| 发明名称 |
APPARATUS AND METHODS FOR ACTUATION OF FLIGHT CONTROL SURFACES |
| 摘要 |
Apparatus and methods for actuating flight control surfaces (16A-C) of fixed-wing aircraft are disclosed herein. An exemplary apparatus disclosed includes a common movable driving member (20) for actuating a plurality of flight control surfaces; a first power transfer device (24A) configured to variably adjust power transfer from the common movable driving member to a first of the plurality of flight control surfaces; and a second power transfer device (24B) configured to variably adjust power transfer from the common movable driving member to a second of the plurality of flight control surfaces. The power transferred to the second flight control surface may be adjusted independently of the power transferred to the first flight control surface. Apparatus and methods for actuating flight control surfaces using magneto-rheological fluid or electro-rheological fluid are also disclosed. |
| 申请公布号 |
US2016355253(A1) |
申请公布日期 |
2016.12.08 |
| 申请号 |
US201515114532 |
申请日期 |
2015.01.30 |
| 申请人 |
BOMBARDIER INC. ;UNIVERSITÉ DE SHERBROOKE |
发明人 |
NFONGUEM Gustave;CHOUINARD Patrick;PLANTE Jean-Sebastien |
| 分类号 |
B64C13/36;F16D37/00;F16D37/02;B64C13/34 |
主分类号 |
B64C13/36 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An apparatus for differentially actuating a plurality of flight control surfaces of a fixed-wing aircraft, the apparatus comprising:
a common movable driving member for actuating the plurality of flight control surfaces; a first power transfer device configured to variably adjust power transfer from the common movable driving member to a first of the plurality of flight control surfaces; and a second power transfer device configured to, independently of the power transferred to the first flight control surface, variably adjust power transfer from the common movable driving member to a second of the plurality of flight control surfaces. |
| 地址 |
Dorval CA |
