The invention relates to a sealing arrangement for use between flaps of an aircraft, the sealing arrangement comprising a first sealing portion and a second sealing portion, the first and second sealing portions interfacing one another between the flaps, where the first sealing portion comprises a plurality of discrete first seals, and the second sealing portion comprises a plurality of discrete second seals. And the second sealing portion includes a plurality of discrete second seals. The sealing structure with the separated design is more suitable for the situation of scissors difference between the inner flap and the outer flap.
本发明涉及一种用于飞机的襟翼之间的密封结构,这种密封结构包括第一密封部分和第二密封部分,第一密封部分和第二密封部分在襟翼之间彼此对接,其中,第一密封部分包括多个离散的第一密封件,并且第二密封部分包括多个离散的第二密封件。这种分离式设计的密封结构更适用于内外襟翼间剪刀差的情形。
Sealing structure used between flaps of airplane
一种用于飞机的襟翼之间的密封结构
2023-12-08
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Application of slots and flaps to airplane wings in America
Engineering Index Backfile | 1933
|Flight Tests of Dive-recovery Flaps on an XP-51 Airplane
NTRS | 1945
|