The present invention is an aero engine that is provided with compression combustion and weighs less than 725 lbs. The present invention is further a method of forming the aero engine.
申请公布号
EP2766588(A1)
申请公布日期
2014.08.20
申请号
EP20120839362
申请日期
2012.10.12
申请人
ENGINEERED PROPULSION SYSTEMS, INC.;WEINZIERL, STEVEN M.;FUCHS, MICHAEL J.
