Duration is how you shift the powerband either lower or higher.   If you
want lots of torque at low RPM and don't care about high RPM (that's us),
you want short duration rather than long.   If you've upped the displacement
of the engine by boring and/or stroking, you'll probably need to compensate
for the lack of valve area by increasing the lift.  The stock cam with high
lift rockers is a step in the right direction, or the mildest of  "street"
cams.  Lift is a good thing, but too much of it can lead to accelerated
valve train wear.  I don't think valve train (cam, lifter, rockers) is the
big wear item on aircraft engines though, so that wouldn't be my determining
factor, personally.  You can just bolt on some higher lift rockers and get
the higher lift, but there are other ramifications (that's for Dan's sake).

Stock cams are something like 226 degrees of duration with .315" inches of
lift at the cam, and the mildest Engle 100 is 276 degrees of duration with
.374" of lift at the cam.  The Engle 100 would probably make a pretty good
cam for a 2180 airplane engine, but I'm just guessing.

I would think that Steve Bennett at www.GPASC.com would have a pretty good
idea what cam works best for aircraft use, and if he sells them, I'm sure
there's not much of a markup.  His prices have always struck me as being
very reasonable.

I've been told that Webcam makes something called the P-100 that's good for
aircraft use, but I just pulled that out of some pretty deep recesses, and
there may not actually be any such thing.  I think that's what was in the
Type 4 that I bought from Mark Stephens.

I just ran across this website at http://hometown.aol.com/dvandrews/cams.htm
that pretty well explains the relationships of duration and lift.

Mark Langford, Huntsville, Alabama
N56ML "at" hiwaay.net
see KR2S project at http://home.hiwaay.net/~langford


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