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A lifter has a sharp wire and a blunt one, the sharp one ionises the air, which is attracted to the blunt electrode. If it didn't neutralise there wouldn't be any thrust. I think maybe Scott is confusing this with ion propulsion.
Registered Member #531
Joined: Sat Feb 17 2007, 10:51AM
Location: Burlington, Vermont
Posts: 125
Perhaps I am to an extent. I'll review and recant as needed.
EDIT:
And recant I shall. Sorry Patrick, I was not remembering the lifter correctly. Assuming all the ions are collected you are correct. The thin air / glow discharge problem will still be there though.
Alexander - It's unclear to me how neutralization is responsible for the thrust. The second electrode would seem to me to provide a preferred direction to the ion drift, yielding net thrust, and control the buildup of a deleterious space charge. Maybe I am still confused? (not an unusual occurrence)
It's my understanding that any charge that escapes the blunt electrode creates an equal and opposite impulse on it's journey away from the lifter.
I think you may also have a point about charge buildup on the craft, if this happens it will pull earthwards by electrostatics. Not sure of the magnetude of this effect. Additional lifter segments operating on reverse polarity may help.
This is such a cool project but the numbers I'm getting from web searches look horrendous, 90W lifts 2 ounces. Would it be cheating to make the craft neutrally buoyant first with a helium cell?
Registered Member #531
Joined: Sat Feb 17 2007, 10:51AM
Location: Burlington, Vermont
Posts: 125
My understanding is that the thrust is due to ionized air molecules colliding with neutrals and imparting momentum to said neutrals as the ionized fellow drifts in the field toward the blunt electrode. The purpose of the blunt electrode appears to be field shaping for directing of the net drift. From a thrust generation standpoint I don't see that it makes any difference as to whether that ionized molecule is scavenged by the blunt electrode or if it continues off to infinity as far as the system is concerned.
Of course from the standpoint of Patrick's self contained system, the blunt electrode needs to collect the majority of the carriers else things will eventually stop working.
You are right about the efficiencies, absolutely abysmal. I would say Patrick has his work cut out for him.
Registered Member #2431
Joined: Tue Oct 13 2009, 09:47PM
Location: Chico, CA. USA
Posts: 5639
scott fusare wrote ...
My understanding is that the thrust is due to ionized air molecules colliding with neutrals and imparting momentum to said neutrals as the ionized fellow drifts in the field toward the blunt electrode. The purpose of the blunt electrode appears to be field shaping for directing of the net drift. From a thrust generation standpoint I don't see that it makes any difference as to whether that ionized molecule is scavenged by the blunt electrode or if it continues off to infinity as far as the system is concerned.
Of course from the standpoint of Patrick's self contained system, the blunt electrode needs to collect the majority of the carriers else things will eventually stop working.
You are right about the efficiencies, absolutely abysmal. I would say Patrick has his work cut out for him.
the purpose of the sharp electrode is to glow and generate ions through homo-nuclear clevage, at as low of a voltage as possible. the purpose of the lower rounded electrode is prevent the generation of counter current which would cancel the upper electrodes contribution.
Alexander wrote ...
It's my understanding that any charge that escapes the blunt electrode creates an equal and opposite impulse on it's journey away from the lifter.
I think you may also have a point about charge buildup on the craft, if this happens it will pull earthwards by electrostatics. Not sure of the magnetude of this effect. Additional lifter segments operating on reverse polarity may help.
This is such a cool project but the numbers I'm getting from web searches look horrendous, 90W lifts 2 ounces. Would it be cheating to make the craft neutrally buoyant first with a helium cell?
As for your efficiency points your absolutely right, the energy efficiency is apalling , but ive got a trick hidden up my sleeve, if im right, IF im right i can make these devices small enough to replace conventional jet engines, but more energy efficent per unit of J/kg of chemical propellent/ energy conversion source.
i have some ideas that need to be demonstrated/validated via my HV oscilloscope probe.... and aerodynamic instruments... hence the 1 year spent building and figuring out the HV probe, and the past 16 years ive been doing the math and physics on the DeSeversky idea.
Registered Member #1938
Joined: Sun Jan 25 2009, 12:44PM
Location: Romania
Posts: 701
Patrick wrote ...
As for your efficiency points your absolutely right, the energy efficiency is apalling , but ive got a trick hidden up my sleeve, if im right, IF im right i can make these devices small enough to replace conventional jet engines, but more energy efficent per unit of J/kg of chemical propellent/ energy conversion source.
Would be nice to see this working. As we're all skeptical about this idea, I can only encourage you to build the device and prove it is working. Good luck !
Registered Member #531
Joined: Sat Feb 17 2007, 10:51AM
Location: Burlington, Vermont
Posts: 125
Patrick wrote ...
the purpose of the sharp electrode is to glow and generate ions through homo-nuclear clevage, at as low of a voltage as possible. the purpose of the lower rounded electrode is prevent the generation of counter current which would cancel the upper electrodes contribution.
"Homo-nuclear cleavage"? You are referring to dissociation of the diatomic gasses? Electron attachment processes are dominant, lots and lots of info out there on atmospheric ions. Of course, having worked on the math and physics for 16 years, you should already have this worked out
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