|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 24|
An aircraft flight control surface actuation system includes a plurality of electric motors-driven flap actuators, and a plurality of electric motor-driven slat actuators. The motor-driven actuators receive activation signals from flap and slat actuator controllers and is, in response to the activation signals, move the flaps and slats between stowed and a deployed positions. The flap and slat actuator controllers each include a plurality of independent actuator control channels that independently supply the activation signals to the motor-driven actuato...
We claim: 1. A flight control surface actuation system for aircraft having a plurality of flaps and slats on each aircraft wing, the system comprising: a plurality of electric motors, each electric motor coupled to receive activation signals and operable, upon receipt thereof, to supply a drive force; a plurality of flap actuators, each flap actuator coupled to receive the drive force from at least one of the electric motors, to thereby move a flap between a stowed and a deployed position; a plurality of slat actuators, each slat actuator coupled to rec...