|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/434 ; 364/187 ; 371/68 ; 318/564|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 105 인용 특허 : 9|
Each wing of an aircraft carries a set of five outboard spoilers, one inboard spoiler, one inboard aileron and one outboard aileron, together constituting the lateral control surfaces for the aircraft. Each spoiler is positioned by means of a single thread electrohydraulic servoactuator. Each outboard aileron is positioned by means of a one/one fail-operational electrohydraulic servoactuator. Each inboard aileron is positioned by a two/one fail-operational, electrohydraulic servoactuator. The control system is operated by four independent electrical cont...
In an aircraft, a fly-by-wire lateral control system, comprising: a symmetrical pair of lateral control surfaces, one on each wing of an aircraft; a plurality of two/one fail-operational, electrohydraulic actuators, each of which is drivingly connected to a separate lateral control surface, each said actuator comprising two hydraulic sections for redundant operation; four separate hydraulic pressure supplies; four separate electric control signal command channels; each actuator including control means for controlling each of its said two hydraulic sectio...