Sealing structure used between flaps of airplane

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。