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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/76R ; 244/227 ; 244/78 ; 244/221|
|우선권정보||DE-3631063 (1986-09-12); DE-3638820 (1986-11-13)|
|발명자 / 주소||
|출원인 / 주소||
|인용정보||피인용 횟수 : 30 인용 특허 : 0|
A vertical rudder control and drive system for an aircraft, such as an airplane, is equipped with electrically controllable vertical rudder drive systems on each side of the aircraft. Additionally, the control system is equipped with a mechanically controllable auxiliary drive system for the operation of the vertical rudder in response to foot pedals operated by the pilot when there should be a failure in the electrically controlled drive systems. A mechanical control signal transmitting link is provided between the foot pedals and the hydro-mechanical d...
A control system for controlling a vertical rudder of an aircraft, comprising pilot operated pedal means for generating a mechanical control signal, autopilot computer means for generating vertical rudder control signals, three hydraulic drive systems operatively connected to the vertical rudder, two electrical signal control channels for electrically transmitting rudder control signals from said autopilot computer and/or from sensors at pilot-operated pedal means to two of said three hydraulic drive systems which are electrically controlled, the third o...