| 摘要 |
A device for overlapping a slot between wing and slat of aircraft is disclosed. The device contains an elasto-plastic seal located along the lower end of the slat and secured by fastening device on the inside of horizontal shelf of longitudinal load-bearing element of slat. In this case in the elasto-plastic seal a longitudinal set of windows is made, and fastening device is made in the form of discretely installed brackets, which free shelf is turned to the wall of the longitudinal load-bearing element of slat and is made in the form of a half-loop located in the window of elasto-plastic seal, and the rod-catch located inside the elasto-plastic seal, which connects half-loops. |
