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#11
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Small machines using vectored thrust are going to be noisy, no
matter what, and inefficient (how efficient is a Harrier?). Fly-by-wire isn't cheap, either (what's an F-16 worth?). These small machines are no doubt possible, if enough money is spent, but what's the market going to look like for a two-place model that costs $15 million and gets 1/2 mile per gallon, giving it a 50-mile range, say? And wakes up half the city? And don't get me started about electric motors and their weight and the generators needed and all that. Thrust is most efficient when it's generated by large-diameter slow-turning props, rotors or fans. Small units have to spin at high speed, losing way too much power to drag. A 400-hp helicopter makes way more thrust than a 400-hp aircraft engine and prop. Airliners use big fans now instead of the old straight turbojets. All of it proves that small-diameter air movers are not good and unless there's a powerplant developed that weighs nearly nothing and turns out huge hp at near 100% efficiency, these little machines will remain a dream, just like powered flight was a dream until metallurgy and fuels developed to the point that the Wrights could build an engine that would actually fly. Dan |
#12
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On Mon, 7 Mar 2005 at 18:59:18 in message
, Larry Dighera wrote: I don't see the control system as being that difficult a hurdle. After all, the Harrier is able to hover with only two nozzles. I think you will find that the Harrier has four main swivelling nozzles, the front pair are cold air from the compressors, the rear pair are hot exhaust from the turbine. In addition it has air driven control jets at nose, tail and both wing tips. All of then are required for hovering flight. -- David CL Francis |
#13
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On Mon, 7 Mar 2005 at 14:19:31 in message
, Montblack wrote: Reason I've read for its demise was fear of noise pollution (Right, like a 1st generation 707 wasn't loud? And what about those 2 Harrier jump-jet at OSH last year?). Another reason I've read for the project's cancellation was British Govt. inside politics - with Fairey being outside. Those people who heard one can testify that it was extremely loud. As to the politics I cannot say. I say 'those people' because I have a memory of hearing the ear-splitting noise at a Farnborough Air show. But it could have been the Flying Bedstead. I saw then both but did I see both of them fly? - not quite sure of this because of it being around 50 years ago and I am now much older. :-( -- David CL Francis |
#14
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![]() "David CL Francis" wrote Those people who heard one can testify that it was extremely loud. As to the politics I cannot say. I say 'those people' because I have a memory of hearing the ear-splitting noise at a Farnborough Air show. If it is the Harrier you are talking about, I can testify to the fact that they are very loud, having been as close as 75 feet to one in hover. Ear splitting is more accurate. But the coolness factor still places it *way* up there. g -- Jim in NC |
#15
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On Tue, 08 Mar 2005 21:02:35 GMT, David CL Francis
wrote in :: On Mon, 7 Mar 2005 at 18:59:18 in message , Larry Dighera wrote: I don't see the control system as being that difficult a hurdle. After all, the Harrier is able to hover with only two nozzles. I think you will find that the Harrier has four main swivelling nozzles, the front pair are cold air from the compressors, the rear pair are hot exhaust from the turbine. In addition it has air driven control jets at nose, tail and both wing tips. All of then are required for hovering flight. I've not noticed any other Harrier nozzles than one on each side. Thanks for the information. I suppose in theory it would be possible to hover with only one nozzle. |
#16
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Recently, Larry Dighera posted:
On Sat, 05 Mar 2005 17:26:33 GMT, "Colin W Kingsbury" wrote in . net:: Sure, it might fly, but who wants a machine with the fuel burn of an old Lear (at low altitude), the maintenance costs of a big Sikorsky, and the payload of a 172? [...] It's a start. It portends the future. It's going to need development and refinement, but I believe these vectored thrust machines will eventually be successful in achieving flight and eventually public acceptance. I just wonder *where* these things might be operated. Certainly not down any city street or through any neighborhood? Neil |
#17
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On Wed, 09 Mar 2005 02:14:35 GMT, "Neil Gould"
wrote in : : I just wonder *where* these things might be operated. Certainly not down any city street or through any neighborhood? I know what you mean. And I think you've touched on the cause of their delayed development: a narrow range mission goals. I have read that a primary mission goal would be for rescue of personnel from sky scraper windows where the rotor disk of helos complicates getting close enough for success. I'm not sure that would be a viable mission either given the likelihood the down wash would possibly suck out the glass facade. The military funded some SoloTech research, so I would expect that the concept of zooming soldiers around the battlefield or over mine fields and water has some merit. The lack of suitable missions, other than sheer joy of operation, seems to be a significant hurdle. |
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