|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/075R ; 244/078 ; 244/227 ; 244/228|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 29 인용 특허 : 8|
According to the invention, this system comprises:
[ What is claimed is:] [1.]1. A system for controlling an aerodynamic surface (1) of an aircraft comprising a deliberate-actuation member (6) available to a pilot and a hydraulic servocontrol (2, 5) controlled by said deliberate-actuation member (6), which additionally comprises:an electric machine (8) which can operate either as a motor or as a generator, the output of which is connected mechanically to said aerodynamic surface (1);an electrical power supply (11), which can power said electric machine (8) under the dependency of said deliberate-actuatio...