LSx in a plane
The main problem I can think of is that LSx engines run over 6k rpm, whereas airplane engines usually run in the 3k rpm range.
Is it possible to build a BIG stroker LS2 in the 402 range with small ports that could make peak power at 32-3500 rpm?
It would be really cool to have a lightweight V8 with fuel injection (fuel injected airplane engines are CRAZY expensive). Is there any other real setback that we would come across in doing this?
Im sure a good porter could make a small valve, small port (matterial would be added of course) head, that would peak below 4k rpm which would have a good life at 4k rpm.
Any thoughts?
This seems a little high for a prop engine, but is crazy cool. Its designed by an Indy car engineer.
Trending Topics
Be sure you put it into a "full acrobatic" capable airframe. We're gonna wanna see videos too!
The Best V8 Stories One Small Block at Time
The main problem I can think of is that LSx engines run over 6k rpm, whereas airplane engines usually run in the 3k rpm range.
Is it possible to build a BIG stroker LS2 in the 402 range with small ports that could make peak power at 32-3500 rpm?
It would be really cool to have a lightweight V8 with fuel injection (fuel injected airplane engines are CRAZY expensive). Is there any other real setback that we would come across in doing this?
Im sure a good porter could make a small valve, small port (matterial would be added of course) head, that would peak below 4k rpm which would have a good life at 4k rpm.
Any thoughts?
The Lancair 420P has an aluminum twin-turbo 350 Chevy making 420 hp.
Call Lancair and they'll give you some good info. I have a complete write-up on the plane and engine, it uses a 5-bladed constant speed prop. If I can find it I'll scan it and e-mail them to you.
.
The main problem I can think of is that LSx engines run over 6k rpm, whereas airplane engines usually run in the 3k rpm range.
I'd expect that you'd look into maximizing whatever power is available in that mid-rpm range. Figure on cruising in the 2500 to 3000 rpm range. And set it up so that you can run it up to 4500 to 5000 rpm for takeoff power and other "special" situations that require extra power which would be the "sprint" rating.
Gear reduction and variable pitch would be mandatory. Not sure about how constant speed is done, nor do I know the advantages / disadvantages of it, so I can't comment on that aspect. I expect that a dry sump would only be necessary if you're going to do funny things with the airframe (acrobatics and such), otherwise I'd bet a wet sump would probably do ok.
Lastly, you would want to do something to boost the engine, to make up for lazy performance at altitude (could be lazy to downright lousy). Turbos would be the preferred route, but a supercharger could do the deed also (did on all kinds of WWII aircraft).
The area that a automobile engine falls short of the aircraft designs is redundancy. A typical flat 4 or flat 6 airplane engine has 2 complete ignition systems (2 mags, 2 sets of wires & plugs). And due to the simplicity of carbs, they don't have much need for redundancy there. But an EFI system has a bunch of components, all of which have the possiblility of failure (injectors, fuel pumps, controllers, sensors, etc). That's the only side of doing an automotive to aircraft conversion that would make me nervous. At least with a car / truck / boat conversion you can pull over!
Sidebar: Something I stumbled upon a while ago was one of the last big piston engines for aircraft (commercial stuff, just before they went to jets). They were turbo compounds. Think big multi-row radial with multiple turbocharger hot sections. But instead of the hot section driving compressors, they were geared to the output shaft. They used multi-speed, multi-stage centrifugal superchargers for boost. Pretty impressive, since they were getting something like 3500hp out of them. Talk about using all the technology available. Regardly, it was pretty neat reading.
'JustDreamin'







