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(B2431) wrote in message ...
From: Richard Lamb snip The problem with ducted fans is the increased weight and increased drag really don't help that much. Also, there are efficiency issues. I have thought some about a novel fan arrangement though. This is for a high speed twin engined airplane with the engines mounted on plyons back near the tail. Similar to jet engines on airliners. The set up uses a 50 to 60 HP Rotax 2 stroke turning an unducted multiblade fan - direct drive. The fan pitch would be electrically controlled - virtual constant speed - single power lever per engine. That means the fan would spin 5 to 6 thousand RPM, have short fat blades, have horrible effeciency at low speeds, but the idea is to go like stink at cruise. Oh well, daydreaming doesn't cost much... Richard I have been looking into a similar set up for years. The only successful set up I have ever personally seen is on a gyro. I have considered a constant RPM system as well as inflight adjustable pitch. Both are too complicated, heavy and expensive for a system where the prop efficiency is down to the lower 60s. Things are stranger than you realize g http://www.visionpacific.com/humming...DuctMyths.html The problem with multi-wing fans is that the blades have a lot of camber/concavity. THey are better at generating pressure than at moving air. Serious hovercraft enthusiasts have been to make composite replacements for better performance. Not very certified. The new 4 stroke snow-machine motors look great except 1. Still available only 90 hp and above. 2. I cannot afford one. Dan, U.S. Air Force, retired |
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From: (Ralph DuBose)
snip The problem with multi-wing fans is that the blades have a lot of camber/concavity. THey are better at generating pressure than at moving air. Serious hovercraft enthusiasts have been to make composite replacements for better performance. Not very certified. The new 4 stroke snow-machine motors look great except 1. Still available only 90 hp and above. 2. I cannot afford one. http://www89.pair.com/techinfo/MassFlow/ductbook.htm http://www.cds.caltech.edu/~murray/projects/dfan/ http://www.bridgingworlds.com/DUCKT.HTM Dan, U.S. Air Force retired |
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(B2431) wrote in message ...
From: (Ralph DuBose) snip The problem with multi-wing fans is that the blades have a lot of camber/concavity. THey are better at generating pressure than at moving air. Serious hovercraft enthusiasts have been to make composite replacements for better performance. Not very certified. The new 4 stroke snow-machine motors look great except 1. Still available only 90 hp and above. 2. I cannot afford one. http://www89.pair.com/techinfo/MassFlow/ductbook.htm http://www.cds.caltech.edu/~murray/projects/dfan/ http://www.bridgingworlds.com/DUCKT.HTM Thanks for the links. The kind of ducted fan he is working with seems quite different than what I am familiar with. Hovercraft want better static thrust and much lower tip speeds for noise suppression.. My hovercraft has a 36 in duct, tip speeds around 500ft per sec, 65 hp, and around 250 lb. thrust. Dan, U.S. Air Force retired |
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On 04 May 2004 07:30:44 GMT, (B2431) wrote:
From: Richard Lamb snip The problem with ducted fans is the increased weight and increased drag really don't help that much. Also, there are efficiency issues. I have thought some about a novel fan arrangement though. This is for a high speed twin engined airplane with the engines mounted on plyons back near the tail. Similar to jet engines on airliners. The set up uses a 50 to 60 HP Rotax 2 stroke turning an unducted multiblade fan - direct drive. The fan pitch would be electrically controlled - virtual constant speed - single power lever per engine. That means the fan would spin 5 to 6 thousand RPM, have short fat blades, have horrible effeciency at low speeds, but the idea is to go like stink at cruise. Oh well, daydreaming doesn't cost much... Richard I have been looking into a similar set up for years. The only successful set up I have ever personally seen is on a gyro. I have considered a constant RPM system as well as inflight adjustable pitch. Both are too complicated, heavy and expensive for a system where the prop efficiency is down to the lower 60s. Things are stranger than you realize g http://www.visionpacific.com/humming...DuctMyths.html Dan, U.S. Air Force, retired Didn't McD-D test one on a Super 80? I think the tests were slightly positive, but the costs prohibitive. I remember this from an old Av Leak. -- dillon When I was a kid, I thought the angel's name was Hark and the horse's name was Bob. |
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#7
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B2431 wrote...
Didn't McD-D test one on a Super 80? I think the tests were slightly positive, but the costs prohibitive. I remember this from an old Av Leak. I remeber seeing a video of an open fan on the starboard engine of one. I have no idea of the status. I've got a couple of pictures of it in the Long Beach haze. It was noisy as all get-out - one of the reasons it was abandoned, IIRC Dave 'WHAT?!' Hyde |
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