27 Dec 2025, 00:36 [ UTC - 5; DST ]
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 08:29 |
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Joined: 10/05/11 Posts: 10333 Post Likes: +7422 Company: Hausch LLC, rep. Power/mation Location: Milwaukee, WI (KMKE)
Aircraft: 1963 Debonair B33
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Username Protected wrote: This was for a variable-pitch, constant-speed prop; assumes constant power from SL to 25,000ft, standard atmosphere, 150kts KCAS. % Thrust is the percentage of thrust compared to SL thrust.
% Thrust Altitude (Ft) KTAS 100.00% 0 150 59 92.4% 5,000 162 85.7% 10,000 174 78.3% 15,000 189 70.3% 20,000 205 62.3% 25,000 224
(Apologies for the formatting!)
So, even assuming constant power from SL to FL250, the thrust at FL250 was 62.3% of what it was at SL. Thank you. (What's the "59" to the right of the 150?)
_________________ Be Nice
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 14:41 |
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Joined: 11/06/10 Posts: 12201 Post Likes: +3086 Company: Looking Location: Outside Boston, or some hotel somewhere
Aircraft: None
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Username Protected wrote: I'm thinking of Ferris Beuller- Jim? Jim? Jim Bede?
Its all in the physics- how many BTUs do you need to get from diesel fuel to produce enough HP to get the speed you want? 7 gallons per hour ain't enough BTUs, period!
The bane of auto engine conversions has always been heat rejection reduction gearing longevity at high outputs they weren't designed to produce continuously. What is the HP the engine was designed to produce CONTINUOUSLY ? To say it can pull 280 HP on the dyno is one thing, to do it for hours on end is another world entirely. Actually most auto engines are tested to much worse conditions then our poor "certified aviation" engines. A fun way to waste twenty minutes: [youtube]https://youtu.be/8tEqwXrqzH4[/youtube] Based on some other forums, a few auto engineers have posted that the ecoboost video understates the actually abusive testing. But the reality just does not film as well. Tim
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 14:58 |
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Joined: 08/26/15 Posts: 10057 Post Likes: +10075 Company: airlines (*CRJ,A320) Location: Florida panhandle
Aircraft: Travel Air,T-6B,etc*
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Username Protected wrote: Actually most auto engines are tested to much worse conditions then our poor "certified aviation" engines. A fun way to waste twenty minutes: Thanks for digging this up. It's a popular myth in GA that modern auto engines just aren't physically tough and rugged, that their endurance testing is done at a light load, or that the bottom end can only hold up short bursts of full power. Not to knock you down, Cliff- you're absolutely right about gearboxes and heat rejection in auto conversions. A lot of amateur-built and professionally developed auto conversions have gone by the wayside over the decades for exactly those reasons.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 21:33 |
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Joined: 11/25/11 Posts: 9015 Post Likes: +17229 Location: KGNF, Grenada, MS
Aircraft: Baron, 180,195,J-3
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Username Protected wrote: Jim Bede, Raptor, Theodore R Wright III, Icon.......
Perhaps we're the fools they take us for. Amen, my friend. No truer words ever spoken. Your stock with me just went up. Jg
_________________ Waste no time with fools. They have nothing to lose.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 23:34 |
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Joined: 11/22/10 Posts: 1147 Post Likes: +350 Company: Stanford University Location: Brentwood, CA - C83
Aircraft: RV12, RV10
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Username Protected wrote: Talk is cheap. Are you buying his airplane? Better yet, investing in his company? Yup, #870. Let’s see you do that. Or just keep talking.
_________________ DISCLAIMER: I'm just a jaded engineer and my advice is worth exactly what you're paying for it...
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 13 Dec 2017, 23:51 |
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Joined: 05/11/10 Posts: 13431 Post Likes: +13276 Location: Indiana
Aircraft: Cessna 185
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Username Protected wrote: Talk is cheap. Are you buying his airplane? Better yet, investing in his company? Yup, #870. Let’s see you do that. Or just keep talking. I’ve put my money where my mouth is. This thing is a pig in a poke, so I’m not buying it. But if I’m wrong, that would be a good thing.
_________________ Stu F. "A cynic is a man who knows the price of everything and the value of nothing."
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 14 Dec 2017, 00:03 |
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Joined: 11/08/12 Posts: 12835 Post Likes: +5276 Location: Jackson, MS (KHKS)
Aircraft: 1961 Cessna 172
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Username Protected wrote: So, even assuming constant power from SL to FL250, the thrust at FL250 was 62.3% of what it was at SL. The Raptor guy is not factoring that in, which is a major oversight. Even after I pointed out to him, and he admitted I was right, the over-inflated performance claims remain on his website. Even given the most charitable interpretation, that he just didn't know, the fact that he hasn't revised his performance numbers is deceptive, IMHO.
I get that as the air gets thinner, the prop doesn't work as well. At least to the extent that a prop spinning in outer space will generate no thrust because there is no air. But a prop spinning in outer space requires essentially no power to turn because there's no drag. So if you're putting constant power into a prop and thrust decreases, where is that extra power going? Is this something fundamental that prop efficiency decreases with altitude or could you design a prop that works 100% at FL250 and sucks at MSL?
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 14 Dec 2017, 00:29 |
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Joined: 01/30/09 Posts: 3906 Post Likes: +2455 Location: $ilicon Vall€y
Aircraft: Columbia 400
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Username Protected wrote: So, even assuming constant power from SL to FL250, the thrust at FL250 was 62.3% of what it was at SL. The Raptor guy is not factoring that in, which is a major oversight. Even after I pointed out to him, and he admitted I was right, the over-inflated performance claims remain on his website. Even given the most charitable interpretation, that he just didn't know, the fact that he hasn't revised his performance numbers is deceptive, IMHO.
I get that as the air gets thinner, the prop doesn't work as well. At least to the extent that a prop spinning in outer space will generate no thrust because there is no air. But a prop spinning in outer space requires essentially no power to turn because there's no drag. So if you're putting constant power into a prop and thrust decreases, where is that extra power going? Is this something fundamental that prop efficiency decreases with altitude or could you design a prop that works 100% at FL250 and sucks at MSL?
The relationship is a bit harder to figure out.
If the propeller can control the RPM of the engine at altitude while the engine is producing x-HP, then it is doing its job and turning most of that power into thrust. The efficiency is hard to figure out, because it depends a lot on the propeller design, as well as the atmospheric conditions.
The prop will get less efficient at converting rotational power into thrust as the altitude increases, but exactly how that works out depends a lot on the prop design and the airspeed thus the aircraft's design also plays a role. If the propeller is designed for high-altitude flight, it may do a pretty good job of it, while not doing a good job at lower altitude. (they don't make props with flaps and slats)
Just like wings. As you climb higher and higher, the angle of attack increases and the drag increases and the lift decreases to the point where the L/D ratio doesn't allow the aircraft to climb any higher for a given power input.
The whole project seems entirely preposterous to me. It's one thing to mold an airframe and say it costs "x". But the tooling, building, engineering and other costs have to be spread out on volume.
Then there's all that paperwork that it takes to get an airplane to fly.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 14 Dec 2017, 10:38 |
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Joined: 03/01/14 Posts: 2301 Post Likes: +2087 Location: 0TX0 Granbury TX
Aircraft: T-210M Aeronca 7AC
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How many of you guys put money on the Elio? How’s that deal working out?
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 14 Dec 2017, 10:50 |
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Joined: 08/10/14 Posts: 1807 Post Likes: +881 Location: Northwest Arkansas (KVBT)
Aircraft: TBM850
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Username Protected wrote: On the prop efficiency thing: there's also gotta be some point where blade angle becomes too coarse. This discussion of prop efficiency is very interesting - I started a separate thread to discuss it (independent of the Raptor) here viewtopic.php?f=7&t=146724
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