发明名称 |
VARIABLE DAMPING OF HAPTIC FEEDBACK FOR A FLIGHT-ATTITUDE CHANGING LINKAGE OF AN AIRCRAFT |
摘要 |
The present invention relates to haptic feedback for operating at least one manual flight control device (21) for controlling the cyclic pitch of the blades (5) of a rotary wing (4) of a hybrid helicopter (1) via power assistance (27). Said operations of said control device (21) are defined according to a predetermined damping force relationship (A) that is a function of an instantaneous load factor of the hybrid helicopter (1) in such a manner that the instantaneous load factor is maintained between its minimum and maximum limit values in proportion to a position of a thrust control member (20) between its minimum and maximum thrust values (23, 22).
|
申请公布号 |
US2011024551(A1) |
申请公布日期 |
2011.02.03 |
申请号 |
US20100836646 |
申请日期 |
2010.07.15 |
申请人 |
EUROCOPTER |
发明人 |
BIEST ROMUALD;GEMMATI BERNARD;PRUSS JULIEN |
分类号 |
B64C27/22;B64C13/46;G05D1/00 |
主分类号 |
B64C27/22 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|