| 发明名称 |
THRUST REVERSER DEVICE |
| 摘要 |
A thrust reverser device for an aircraft turbojet engine includes: a movable cowl, translating cascades connected to the movable cowl, a mast; and a front suspension to suspend the turbojet engine. The cascades translates between a direct jet position where the cascades are retracted in a fan casing, and an indirect jet position where the cascades are brought out of the fan casing. In particular, the cascades have a sliding connection with the mast by means of at least one spacer connected to the mast downstream of the front suspension. |
| 申请公布号 |
US2016025039(A1) |
申请公布日期 |
2016.01.28 |
| 申请号 |
US201514841407 |
申请日期 |
2015.08.31 |
| 申请人 |
AIRCELLE |
发明人 |
BOILEAU Patrick;SEGAT Peter;CARUEL Pierre;TISSOT Sarah |
| 分类号 |
F02K1/72;F02K1/82 |
主分类号 |
F02K1/72 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A thrust reverser device for an aircraft turbojet engine comprising:
a movable cowl; translating cascades connected to the movable cowl and displaceable between a direct jet position where the translating cascades are retracted in a fan casing, and an indirect jet position where the translating cascades are brought out of the fan casing; a mast; and a front suspension configured to suspend the turbojet engine, wherein the translating cascades have a sliding connection with the mast by means of at least one spacer connected to the mast downstream of the front suspension. |
| 地址 |
Gonfreville L'Orcher FR |
