发明申请
WO2010052022A2 VANE HAVING A REGULATING FLAP AND A GAP COVERING DEVICE AND AN ADJUSTING MECHANISM FOR A GAP COVERING DEVICE
审中-公开
基本信息:
- 专利标题: VANE HAVING A REGULATING FLAP AND A GAP COVERING DEVICE AND AN ADJUSTING MECHANISM FOR A GAP COVERING DEVICE
- 专利标题(中):用锁的门,分裂调节罩装置的缝隙覆盖和设备WINGS
- 申请号:PCT/EP2009008018 申请日:2009-11-10
- 公开(公告)号:WO2010052022A2 公开(公告)日:2010-05-14
- 发明人: SCHLIPF BERNHARD , PAYNE CHRISTOPER , GIBBERT MARKUS , DOSTMANN TOM
- 申请人: AIRBUS OPERATIONS GMBH , AIRBUS OPERATIONS LTD , SCHLIPF BERNHARD , PAYNE CHRISTOPER , GIBBERT MARKUS , DOSTMANN TOM
- 专利权人: AIRBUS OPERATIONS GMBH,AIRBUS OPERATIONS LTD,SCHLIPF BERNHARD,PAYNE CHRISTOPER,GIBBERT MARKUS,DOSTMANN TOM
- 当前专利权人: AIRBUS OPERATIONS GMBH,AIRBUS OPERATIONS LTD,SCHLIPF BERNHARD,PAYNE CHRISTOPER,GIBBERT MARKUS,DOSTMANN TOM
- 优先权: DE102008056655 2008-11-10
- 主分类号: B64C7/00
- IPC分类号: B64C7/00 ; B64C9/02
摘要:
The invention relates to a vane having a regulating flap (1) that can be moved between a retracted position and an extended position and a gap covering device (10) having an adjusting lever (13) and a gap covering flap (11) arranged thereon, having a flow surface (11 a), ° wherein the adjusting lever (13) having the gap covering flap (11) is prestressed by a prestressing device (20) into a first position in which the gap covering flap (11) is located in the interior (B) of the vane (F), and ° wherein the regulating flap (1) and the adjusting lever (13) having the gap covering flap (11) are coupled mechanically such that when the regulating flap (1) moves into the retracted position thereof, the adjusting lever (1) moves into a second position against the prestress produced by the prestressing device (20), and ° wherein the flow surface (11 a) of the gap covering flap (11) in the second position of the adjusting lever (13) runs between the top side (2) of the retracted regulating flap (1) and the vane flow surface (7).
摘要(中):
翼,其包括在缩回位置和伸出位置可移动的控制阻尼器之间的(1)和一个间隙盖装置(10)与致动杆(13)和布置在该间隙中盖片(11),其具有流动表面(11),° 其中,所述致动杆(13)与所述间隙盖片(11)由一个偏置装置的装置(20)被偏置到第一位置,其中,所述间隙盖折翼(11)在所述翼的内部(B)(F),和 °,其中,所述蝶形阀(1)和与所述间隙盖片(11)的调节杆(13)机械地耦合,使得,在移动蝶阀(1)时在其缩回位置,致动杆的运动(1)抵靠通过 偏压装置(20)引起的偏压到第二位置发生,并且°其中,所述流动表面(11)的顶部之间的致动杆(13)的第二位置的间隙盖片(11)的(2)代 ř缩回蝶阀(1)和翼流动表面(7)。
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C7/00 | 其他类目不包括含的结构或整流装置 |