by Trainor
These forgotten old "Village Idiot Patents"* are amazing in how they could not until now be easily recognized to contain the mighty principles of AWE operation poised to someday power the world. Hughie Trainor is a most hapless hero who must of had a fit when the patent illustrator botched the depiction of the pilot, shown clutching the string in an inoperable death-grip. Poor Hughie must never have had any hopeful result from this pathetic patent adventure. Its hardly even a plausible toy, but it has a very high Classical Toy quotient (combined kite, whistle, and tin-can telephone), a predictor of hidden profundity.
 
Here we have a nice Barn-Door Kite and tether, with an added whistle** transducer to convert upper-wind momentum into phonons (packets of acoustic/mechanical energy) that run down the line to a ground-based transducer converting the line phonons into music (free-space phonons).
 
A key phrase notes -
 
"...other forms of acoustical devices may be used..."
 
So there we have it; the basic theory of operation for the grandest AWES groundgen concepts of today. The current engineering-science issue is to determine the optimal tug frequencies and amplitudes. We can only say at present that the peak amplitudes must stay within a working-load limit (well below the rated yield point), and that the optimal frequency band needs to be determined, especially to avoid too much slack-phase or high dispersion of longitudinal wave-energy into coupled transverse modes.
 
 
* In this case Jersey City, even :)
 
** All our oscillating kites are infrasonic "whistles"

  
Group: AirborneWindEnergy Message: 5833 From: blturner3 Date: 3/19/2012
Subject: Re: Flygen vs Groundgen
OK here is a quick back of napkin math for the generator weight issue. I am leaving out dozens of details here but I think I'm in the ballpark.

If your reeling out tether at 5 mph on a 1 megawatt generator then you have about 50 tons of tension in that line. A 1 megawatt flygen generator would weigh a bit over 2 tons. lifting 2 tons on a kite takes more than 2 tons of force so guess double that. 4 tons. Or 8% of your energy goes to lifting the generator. Not insignificant, but hardly a show-stopper.

There would be no onboard transformers. The generator would produce the transmission voltage directly. The power mosfets might or might not be needed and they would only be a few hundred pounds in any case.

The number most of you will jump on is the 2 tons. Thats because wind turbine generators weigh about 4 to 5 times that now.
Here is an article that reinforces the point.
http://digital-library.theiet.org/getabs/servlet/GetabsServlet?prog=normal&id=IEPAER000152000001000017000001&idtype=cvips&gifs=yes&ref=no
I don't know if that link works so here is the google search link.
http://www.google.com/search?client=safari&rls=en&q=E.+Spooner,+P.+Gordon,+J.R.+Bumby+and+C.D.+French,+"Lightweight,+ironless-stator,+PM+generators+for+direct-drive+wind+turbines"&ie=UTF-8&oe=UTF-8

It's rare earth magnets with an ironless core. Expensive but not unknown tech.

If someone could do a similar analysis on the how tether stretch and sag saps less than 5% that would be cool. On a short stroke it could easily sap 70%.

70% of what is a whole other discussion.

Brian

Group: AirborneWindEnergy Message: 5834 From: Pierre BENHAIEM Date: 3/20/2012
Subject: Re: Flygen vs Groundgen

"The number most of you will jump on is the 2 tons. Thats because wind turbine generators weigh about 4 to 5 times that now.
Here is an article that reinforces the point."Not only:apparent wind on the turbine by far is higher,so the weight of aloft generator (in crosswind flight configuration) is lower,and a gear is not needed.On the other hand the weight of electric wires is not insignificant (probably higher than generator weight).

For groundgen (reel) capacitors can be a solution but are very expensive because of the level of required smoothing between power phase (roughly 2/3 of time) and retrieval phase (1/3 of time).In the other hand capacitors can be avoided for kite-farm implementation which appropriate management,but it is probably not so easy.

Flygen has another (linked to continuous power) pluse:an easier automatic management since there is only one configuration of flight (excepted launching and retrieval).

And a continuous power can be an essential feature for applications like loading electric cars according to a self-service where the customer puts off his unloaded car and takes a loaded car,that without the necessity joining the grid.

For making a correct evaluation we should see the possible applications.For conventional wind turbines joining the grid probably has been an error because of wind irregularity (variations are compensated with more coal due to the inertia of warm).

With AWE let us do not the same error and let us build a whole economic system.Nor electric cars can be good if energy source is clean,and wind irregularity is not a problem for loading and stocking batteries.

Pierre.B
http://flygenkite.com  



Group: AirborneWindEnergy Message: 5835 From: Doug Date: 3/20/2012
Subject: Re: Energy and signal in 1902 by Trainor
One of my favorite village idiot patent is a helicopter/flying machine showing a guy with a shotgun and his dog getting out to go hunting in the wilderness - an illustration suitable for framing on your wall. Forgot the number - sorry...

Group: AirborneWindEnergy Message: 5836 From: Doug Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
Nice to see some simple math - this implies you should take the gen into the sky since you need to lift more than that to pull a tether. Goes along with my previous point about tension-based power transmission serving quite efficiently to pull the machine out of the sky. (doh!)

Without reading the article, ironless core alternators (at least of the axial flux variety) use a lot of steel (thick steel discs) to physically keep the magnets from pulling together, since you need twice as many magnets, to have magnets on both sides of the airgap.
I make supermagnet alternators that have the iron stator because they are faster and easier to make, and use less magnets.

http://www.PM-ALT.com There's that old "They have been doing it this way for 100 years" thing... There are many possibilities once you start using supermagnets, most probably never tried!

Doug Selsam

Group: AirborneWindEnergy Message: 5837 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
I don't think Brian is carefully accounting for many major issues previously posed-
 
Group: AirborneWindEnergy Message: 5838 From: blturner3 Date: 3/20/2012
Subject: Re: Flygen vs Groundgen - wire weight
Today I did the math for the weight of the wire.
1 megawatt via 2000 volts at 500 amps.
0000 aluminum wire 1500 ft long tether. 3000 ft total.
resistance is .2412 ohms. wireless is 60,300 watts or 6%
heat per foot is 40 watts. Gotta make sure it has airflow.
Weight is 195lbs per 1000 ft.
So 600 lbs for the wire. Not a show-stopper.

Thicker wire might be better. And the tensile strength of the wire is not high enough. So it will need some kevlar added. The diameter of the wire will be more than Kevlar. Yes, Dave, composite tether could be a pain.

Brian

Group: AirborneWindEnergy Message: 5839 From: blturner3 Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
--- In AirborneWindEnergy@yahoogroups.com, dave santos <santos137@... No I'm not. I don't really have time for the ones that I am addressing.
Crashing a robot kite into the ocean is hardly a big deal. Aircraft insurance is a manifestation of the bizarre tort laws in the United States. Don't let anyone get close enough to get hurt and the liability is manageable. I know our visions of the future don't match in this area. We already had that thread.

Yes the higher cost of rare earth magnets could be a show-stopper. I have not done that math yet.
The reason that "Rope Driving" reaches I don't get this statement. Higher altitudes are more losses for virtually all systems. But yes I think that flygens will have a harder time reaching 10,000 ft than groundgens.
Yes. I have not calculated that one yet. Probably not a big deal. I think it's only about 30% more diameter.
Yes, and a possible show stopper. My guess here is that the low end of the wind is not missing that much. More math.
Yes. True. But at some scale you hit the tensile strength of your material and then even the membranes scale in 3d. It's an oversimplification.
There is an ample supply of cooling air.
Probably, That is one of the reasons why I have said that I think groundgen has an advantage.

If yahoo groups had a good search and everyone posted with searchability in mind then no all new users could just look it up. I think it's as much a limitation of the format than anything.

That is the question that I am looking to answer. I have yet to see the simple critical path to failure that you speak of. No single disadvantage I have explored is a show-stopper and I have yet to put any number of them together to lead to unavoidable failure.

Small systems of almost any type escape their flaws. That is why I like scales where the concepts can't escape their flaws. It makes me a fan of people and companies that seek to build at those scales. I don't mean to belittle the other researchers It's just more exciting to see the bigger stuff.

I would like to see the grim curve you speak of. If you remember what team, please do post.

Brian
Group: AirborneWindEnergy Message: 5840 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen - wire weight
Brian,
 
While Alu seems favored by weight-to-power, it has poor fatigue life and thus has been found problematic for a typical AWES with tether reeling and surge cycles. Copper has thus been seen as favored, despite the weight gain. Alu is not excluded, but you are clearly stretching to make a case for FlyGens. Obviously pure UHMWPE has far superior fatigue life to either metal.
 
Composite AWES tethers have been found to be very problematic- they are not COTS, so industrial production must start from scratch (no team can escape COTS competition). There is the obvious mismatch of structural properties, thermal issues, electrical/fire safety issues; its really a longterm quest to resolve the many open challenges.
 
There is no single "showstopper" for FlyGens (except ultimate scalability), its "death-by-a-thousand-cuts", the multiplied disadvantages that is stopping the FlyGen show. So of course Makani (as our reference model for flygen) spent about a hundred times more to produce about half the power 5 years after KiteGen in 2006 (as a groundgen reference).
 
If your napkin calculation cannot explain this well established pattern (both predictive and tested), which is holding across all AWE R&D, then maybe you need a fresh napkin ;^)
 
Do both sides of the analysis on a weight-to-power basis, but beware unconciously favoring FlyGen (like assuming Alu over Cu) while guessing pessimistically about GroundGen (like assuming 70% rope-driving transmission loss (where did that particular number come from?)).
 
Again, thanks for taking up the FlyGen cause, to make it more of a proper debate, there is no shame in challenging any assumption,
 
daveS

  
Group: AirborneWindEnergy Message: 5841 From: dave santos Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
Brian,
 
Your wrote-
 
"Crashing a robot kite into the ocean is hardly a big deal."
 
Read the excellent crash investigation of the NASA Helios UAV* for a professional counter-view of crashing a fancy jumbo E-flight wing in the sea. Keep in mind that a metroplex like NYC or the Bay Area requires over a thousand offshore Makani M1-class kiteplanes (more air-traffic than Heathrow), and they would all crash within days with current state-of-the-art autonomous-flight avionics. Crashing fancy flying robots offshore is a big deal if you hope to compete financially against SkySails fishing soggy parafoils out of the water for reuse. A single sea storm will erase these kiteplanes much as the Spanish or Kubla Kahn's Armadas. Ask any old sailor.
 
Remember that aviation culture has clearly mastered land-based operations overhead, and attendent risk issues, including the compensation of victims. It would be a huge step backward to allow "wrong-stuff" incompetence to creep back in, via AWE, in the name of a false libertarianism or lassez-faire sociopathology. Never fear, competent aeronautical engineers master safety issues, as is only right.
 
If you like the big AWES concepts, GroundGen clearly dominates, with several leading teams proposing many interesting integrated gigawatt-scale concepts, compared to optimistic FlyGens scale-limited to 5 megawatt units (Makani). I think maybe it was Altaeros that nicely simulated the predictable generator weight-to-power scaling hit in a paper discussed on this Forum, but any mechanical or power engineer can make the same prediction; scaling-law is scaling-law.
 
One can surely data-mine the old Forum posts more powerfully, but its still humanly possible to read them all, which i would undertake if intending to catch up. We have learned volumes in recent years. Its quite wonderful how much knowledge there is to guide us. AWE truly advances by dry homework; not just field-testing everything and building kite flight hours,
 
daveS
 
* The crash report is at:
 
 

 
    
Group: AirborneWindEnergy Message: 5842 From: dave santos Date: 3/20/2012
Subject: Displacing fuel and slashing costs- Wind Powered Aviation
To displace fuel consumption directly with kites is true energy awareness and mastery. The most exciting such kite use is to directly displace conventional fuel-based aviation. Not only is there the ecological benefit, but high costs are slashed: Aviation is thus made affordable to virtually everyone.
 
Initially the expansion of kite-based aviation is confined to special niches. Generally these niches are in "low and slow" local markets. KAPers (Kite Assisted Photographers) are severely eroding the market-share of elite helicopter-based wedding photography, while creating a greatly expanded aerial photography market. Now even a middle-class child's party can be affordably captured from above. The absence of noise and greater safety also count. Avgas, by the way, still has lead added.
 
We see how kites can serve agriculture. We see how wind-driven wildfires will be fought by kite. Once again, existing aviation sectors can be directly displaced. A kite system set high above in good wind can raise almost anything with simple tackle. Kite-based pick and place over a cluttered surface of massive out-sized objects can be very competitive with Skyhook service.
 
Cool aviation sports need not involve high fuel use if windpower will do. Skydiving will become widely popular when two dollar kite jumps replace twenty-five dollar airplane jumps. Kite-towing gliders aloft is the kind of open niche almost anyone can study and figure out. A kite can tension a bungee to launch sport aircraft and humans ballistically. Kites are a most playful revolution in a desperate practical world.
 
To be "cheaper than coal" is hard; coal is so damn cheap. To be "cheaper than fueled aviation" is far easier, more like just being "cheaper than diamonds". Anyone who wants to make a nice quick buck in AWE, the new fuelless aviation is the way.
 
 
coolIP
 
 
Group: AirborneWindEnergy Message: 5843 From: Joe Faust Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
Momentum is a vector quantity. Mass moving in a direction with a given velocity is mv. It will ever cost to change the direction of mass flying. 
Group: AirborneWindEnergy Message: 5844 From: Joe Faust Date: 3/20/2012
Subject: Re: Flygen vs Groundgen
Corrected phrase:
Mass moving in a direction with a given velocity results in momentum of mv.
Group: AirborneWindEnergy Message: 5845 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
Brian

That paper was a good find. I have been working in that direction for
some time so I will need to dig out a full copy of it the next
opportunity I get.

Last year when I considered that a certain amount of flygen was a good
idea (say 10 to 20% flygen, balance groundgen) I started a spreadsheet
looking at tether strength and drag and mass etc. I will try to get it
into a presentable form asap. Since then I have discovered a source of
dyneema for a price comparable to steel. Dyneema is so much safer than
steel - no splinters, or snap-back on breakage, far better fatigue
tolerance.

Loyd estimated that the optimum reeling out speed is half the wind
speed. Therefore in your example the wind is at 10mph. You would need an
absolutely enormous kite to generate 50t tension plus the excess needed
to keep the generator airborne in such a mild wind. A flygen still needs
a stiff turbine and they get rapidly heavier as they get bigger. With
the size of generator Pierre uses it should be easy to reach the 0.5W/kg
example you use. A paper I found claimed that turbine mass increases in
proportion to the diameter to the power of 2.7 (I think). They used real
examples, not any theoretical estimates. Therefore groundgens scale much
better than flygens.

Another thing against flygen is radar interference. Not a trivial matter
apparently.


Robert.



Group: AirborneWindEnergy Message: 5846 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
On Sat, 2012-03-17 at 16:14 +0000, blturner3 wrote:
This is not an issue. Any wind generator needs to be hooked to either
the grid or a battery bank. Neither will be bothered by the intermittent
power.


Dyneema is incredibly good.

Not if it is designed well.

This is a potential advantage. For a flygen you could swop the
generator/turbine unit between different sized wings but it could only
be optimised for one size. With groundgen the airborne component (kite)
is low mass so it is potentially much cheaper that the flygen kite.
Groundgen can therefore afford to have a range of kites to suit a range
of wind conditions which greatly increases utilization of the expensive
generator and power electronics. Each kite would have its own tether and
reel because the low wind kite will need heavier tethers on a bigger
reel. When you have several to use tether and kite wear becomes less of
a problem.

Pull the kite away at ground level to extend the tether then use the
rewind mechanism to launch the kite.

I started working on it but have too many others things to do to finish.
Motivation also dropped when it became obvious groundgen is the clear
winner.

Robert.
Group: AirborneWindEnergy Message: 5847 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Makani Seeks Two Engineers
Doug,

Just to be clear I have not seen anything on Youtube resembling what I
made. This inventor had patented a variation of a common Savonius
turbine. I made a Savonius by cutting a Pringles cardboard tube in half
to make the blades. I sandwiched the blades between 2 CDs. Gives you an
idea of its size and how easy it was to make. Tiny turbines are
appallingly inefficient but you can do comparisons. Building the same
sized turbine according to the patent produced worse results so that
settled the issue in my mind.



Group: AirborneWindEnergy Message: 5848 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen - wire weight
A pair of separated independent ropes made from steel is the only
sensible option for flygen. Its conductivity is good enough and anything
else costs too much. Combining steel with any polymer is asking for
trouble. The interface between the 2 will wear badly. Even though
Dyneema has a similar elasticity to steel I think it would just get in
the way.

Robert.


Group: AirborneWindEnergy Message: 5849 From: Joe Faust Date: 3/21/2012
Subject: Startram
Watching Startram for any AWES rubs: 

Group: AirborneWindEnergy Message: 5850 From: blturner3 Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
Yes, I should add that to the list. Changing directions is a function of speed and mass. The energy to do that has to come from somewhere. Control inputs also consume power.

Brian
Group: AirborneWindEnergy Message: 5851 From: dave santos Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
Many physics statements being made on this thread seem confused and off-topic. Its far more to the point to analise ROI of Flygen v. GroundGen in terms like insurability, rather than futzing with high-school physics.
 
Momentum is the product of mass and velocity. Direction need not be explicitly invoked in this most basic definition. "Changing directions" is not well described as a "function of speed and mass". One can in fact define a true direction in a coordinate system and then change it, with no need to invoke speed or mass. That "the energy to do that has to come from somewhere" is very misleading, since energy is conserved in elastic collisions (like a photon changing direction off a mirror) and rotating objects that constantly change direction.
 
"Control inputs also consume power" also seems far from the topic of FlyGen v GroundGen, as both share the same fundamental control physics (Shannon's Information Theory as the culmination of Carnot's Classical Thermodynamics). This point would thus be better as a wholly separate topic (like Active Avionic Control v. Passive Stabilities).
 
Note also that steel is not "the only sensible option for FlyGen". Steel weighs almost as much as Copper, but is ten times more resistive. Steel weighs over ten times more by rated working load than UHMWPE. Saving marginal capital-cost by adding weight is not a promising flight-engineering practice.
 
Also, Generators do become increasingly hard to cool as they scale, as the cooling surface only grows at the square and the internal mass and volume grows at the cube. Internal heat has a longer path to dissipation. Nor is there "plenty of air" to cool flygens. Air is a rather poor conductor of heat. Cooling scaled-up hard-driven FlyGens is such a toughie that Makani's CTO specifically identified this as a priority in the "private" NearZero Expert Panel.
 
Lets try extra hard to inform this list of AWE engineering science at a professional level, rather than keep the forum as a perpetual bunny slope (which it truly was at first). Forum technical standards are rising fast as we learn. Separate AWE newbie forums at some point will be needed to orient beginners, or a super-wonky new forum will have to be set up. Hopefully we can keep this original forum advancing.
 
By now every serious AWE researcher knows: 1) AWE works on paper; 2) AWE works in reality, by dozens of prototype demos (imperfectly, yes); 3) There is considerable clarity on many once mysterious detail-engineering issues, with so much study and direct test results to draw on.

 
Group: AirborneWindEnergy Message: 5852 From: Dave Lang Date: 3/21/2012
Subject: Re: Flygen vs Groundgen

At 1:56 PM -0700 3/21/12, dave santos wrote:
Group: AirborneWindEnergy Message: 5853 From: dave santos Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
DaveL
 
I was insisting that "direction" is corollary to the "momentum" issue, as i understood it. Direction per se has little to do with FlyGen v. GroundGen. Of course a vector quantity has direction, we all agree, but this need not be superfluously explicit, if we seek the simplest applicable definition. Velocity is also a vector quantity; but in many of our velocity calculations, we completely disregard direction.
 
Direction of momentum can change with conservation of forces, such as a spinning rod, oscillating spring-mass, or reflected photon (elastic collision). My objection was to a phrase that to me suggested direction change as a dissipative process, when conservation of energy is our major working principle.
 
I summarize by asserting that power-to-weight is the concise predictive physics, but this topic is hardly just about physics,
 
daveS

 
Group: AirborneWindEnergy Message: 5854 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
Newton's first law of motion: "The velocity of a body remains constant
unless the body is acted upon by an external force."
from
http://en.wikipedia.org/wiki/Newton%27s_laws_of_motion

and

"In physics, velocity is speed in a given direction." ie. a vector.

A single kite flying in circles or figure 8's will use energy to change
direction. That is just one reason why dancing pairs is ultimately the
way to go. The work done by one kite to change direction is transmitted
by the tether between them to move its partner in the opposite
direction.

The pair becomes like a 2 blade turbine. Obviously 3 kites could also be
used but I see little advantage. The advantage over a turbine is that
everything is in tension so mass is greatly reduced. Airborne mass is
real bad news as already discussed.

The huge importance of all airborne structures being under tension also
means the power must be transmitted to the ground by tension - not
torsion.

Robert.
Group: AirborneWindEnergy Message: 5855 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
On Wed, 2012-03-21 at 13:56 -0700, dave santos wrote:
Power lines all over the world transmit 32kV and more and they are
insulated only by the gap between the lines. There is no reason a flygen
should not do the same. Therefore the resistance of steel is not a
problem. Strength is the issue and in terms of ROI nothing I can find
comes close to steel. I will post the spreadsheet proving that once it
is made presentable. We are agreed UHMWPE (Dyneema) wins for groundgens.

We need a website with a concise clear tutorial.

Robert.
Group: AirborneWindEnergy Message: 5856 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Startram
It makes so much more sense than the space elevator. They have a few
things wrong though; the tube should be vertical and it should be near
the equator.


Group: AirborneWindEnergy Message: 5857 From: Robert Copcutt Date: 3/21/2012
Subject: Re: Flygen vs Groundgen
A clarification for Joe. In Loyd's 1980 paper in J. Power in Fig 4 he
plots 3 curves. Fs is of no practical interest. Fc peaks at 1/3 wind
velocity and Fd peaks at 1/2. The paper needs to be read carefully to
understand what Fc and Fd mean. My understanding is that Fd requires a
controllable angle of attach. It is the best outcome so it is what I
work with for my feasibility studies.

Robert.