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20 Oct 2025, 19:46 [ UTC - 5; DST ]


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 10:19 
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Having participated in the construction of a TIO 550 powered Lancair IVP, Dick Rutan's Voyager, and building 3 composite plansbuilt planes by myself, i suggest the odds of the Veloce 600 prototype flying in February 2025 is significantly less then zero, regardless of how many experienced builders they have on staff. Their composite shop, Volato Aeronaaves in Brazil, does know how to build molds, bag parts and bond structures...but that ain't the hard part.

I won't comment on the design, engineering, systems integration, costs or performance.


They have built quite a few airplanes that are flying. I am not defending them, but peter had zero credentials. I always cringe when I hear pressurized though, that is such a tall hill to climb.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 11:01 
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Sort of like BD-5 discusions used to be.

I came this close > < to putting money on a BD-12/14. Then the prototype failed on its first test flight and it was never heard from again.

I thought, ”That’s it? One bad flight and you say ‘Forget it?’ You just throw the parts back in the box and put the box in the Recycle?” Little Thirtysomething Stuey learned about business that week, without actually putting his own money on the line. The glory days of rec.aviation.homebuilt.


That one really was odd. I thought the same thing. Bede brought mock-ups to Osh and SnF for a year or two after the prototype crashed, but the project never moved forward.

And I loved rec.aviation.homebuilt and several other usenet forums...

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 12:21 
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> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.

The Doors/seals are a bear, but with todays modern composites I don't see the structure being that bad. (I really like the rutan boomerang doors for simplicity)

Also with modern brushless motors, one could probably do all electric pressurization.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 12:29 
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Username Protected wrote:
> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.


Which is why it is so effective as part of any snake oil sales pitch.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 12:46 
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Username Protected wrote:
> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.

The Doors/seals are a bear, but with todays modern composites I don't see the structure being that bad. (I really like the rutan boomerang doors for simplicity)

Also with modern brushless motors, one could probably do all electric pressurization.


Pressurization is amazing, I have been flying with it for 8 years in my Malibu. The problem is not pressurization, it’s the turbos, air conditioning, expensive windows/seals and de ice needed to fully support it. Any cocktail math on the amps required to run pressurization?


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 12:54 
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The specs for the Rutan Boomerang
https://en.wikipedia.org/wiki/Rutan_Boomerang
Aren't that far off...220knots and 2000nm range.


I have some time in the 'rang. By far the best flying qualities and most efficient of all of Burt's designs, and is waaaay better than any other fast glass homebuilts I've flown - and I've been fortunate enough to fly most of the piston and a couple of turbine models.

Remember, one of several companies Burt sold SCALED to was Beech under Linden Blue when they were still smitten with the Starship. There were aspirations for the 'rang far beyond yokels like me sniffing epoxy in their garages.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 13:02 
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Username Protected wrote:
Having participated in the construction of a TIO 550 powered Lancair IVP, Dick Rutan's Voyager, and building 3 composite plansbuilt planes by myself, i suggest the odds of the Veloce 600 prototype flying in February 2025 is significantly less then zero, regardless of how many experienced builders they have on staff. Their composite shop, Volato Aeronaaves in Brazil, does know how to build molds, bag parts and bond structures...but that ain't the hard part.

I won't comment on the design, engineering, systems integration, costs or performance.


They have built quite a few airplanes that are flying. I am not defending them, but peter had zero credentials. I always cringe when I hear pressurized though, that is such a tall hill to climb.


Yep, that's why I mentioned the IV P Lancair I helped with. I got a hell of an education on the complexity and difficulties pressurization brings to the party - especially in this case what's a glorified homebuilt. The turbine version of the A500 sent that talented team to school too.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 17:06 
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Username Protected wrote:
> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.

The Doors/seals are a bear, but with todays modern composites I don't see the structure being that bad. (I really like the rutan boomerang doors for simplicity)

Also with modern brushless motors, one could probably do all electric pressurization.


I bet electric motor pressurization would be pretty heavy, though, and there would be considerations for loss of electrical power.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 20:47 
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Username Protected wrote:
> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.

The Doors/seals are a bear, but with todays modern composites I don't see the structure being that bad. (I really like the rutan boomerang doors for simplicity)

Also with modern brushless motors, one could probably do all electric pressurization.


I bet electric motor pressurization would be pretty heavy, though, and there would be considerations for loss of electrical power.

The HP is pretty much directly proportional to the pressure difference and rate of airflow (leakage). Using 6psi differential and 200 CFM I get 6-7 HP depending on the blower's efficiency. That would take 160-200A at 28v. I picked 200 CFM because that's 10% of the CFM passing through an IO550 at 2500 RPM but I have no idea how much airflow is really needed. If you could seal the cabin enough that you only needed 50 CFM the required HP and electric power or current would be a fourth of that (1.5 HP and 40A @28v). The weight of a 1.5H electric blower could be as low as 10 lb.
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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 20:55 
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Boeing has electric pressurization on the 787 and probably all aircraft moving forward. Ducting hot bleed air all around, having heat exchange packs etc seems like a bad idea these days.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 21:01 
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Early King Airs had a hydraulic driven Roots supercharger blower in the nacelle like you see on hot rods. It utilized a pretty small engine driven hydraulic pump/motor combination.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 21:23 
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Username Protected wrote:
> I always cringe when I hear pressurized though, that is such a tall hill to climb.
Once you've flown pressurized you will always want it, opens up so many options/possibilities.

The Doors/seals are a bear, but with todays modern composites I don't see the structure being that bad. (I really like the rutan boomerang doors for simplicity)

Also with modern brushless motors, one could probably do all electric pressurization.


I bet electric motor pressurization would be pretty heavy, though, and there would be considerations for loss of electrical power.

For a piston engine, what is the perceived advantage? Presumably if you are flying high enough to need / want pressurization, the engine needs a turbocharger. If you have a turbocharger, then the cost of the pressure source is just the sonic venturi, which has no moving parts. How is replacing that with an electric blower helpful? I don't know about the optimization of the 787, where they sought to completely eliminate bleed air, but does the same logic apply to a piston airplane?

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 21:56 
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Username Protected wrote:
How is replacing that with an electric blower helpful?

No ducts, no air leaks. Electrical cables are way easier to route than air ducts. Pressure is generated where it's needed. Electricity could be fed from multiple alternators / engines.


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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 22:23 
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How is replacing that with an electric blower helpful?

No ducts, no air leaks. Electrical cables are way easier to route than air ducts. Pressure is generated where it's needed. Electricity could be fed from multiple alternators / engines.

I hear you, those ducts are a pain to route, and maybe they have to be replaced every 20-30 years. Ducts to the heater and defrost vents are more often an issue, and would still exist. How long will an electric blower last, and would it be lighter, or heavier?

Maybe it's typical that engineers become Luddites as they age. Bah humbug.

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 Post subject: Re: Raptor Aircraft 5 Seat Pressurized 3,600 NM Range Die
PostPosted: 15 Dec 2024, 23:06 
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On one or two testbeds we ran the bleed air through an ejector that mixed it with ambient air. This reduced the required amount of bleed air enough to be useful, but it wouldn't have worked as well with a higher pressure differenital or at higher altitudes.


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