Archie wrote:
Surely by now, someone has lightened rotors to
some maximum amount.
A cursory look tells me a pound per rotor may be
feasible.
Any info on this?
Archie
Titanium has been tried but I think the thermal characteristics
were found to be less than Ideal.
I think a steel aluminum composite
design similar to the rotor housing might work. Better heat conduction
out near the apex seal slots might help cool the apex seal springs
better.
A two piece design 3D milled out of steel and laser welded
together on center line might also work.
Paul Lamar
The Aircraft Rotary Engine Newsletter. Powered by Linux.
http://home.earthlink.net/~rotaryeng/ http://www.linux.org