20 Apr 2024, 07:49 [ UTC - 5; DST ]
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 23 Jun 2020, 01:23 |
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Joined: 03/15/16 Posts: 450 Post Likes: +346 Location: NC
Aircraft: Looking for one
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Username Protected wrote: I have found my antidote for Raptor/Peter videos ... Scrappy/Patey is the antidote. I find Patey to be boring. First, he knows what he is doing. Second, he sticks to the old fashioned design first, then build second approach. There's no drama or excitement in that!
Also, I think the only way he gets so much done so fast is through cloning. I know there are at least two of him, likely more. It may or may not be illegal to clone yourself, but that is a moral grey area I am not quite ready to overlook.
You know the sad and funny thing. There are people that think that he’s going to fly it and turn around and make a production run. Oh, it’s going to be easy to shed 1000# from it too.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 23 Jun 2020, 02:00 |
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Joined: 06/17/14 Posts: 5012 Post Likes: +1951 Location: KJYO
Aircraft: C-182, GA-7
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Username Protected wrote: You know the sad and funny thing. There are people that think that he’s going to fly it and turn around and make a production run. Oh, it’s going to be easy to shed 1000# from it too. They can shed 850 by removing the pilot and passengers and even more if they drain all of the fuel. Problem solved.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 23 Jun 2020, 09:07 |
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Joined: 01/24/19 Posts: 398 Post Likes: +187 Location: Birmingham
Aircraft: Vans RV-6; Archer II
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Username Protected wrote: My Audi 2.7T Twin Turbo engine went to 241k before it gave up the ghost.... Wow that’s great news for the raptor program. If he’s taxied 20 miles in his demo vids to date, we can look forward to years of taxi testing.
I needed a good laugh this morning and this was it.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 23 Jun 2020, 20:47 |
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Joined: 10/06/16 Posts: 114 Post Likes: +183 Location: Tucson, AZ (winter) & Brunswick, ME (summer)
Aircraft: T210, Aerostar 702P
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Quote: I'm not sure why everyone gets hung up on the need for dual FADEC. When's the last time you saw a "computer" failure in a car engine? Put me down for just one, in a Honda Civic FWIW. It was a very reliable car, but the engine control computer abruptly died about mid-life. Mark
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 00:23 |
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Joined: 05/01/14 Posts: 8792 Post Likes: +13534 Location: Операционный офис КГБ
Aircraft: TU-104
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Username Protected wrote: Quote: I'm not sure why everyone gets hung up on the need for dual FADEC. When's the last time you saw a "computer" failure in a car engine? Put me down for just one, in a Honda Civic FWIW. It was a very reliable car, but the engine control computer abruptly died about mid-life. Mark I lost one due to a lightning strike. Not even a direct hit, but very close. Luckily there was a fallback limp mode. I would prefer some form of backup in an aircraft engine, considering the relatively low cost and insignificant weight penalty.
_________________ Be kinder than I am. It’s a low bar. Flight suits = superior knowledge
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 00:48 |
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Joined: 12/07/17 Posts: 7035 Post Likes: +5807 Company: Malco Power Design Location: KLVJ
Aircraft: 1976 Baron 58
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Username Protected wrote: I lost one due to a lightning strike. Not even a direct hit, but very close. Luckily there was a fallback limp mode. I would prefer some form of backup in an aircraft engine, considering the relatively low cost and insignificant weight penalty.
That’s the thing though. A modern ECU is not an negligible cost or weight penalty. It depends on literally dozens of sensors all around the engine. Now you have to engineer in either dual sensors or dual pickups on single sensors and hope whatever took out the first ECU didn’t take out any of the important sensors. Then there are the outputs. A modern ECU controls all sorts of things from spark, injection, and valve timing in spark ignition engines to as many as 20 separate fuel injection pulses per cycle in compression ignition engines. How is redundancy going to be handled there? Dual valve trains? Dual injectors and high pressure fuel pumps? The thing will never fly. No, give me a proven engine design with known good single systems that is mass produced for much lower cost than what we have now. If You want any power plant redundancy in a modern engine the way to get it is a second complete engine on the other wing.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 09:04 |
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Joined: 03/01/14 Posts: 2152 Post Likes: +1643 Location: 0TX0 Granbury TX
Aircraft: T-210M Aeronca 7AC
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But... but.... it has a chute.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 09:21 |
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Joined: 11/22/12 Posts: 2597 Post Likes: +2356 Company: Retired Location: Lynnwood, WA (KPAE)
Aircraft: 1993 Bonanza A36TN
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Username Protected wrote: I lost one due to a lightning strike. Not even a direct hit, but very close. If You want any power plant redundancy in a modern engine the way to get it is a second complete engine on the other wing. But a second engine would also have been "very close" and susceptible to that lightning strike. Redundancy doesn't help when a single event takes out both.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 09:22 |
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Joined: 05/11/10 Posts: 12403 Post Likes: +11412 Location: Indiana
Aircraft: Cessna 185, RV-7
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Username Protected wrote: But... but.... it has a chute. Excellent point. If it flies once, gets to chute height at less than max chute speed, deploys the chute and comes down without hurting anyone, a certain type of aviation enthusiast might call that a total success!
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 09:36 |
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Joined: 12/07/17 Posts: 7035 Post Likes: +5807 Company: Malco Power Design Location: KLVJ
Aircraft: 1976 Baron 58
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Username Protected wrote: But a second engine would also have been "very close" and susceptible to that lightning strike. Redundancy doesn't help when a single event takes out both. So would anything you added to the first engine for “redundancy.” If we’re ever going to get away from flying behind Stone Age engines were going to have to get over the irrational fear of the engines getting killed by freak events.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 10:12 |
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Joined: 05/01/14 Posts: 8792 Post Likes: +13534 Location: Операционный офис КГБ
Aircraft: TU-104
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Username Protected wrote: But a second engine would also have been "very close" and susceptible to that lightning strike. Redundancy doesn't help when a single event takes out both. So would anything you added to the first engine for “redundancy.” If we’re ever going to get away from flying behind Stone Age engines were going to have to get over the irrational fear of the engines getting killed by freak events.
A decent fall back system doesn’t need to be as complex and capable as the primary ECU. A Stone Age limp mode that offers significantly less power and lower fuel economy, but will get me 25-50 miles to a safe landing is much better than becoming an insta-glider or pulling the chute handle.
_________________ Be kinder than I am. It’s a low bar. Flight suits = superior knowledge
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 10:47 |
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Joined: 10/28/12 Posts: 3338 Post Likes: +2754 Company: IBG\Altapraem M&A Advisors Location: Kerrville, TX (60TE)
Aircraft: SR22-G2 GTS
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Username Protected wrote: So would anything you added to the first engine for “redundancy.”
If we’re ever going to get away from flying behind Stone Age engines were going to have to get over the irrational fear of the engines getting killed by freak events.
A decent fall back system doesn’t need to be as complex and capable as the primary ECU. A Stone Age limp mode that offers significantly less power and lower fuel economy, but will get me 25-50 miles to a safe landing is much better than becoming an insta-glider or pulling the chute handle.
Crazy idea maybe, certainly would cost some payload - what about a stowable electric motor that would deploy on demand, one of those used by motor gliders but scaled up a bit?
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 11:06 |
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Joined: 08/26/15 Posts: 9543 Post Likes: +8779 Company: airlines (*CRJ,A320) Location: Florida panhandle
Aircraft: Travel Air,T-6B,etc*
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Username Protected wrote: Crazy idea maybe, certainly would cost some payload - what about a stowable electric motor that would deploy on demand, one of those used by motor gliders but scaled up a bit? Motor plus fuel (battery), here are some latest and greatest numbers to kick around in your head. The new Pipistrel electric airplane just got its Euro type certificate (great news for tech fans!). The motor is about 80hp and weighs 20kg (44lbs), dunno if that's with the propeller too. The battery pack weighs a bit less than 300lbs and holds 21kWh. 21kWh is about 28 horsepower·hours, which is about what two gallons of avgas will yield in a typical aviation piston engine. Not saying whether it's a crazy idea or a brilliant idea, like I said those are just numbers for the thought experiment. They're a realistic estimate of what you'd have to do to make it work- and what the tradeoff would be in terms of what weight or payload you'd have to sacrifice from the rest of the airplane.
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 11:45 |
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Joined: 06/17/14 Posts: 5012 Post Likes: +1951 Location: KJYO
Aircraft: C-182, GA-7
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Pound for pound, liter for liter, and for the sake of safety of a Class 4 Flammable, nothing beats dinosaur juice!
Is 21KWh about $2.94?
It would not hurt my feelings just toying around to build time at that rate. Though those batteries have to be pricey to replace. A few of the LSAs And electric planes back at Oshkosh 2017 had replacement battery packs. I watched 6 people load the Pipistrel into a semi with the wings off and assuming the battery pack was out.
I am sad that Airbus stopped eFan development. That looked like cheap multi time!
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Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die Posted: 24 Jun 2020, 12:07 |
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Joined: 08/26/15 Posts: 9543 Post Likes: +8779 Company: airlines (*CRJ,A320) Location: Florida panhandle
Aircraft: Travel Air,T-6B,etc*
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Username Protected wrote: Pound for pound, liter for liter, and for the sake of safety of a Class 4 Flammable, nothing beats dinosaur juice!
Is 21KWh about $2.94?
It would not hurt my feelings just toying around to build time at that rate. Though those batteries have to be pricey to replace. A few of the LSAs And electric planes back at Oshkosh 2017 had replacement battery packs. I watched 6 people load the Pipistrel into a semi with the wings off and assuming the battery pack was out.
I am sad that Airbus stopped eFan development. That looked like cheap multi time! Oh yes, I absolutely agree with you on all of your points. I do find it appealing, the idea of an electric runabout/motorglider that makes only propeller noise- how cool would that be even taxiing the thing in near silence, including shutting down the prop at the hold short line while you're waiting your turn? But the cost structure and the performance numbers are undeniable. It's not for me... not at this stage of the game anyway.
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