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Old 06-20-2014, 05:59 PM   #21 (permalink)
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I think this is a job for Wonka

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Old 06-21-2014, 04:36 AM   #22 (permalink)
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Old 06-21-2014, 01:27 PM   #23 (permalink)
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Old 06-21-2014, 07:59 PM   #24 (permalink)
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Lol well I'm still scratching my head on it, so I thought getting rid of all the aerodynamic razzle dazzle and making it a plain buoyancy/regen problem might help. The first thing that jumped out was the pressure change is definitely working against compression/expansion.

For a gross approximation, I would assume 100% regen efficiency in compressor and winch and battery, and ignore energy in reeling up slack/piston friction etc, just a pv=nrt and energy available in ascent and energy lost in compressing at top and expanding at bottom (less force for the same distance), with some arbitrary ascent height, and assume the cylinder/piston is insulated and neutrally buoyant when fully compressed at the bottom.



I don't think there is free energy there, but havent done the math...
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Old 06-21-2014, 09:20 PM   #25 (permalink)
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How much energy can you get out of something that is only slightly more or less buoyant than the surrounding water. It's like a balloon that has a pencils worth of positive buoyancy. It'll go up pretty high into the atmosphere, but you'll get very little energy generation from it.

It'll probably go on for a very long time underwater, because you don't need much energy to rise or fall if you're straddling the line of neutral buoyancy. It would rise slowly and slowly to turn a generator. The height it ascends or descends may be large, but not a reflection on how much power it could generate. If you used more energy for more positive lift, you'd fight against the drag of water going up.

It's like the drinking birds. They'll bob up and down forever, but there just running off of the heat differential. There's waste somewhere, and eventually it'll stop.
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Old 06-21-2014, 10:24 PM   #26 (permalink)
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I was ruling out all the other losses, because even if the theoretical net compression losses perfectly equal the theoretical ascent gains, then it is *mathematically* proven to be a stupid idea. (yes, slow assumed under water, ignore the drag for now too. With a direct coupling via a tether the speed doesn't really matter, just force and distance).

I'm no Archimedes though. Apparently the compressiblity of air is a factor too, a ballon will be more buoyant on the ground, but a barrel in the water isn't more buoyant at depth, just a function of displacement...
http://www.physicsforums.com/showthread.php?t=322544

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Old 06-22-2014, 11:29 AM   #27 (permalink)
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Quote:
Originally Posted by mort View Post
Hello P-hack,
Naturally the design could be optimized to demonstrate the viability of the idea. For instance, make the gas envelope a torus with the wind generator-propeller in the opening and the various mechanicals underslung of the gas bag.
Consider the Goodyear blimp, Spirit of Goodyear. It has a gas capacity of about 200,000 cu ft which in helium provides 14,000 lbs. of lift (at sea level etc.)
The amount of power you can get out of the wind, that's during rapid descent, is:
P = 1/2 A*d*v**3
where v is the wind speed
d is air density
and A is the swept area of the blades
For modern designs, efficiency of the actual wind power mechanism is around
45% - that is 45% of the kinetic energy in the wind can be recovered as electricity.
A regular torus 120 feet wide with a hole 30 feet wide (R=45' and r=15') has a volume of 200,000 cu ft. The hole in the center has an area of 700 sq ft
Air density is 0.0023769 slugs/cu ft (sea level, 70 degrees F, etc.) The power produced is about:
P = .45 * .832 * v**3 (efficiency times area times density times speed cubed)
Now this gets a bit scary-
If you could descend at 125 mph (183 ft/sec) that would develop 9000 hp for 54 seconds (falling 10,000 ft) Assume a compressor-expander with round trip efficiency about 80% 9000 hp now is the difference between the power needed to compress the gas and the power you get back expanding the gas. You could run a compressor at 45000 hp for .91 minutes and compress 200,000 cu ft of helium in that time (3 stage compressor 15 psi to 215 psi helium adiabatic expansion coefficient=1.67). By the way that's about 8 Tesla S batteries worth of juice. That's about 100% of your gas bag volume. Assume the torus is actually streamlined for descent, and the Cd is just about the Cd of the windmill -- .5 at 700 sq ft. The drag on the airship falling at 183 ft/sec is 14,000 lb, so the ship is at terminal velocity for free fall.
The point is that you can fall fast enough to generate the power needed to recharge the battery. You don't need to completely deflate the bag to descend, but the faster you fall the better.

The airship could be scaled up to quite huge size so the load capacity would be sufficient to carry that big compressor and battery.
-mort

There's an additional factor: generator torque. You need to keep the main body from rotating to get the most out of the wind turbine.
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Old 06-22-2014, 09:27 PM   #28 (permalink)
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counter rotating windmill, idea still seems a bit wack.

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