发明名称 |
LOAD OPTIMIZED REDUNDANT FLIGHT CONTROL SURFACE ACTUATION SYSTEM AND METHOD |
摘要 |
An aircraft flight surface control system and method simultaneously provides the benefits of both an active/active system architecture and an active/standby system architecture. The system is preferably implemented using hydraulic actuator assemblies and electromechanical actuator assemblies coupled to the same flight control surface. During normal system operations the electromechanical actuator assemblies are energized to supply a relatively minimal force to associated flight control surfaces. In effect, the electromechanical actuators, although energized, may be pulled along by the associated hydraulic actuator assemblies, until needed. Thus, the electromechanical actuator assemblies are controlled in a manner that closely resembles the active/standby architecture.
|
申请公布号 |
CA2622705(A1) |
申请公布日期 |
2008.08.27 |
申请号 |
CA20082622705 |
申请日期 |
2008.02.27 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
YOUNT, LARRY J;JACKSON, JOE;HANLON, CASEY;JOHNSON, ANDY |
分类号 |
B64C13/38 |
主分类号 |
B64C13/38 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|