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Corvair conversion engines



 
 
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  #1  
Old January 19th 06, 03:40 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

But would you have to replace the engine?
Maybe just a crank overhaul every 4-500 hours, in the middle of
winter, after a good snow storm, nothing else to do.

  #2  
Old January 19th 06, 05:00 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines


I just think hanging a prop on a crank directly is a non-starter in
the first place...especially on a crank and case not specifically
designed for this in the first palce. Maybe a good redrive and flywheel
would be a better way to go?

  #3  
Old January 19th 06, 08:35 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines


"Bret Ludwig" wrote in message
oups.com...

I just think hanging a prop on a crank directly is a non-starter in
the first place...especially on a crank and case not specifically
designed for this in the first palce. Maybe a good redrive and flywheel
would be a better way to go?


That is my opinion, also.
--
Jim in NC

  #4  
Old January 19th 06, 11:38 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

When it really gets down to facts, most often aircraft engines really
don't cost any more than auto conversions and the aircraft engine
appears to be more reliable.
No redrives needed, redundant ignition and lots of other things that
makes them better.

I was a firm believer in auto engine conversions but i haven't seen many
last a long time except for the Subaru and Rotax engines.



Morgans wrote:

"Bret Ludwig" wrote in message
oups.com...


I just think hanging a prop on a crank directly is a non-starter in
the first place...especially on a crank and case not specifically
designed for this in the first palce. Maybe a good redrive and flywheel
would be a better way to go?



That is my opinion, also.

  #5  
Old January 19th 06, 11:45 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines


wrote in message ...
When it really gets down to facts, most often aircraft engines really
don't cost any more than auto conversions and the aircraft engine
appears to be more reliable.
No redrives needed, redundant ignition and lots of other things that
makes them better.

I was a firm believer in auto engine conversions but i haven't seen many
last a long time except for the Subaru and Rotax engines.


There are many V-6's running, some significant numbers, time wise.

VW's flying all over the place.

Mercedes diesels in what, Thielert brand name?

Oh, by the way, Rotax is NOT an auto conversion.
--
Jim in NC
  #7  
Old January 20th 06, 02:06 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

wrote:
On Thu, 19 Jan 2006 17:38:52 -0600,
wrote:


When it really gets down to facts, most often aircraft engines really
don't cost any more than auto conversions and the aircraft engine
appears to be more reliable.
No redrives needed, redundant ignition and lots of other things that
makes them better.

I was a firm believer in auto engine conversions but i haven't seen many
last a long time except for the Subaru and Rotax engines.



I bought two 3.8L Ford V6's for $150 each, bought new pistons from
Roush racing, new rings, had the best block shot peened bored and
honed, had the best crank turned and nitrided, bought new bearings,
new cam, new distributer with two sensors installed for dual ignition,
new pistons, new timing gears and chain, planed the heads, had four
new intake valves installed and new guides installed as well, new
valve springs, roller rockers, new lifters, new carburetor, old style
NWAero psru, ARP studs for the crank bearings and cylinderheads,
fabricated my own headers, and STILL spent only about $6,000.

Now, how much does one pay for a remanufactured aircraft engine of 200
horsepower?

Corky Scott


I don't think there's any dispute over the relative cost of engines.
This issue is longevity and whether one wants to fly an airplane with an
engine that might not make it to the next airport.




  #8  
Old January 20th 06, 05:27 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

On Fri, 20 Jan 2006 08:06:33 -0600, Cal Vanize
wrote:

I don't think there's any dispute over the relative cost of engines.
This issue is longevity and whether one wants to fly an airplane with an
engine that might not make it to the next airport.


Cal, the statement I was responding to was from the guy who said that
auto engines end up essentially costing as much as an aircraft engine.
I was posting my actual costs to suggest that the costs are, or can
be, very much lower for the auto engine conversion than for a rebuilt
aircraft engine.

But I chose to do all the work, except for the machining of the engine
parts, myself. If you do not wish to put in that kind of time, or do
not have the knowledge to do so, then the options tend to be a lot
more expensive.

Buying a firewall forward package and simply bolting it in place and
connecting the wires and fuel lines will of course cost a bunch more
than doing everything yourself. Perhaps this is what that gentleman
was talking about.

Corky Scott
  #9  
Old January 21st 06, 07:32 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

On Fri, 20 Jan 2006 08:06:33 -0600, Cal Vanize
wrote:



I don't think there's any dispute over the relative cost of engines.
This issue is longevity and whether one wants to fly an airplane with an
engine that might not make it to the next airport.


You mean like a Lycoming? or an old Franklin?




  #10  
Old January 20th 06, 07:17 PM posted to rec.aviation.homebuilt
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Default Corvair conversion engines

wrote)
I bought two 3.8L Ford V6's for $150 each, bought new pistons from Roush
racing, new rings, had the best block shot peened bored and honed, had the
best crank turned and nitrided, bought new bearings, new cam, new
distributer with two sensors installed for dual ignition, new pistons, new
timing gears and chain, planed the heads, had four new intake valves
installed and new guides installed as well, new valve springs, roller
rockers, new lifters, new carburetor, old style NWAero psru, ARP studs for
the crank bearings and cylinderheads, fabricated my own headers, and STILL
spent only about $6,000.



Why not fuel injected?

Also, is that two for $3K each?

What does that setup weigh?

Was matching a prop to your engine a problem? 3 bladed prop?

Curious...


Montblack

 




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