| 摘要 |
Fixing system for a modular leading edge ( 2 ) to the structure of an aircraft lift plane ( 1 ), in which the leading edge ( 2 ) has a covering ( 4 ) formed from a first lamina ( 5 ) and a second lamina ( 6 ) between which there is an interior airtight chamber, and the fixing system comprises a main attachment element ( 3 ) whose cross-section has a central element ( 13 ), a first arm ( 14 ) which is fixed to the first lamina ( 5 ) of the covering ( 4 ) of the leading edge ( 2 ), and a second arm ( 15 ) which is fixed to the second lamina ( 6 ) of the covering ( 4 ), and the central element ( 13 ) is in turn fixed to a covering ( 10 ) of the torsion box ( 8 ) of the structure of the lift plane ( 1 ).
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