|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/099.4; 244/220; 244/225; 244/087; 244/099.9; 244/211|
|우선권정보||DE-10 2008 022 092 (2008-05-05)|
|§371/§102 date||20101123 (20101123)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 6 인용 특허 : 33|
A fault-tolerant actuating system with at least one flap, adjustable on a respective wing of an aircraft, and with a control and monitoring device, includes: drive devices that are functionally connected to the control and monitoring device, with one of these drive devices in each case being associated with a flap, where each flap in each case is associated with a drive device, in each case including: two drive motors, two brake mechanisms, where each drive motor is associated with a brake mechanism for stopping rotation of the output of the respective d...
1. A fault-tolerant actuating system, comprising: at least one flap, adjustable on a respective wing of an aircraft;a control and monitoring device;drive devices that are functionally connected to the control and monitoring device, each drive device being associated with a respective flap, each drive device comprising: (i) two drive motors, and two brake mechanisms, wherein each drive motor is associated with a respective brake mechanism for stopping rotation of an output of the respective drive motor, (ii) a differential that couples the outputs of the ...