公开(公告)号：US11473520B2

公开(公告)日：2022-10-18

申请号：US16827142

申请日：2020-03-23

Applicant: General Atomics Aeronautical Systems, Inc.

Inventor： Steven M. Weinzierl ,  Michael J. Fuchs ,  Alexander Seybold-Epting

IPC: F02D41/40 ,  B64D27/04 ,  B64D31/06 ,  F02C9/26 ,  F02D35/02 ,  F02D41/00 ,  F02D41/28

Abstract: A control system for an aero compression combustion drive assembly, the aero compression combustion drive assembly having an engine member, a transmission member and a propeller member, the control system including a sensor for sensing a pressure parameter in each of a plurality of compression chambers of the engine member, the sensor for providing the sensed pressure parameter to a control system device, the control system device having a plurality of control programs for effecting selected engine control and the control system device acting on the sensed pressure parameter to effect a control strategy in the engine member A control method is further included.