Dynamic sealing mechanism between telescopic wing and aircraft cabin
Dynamic sealing mechanism between telescopic wing and aircraft cabin
- Neue Suche nach: XU QUAN
- Neue Suche nach: XU SHENGLI
- Neue Suche nach: ZHANG DI
- Neue Suche nach: WANG BOLAN
- Neue Suche nach: FU JIANMING
- Neue Suche nach: MO LIN
- Neue Suche nach: ZHAO HONGYU
- Neue Suche nach: LIANG WEI
- Neue Suche nach: LIU GUANG
- Neue Suche nach: REN ZHIYI
- Neue Suche nach: TANG XIAOFENG
- Neue Suche nach: CHEN JINGHUA
- Neue Suche nach: LIU GUOGANG
- Neue Suche nach: XU QUAN
- Neue Suche nach: XU SHENGLI
- Neue Suche nach: ZHANG DI
- Neue Suche nach: WANG BOLAN
- Neue Suche nach: FU JIANMING
- Neue Suche nach: MO LIN
- Neue Suche nach: ZHAO HONGYU
- Neue Suche nach: LIANG WEI
- Neue Suche nach: LIU GUANG
- Neue Suche nach: REN ZHIYI
- Neue Suche nach: TANG XIAOFENG
- Neue Suche nach: CHEN JINGHUA
- Neue Suche nach: LIU GUOGANG
The invention provides a dynamic sealing mechanism between a telescopic wing and an aircraft cabin. The mechanism comprises a sealing mounting bracket mounted on the aircraft cabin, wherein an avoidance opening for avoiding the telescopic wing is formed in the sealing mounting bracket, a sealing moving block is mounted on any one side wall, parallel to the telescopic direction of the telescopic wing, of the avoidance opening, and the sealing moving block is mounted on the other side wall of the avoidance opening; a spring is connected between any sealing movable block and the side wall of thereceding opening where the sealing movable block is located, the telescopic direction of any spring is parallel to the thickness direction of the telescopic wing, the side, away from the side wall ofthe receding opening connected with the sealing movable block, of any sealing movable block abuts against the telescopic wing, and the sealing movable block and the telescopic wing are matched to sealthe avoidance opening. The mechanism is advantaged in that high-speed airflow flowing into the aircraft cabin body along the gaps between the telescopic wings and the aircraft cabin body can be reduced, and therefore damage to the internal structure of the flight cabin body and damage to equipment in the flight cabin body can be reduced.
本发明提供了一种伸缩翼与飞行器舱体间的动密封机构，包括安装在飞行器舱体上的密封安装支架，所述密封安装支架上开设有用于避让伸缩翼的避让口，所述避让口平行于伸缩翼伸缩方向的任一侧壁上均安装有密封动块，任一所述密封动块与其位于的避让口侧壁之间均连接有弹簧，任一所述弹簧的伸缩方向均平行于伸缩翼的厚度方向，任一所述密封动块远离与其连接的避让口侧壁的一侧均抵在伸缩翼上，且所述密封动块与伸缩翼配合封闭避让口。有助于减少高速气流沿伸缩翼与飞行器舱体间的间隙流入飞行器舱体内，从而有助于减少飞行舱体的内部结构以及飞行舱体内设备的损伤。
Dokumentinformationen
Dynamic sealing mechanism between telescopic wing and aircraft cabin
一种伸缩翼与飞行器舱体间的动密封机构
2021-03-30
Patent
Elektronische Ressource
Chinesisch
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