| 发明名称 |
AIRCRAFT COMPRISING A CONTROL DEVICE FOR A JET PIPE NOZZLE WITH VARIABLE CROSS-SECTION POWERED BY TWO INDEPENDENT ELECTRICAL POWER SUPPLIES |
| 摘要 |
The subject of the disclosure is an aircraft comprising at least one left motor generator, at least one right motor generator, a control device for a jet pipe nozzle with variable cross-section of the aircraft comprising at least one control member powered by a first airplane electrical power supply linked to at least one right or left motor generator, the control member powered by a second electrical power supply linked to an electrical power source of the aircraft independent of the first airplane electrical power supply. |
| 申请公布号 |
US2015266588(A1) |
申请公布日期 |
2015.09.24 |
| 申请号 |
US201414480016 |
申请日期 |
2014.09.08 |
| 申请人 |
Airbus Operations (S.A.S.) |
发明人 |
Bulin Guillaume;Calvairac Pierre;Lecointre Nicolas;Roux Paul-Emile |
| 分类号 |
B64D33/04;B64D35/08;B64D31/14 |
主分类号 |
B64D33/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising at least one left motor generator, at least one right motor generator, a control device for a jet pipe nozzle with variable cross-section of the aircraft comprising at least one control member which drives at least one actuator which generates, via a mechanical transmission chain the movement of at least one moving part of the jet type nozzle with variable cross-section, the control member being powered by a first airplane electrical power supply linked to at least one right or left motor generator, the control member being powered by a second electrical power supply linked to an electrical power source of the aircraft that is independent of the first airplane electrical power supply. |
| 地址 |
Toulouse FR |
