Courierguy wrote:
Pretty heavy....
At 185 pounds for a 135HP blown motor with reduction gearbox, I am in the grey area . From the
Bearhawkin website http://www.bearhawkin.com/FAQ-Engines.html the following figures for some Lycoming powerplants.
Model Comp. Ratio HP RPM WeightO-320-A,E 7.00:1 150 2700 244
O-320-B,D 8.50:1 160 2700 255
O-320-H 9.00:1 160 2700 253
IO-320-B,C 8.50:1 160 2700 259
Model Comp. Ratio HP RPM WeightO-360-A 8.50:1 180 2700 269
O-360-E 9.00:1 180 2700 269
O-360-F 8.50:1 180 2700 270
IO-360-B 8.50:1 180 2700 270
IO-360-A,C 8.70:1 200 2700 293
At 8.50 Comp. Ratio Mogas is probably going to be okay. So pounds-horsepower comparisons are 185lbs-135HP, 255lbs-160HP, & 269lbs-180 HP
I think I’ll crack open another Budweiser, and think about it more.

Yeah a totally clean design would have been great. I read that a lot of their engines go into US Military apps (drones, UAVs) and that the testing and qualification process is really tedious. Maybe that's one reason for sticking with a legacy design