19 Dec 2025, 19:05 [ UTC - 5; DST ]
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 19:30 |
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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: [Sept 4th] He did do some static thrust measurements. He rigged it to the rear tire and measured force there and the force applied on the tires and then calculated to just over 800 lbs. 800 seems low for a 300+hp engine, and 175hp seems low for that engine- at least for the output he's trying to achieve out of it and the demonstrated takeoff performance on his televised takeoff runs. Still, the numbers don't add up no matter which way you look at them. We've already agreed in this thread that the engine installation badly needs a really good, experienced, resourceful, diesel engine tuner. I think it could benefit from a good propeller guy too. Just for comparison, some of the VAF guys get up to 800lbf static out of an O-360 with some reasonable prep and a good propeller. Different airplane, different engine and propeller, different cruise point, but it's a number. (The O-360 in a C172 gets more like 500-600.) It's not really an apples-to-apples comparison though, or apples-to-oranges, or apples-to-pomelos, or...
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 19:52 |
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Joined: 12/10/07 Posts: 36198 Post Likes: +14533 Location: Minneapolis, MN (KFCM)
Aircraft: 1970 Baron B55
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Username Protected wrote: Onlooker: Say, Pete, have you dynoed that engine?
Peter: No, but I compared it to a video of a 200hp SR20 that weighed 1000# less, at an airport 1000’ higher, with no knowledge of OAT, and got speeds that were within measurement error of that, so I figure I’m at about 300hp. Never look for factual data when uneducated wild guesses are available. Quote: He did cover the wheel wells, but even there he added weight when he didn’t have to. Why use 200mph tape when you can use sheets of aluminum? Seems to me that given Peter's affection for bailing wire+bubblegum fixes, I'm just surprised he didn't use duct tape.
_________________ -lance
It's easier to fool people than to convince them that they have been fooled.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 19:56 |
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Joined: 11/04/13 Posts: 211 Post Likes: +173 Company: USMCR Location: Ardmore, OK
Aircraft: PA-46T, B100, Tiger
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I am a fairly early deposit holder and I've been skeptical for some time, and still am, that I will ever own or fly a raptor.
But I received Peter's letter today, basically telling me to take my deposit back and he'd hold my place in line for me.
I know he's made plenty of mistakes and documented them. He's certainly not taken any of my advice about separating power plant and airframe and attacking separately. But he's been nothing but honest and beyond fair in his financial dealings with his deposit holders.
Several of you have made some pretty derogatory comments about his integrity and him attempting to make off with the deposits.
Now what do you have to say?
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 20:01 |
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Joined: 12/10/07 Posts: 36198 Post Likes: +14533 Location: Minneapolis, MN (KFCM)
Aircraft: 1970 Baron B55
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Username Protected wrote: Perhaps we should start a pool regarding the week he will have the 40TT completed? Does that count include high speed taxi, and ground effect hops?
_________________ -lance
It's easier to fool people than to convince them that they have been fooled.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 21:13 |
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Joined: 03/05/14 Posts: 2986 Post Likes: +3170 Company: WA Aircraft Location: Fort Worth, TX (T67)
Aircraft: 1969 Bonanza E33C
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Username Protected wrote: Several of you have made some pretty derogatory comments about his integrity and him attempting to make off with the deposits.
Now what do you have to say? It looks like I might be wrong and I hope I’m wrong. I also hope this contraption doesn’t kill anyone. I like being wrong when it comes to speculation of bad outcomes.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 21 Oct 2020, 21:18 |
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Joined: 02/17/09 Posts: 1958 Post Likes: +2319 Location: North Idaho!
Aircraft: F33A
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Username Protected wrote: Does that count include high speed taxi, and ground effect hops? The 40 hours of Phase 1 testing is where one must establish the numbers for the Operating Limitations. Best rate of climb Best angle of climb Best glide Stall clean Stall dirty Yada Yada EAA now has test cards for homebuilders to walk through Phase 1 step-by-step.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 22 Oct 2020, 07:29 |
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Joined: 05/11/10 Posts: 13425 Post Likes: +13271 Location: Indiana
Aircraft: Cessna 185
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Username Protected wrote: Several of you have made some pretty derogatory comments about his integrity and him attempting to make off with the deposits.
Now what do you have to say? It appears that my comparisons of Jim Bede were wrong. But I stand by my comparison of Peter with “Zoom” Campbell and others with personality disorders.
_________________ 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: 22 Oct 2020, 15:42 |
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Joined: 12/22/07 Posts: 14721 Post Likes: +16859 Company: Midwest Chemtrails, LLC Location: KPTK (SE Michigan)
Aircraft: C205
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Username Protected wrote: According to a post on HBA, a long while back the engine did get dynoed. The dyno said it made 175hp @3900 rpm. Peter’s explanation......the dyno is broken. Any idea if the 175HP is with or without the belt drive?
_________________ Holoholo …
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 22 Oct 2020, 19:08 |
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Joined: 10/07/18 Posts: 3722 Post Likes: +2660 Company: Retired Location: Columbus, Ohio
Aircraft: Baron 58, Lear 35
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I’d say without.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 22 Oct 2020, 20:36 |
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Joined: 07/06/14 Posts: 4151 Post Likes: +2861 Location: MA
Aircraft: C340A; TBM850
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Username Protected wrote: I’d say without. That's from this 2017 video, but it just shows the setup, not any dyno results. [youtube]https://youtu.be/lKsJZXBdNos[/youtube]
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 22 Oct 2020, 21:23 |
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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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I'm kinda surprised he hasn't rigged a poor man's dyno by placing a scale under each wheel, doing a high power turn, and deriving propeller torque from the difference between the left and right wheels. (Torque × rpm = horsepower). Point those wingtip cameras at the scale readouts and get real time data... it'd be fun to watch, even if it's not a very good idea.  (There might be some aerodynamic force from the induced flow of the propeller draw, so the results would be less than 100% accurate.)
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 26 Oct 2020, 19:41 |
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Joined: 09/29/10 Posts: 5660 Post Likes: +4882 Company: USAF Simulator Instructor Location: Wichita Valley Airport (F14)
Aircraft: Bonanza G35
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Username Protected wrote: Perhaps we should start a pool regarding the week he will have the 40TT completed? I’ll take “Never.” Where do I send my $5?
_________________ FTFA RTFM
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 27 Oct 2020, 04:38 |
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Joined: 03/15/16 Posts: 441 Post Likes: +349 Location: NC
Aircraft: Looking for one
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Username Protected wrote: Perhaps we should start a pool regarding the week he will have the 40TT completed? I’ll take “Never.” Where do I send my $5?
This is why you need a 3rd party doing the test evaluation. He has maybe 60 more seconds of flight time with his modifications, has no real clue on what the aeros are doing. But, he’s already moved on in his mind to the 40 hours and production.
I mean if the dang thing flew perfect, he would have to redesign the whole thing to get the weight at some reasonable level. He can’t even test the pressurization in this one.
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