IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
|
| 국제특허분류(IPC7판) |
|
| 출원번호 |
US-0320094
(1989-01-09)
|
| 우선권정보 |
FR-0008870 (1987-06-24) |
| 국제출원번호 |
PCT/FR88/00329
(1988-06-20)
|
| §371/§102 date |
19890109
(19890109)
|
| 국제공개번호 |
WO-8810458
(1988-12-29)
|
|
발명자
/ 주소 |
- Farineau Jacques (Toulouse FRX)
|
| 출원인 / 주소 |
- Aerospatiale Societe Nationale Industrielle (Paris FRX 07)
|
| 인용정보 |
피인용 횟수 :
32 인용 특허 :
4 |
초록
▼
System for controlling roll and yaw of an aircraft. The system includes a device capable of elaborating, from electric signals respectively representative of the position of a first voluntary actuation member, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of a seco
System for controlling roll and yaw of an aircraft. The system includes a device capable of elaborating, from electric signals respectively representative of the position of a first voluntary actuation member, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of a second voluntary actuation member, a single electrical order for roll control formed by a linear combination of the electric signals. There is a device capable of elaborating, from the same electric signals, an electrical order for yaw control formed by a linear combination of the electric signals. There is also a device which makes it possible to combine the electrical order for yaw control and a mechanical order coming directly from the second voluntary actuation member.
대표청구항
▼
System for controlling roll and yaw of an aircraft (1) comprising roll control surfaces (8, 9) actuated from a first voluntary actuation member (14) and a rudder (11) actuated from a second voluntary actuation member (15), via a mechanical transmission (24), said first and second voluntary actuation
System for controlling roll and yaw of an aircraft (1) comprising roll control surfaces (8, 9) actuated from a first voluntary actuation member (14) and a rudder (11) actuated from a second voluntary actuation member (15), via a mechanical transmission (24), said first and second voluntary actuation members (14, 15) being associated with transducers (37, 39-41) delivering respectively first and second electrical signals depending on the position of said members, said aircraft comprising in addition means (43, 47) capable of delivering third, fourth, fifth and sixth electrical signals respectively representative of the rolling speed, the attitude, the yaw speed and the sideslip of said aircraft, said system comprising: (a) a device (16) capable of elaborating, from said first, third, fourth, fifth, sixth and second electrical signals respectively representative of the position of said first voluntary actuation member, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of said second voluntary actuation member, a single electrical order for roll control formed by a linear combination of said first to sixth electrical signals; (b) a distribution device (20) which, from said single electrical roll control order, controls each of said roll control surfaces via first actuation means (21); (c) a device (18) capable of elaborating, from said first, third, fourth, fifth, sixth and second electrical signals respectively representative of the position of said first voluntary actuation members, the rolling speed, the attitude, the yaw speed, the sideslip and of the position of said second voluntary actuation member, an electrical order for yaw control formed by a linear combination of said first to sixth electrical signals; and (d) a device (23) for combining said electrical yaw control order and a mechanical order coming directly from said second voluntary actuation member (15) via said mechanical transmission (24), to delivery a single combined order of yaw control, which controls said rudder (11), via second actuation means (26).
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