SKIN-PANEL INTERFACE OF AN AIRCRAFT
A wing (114) or stabilizer (116, 118) of an aircraft (100). The wing or stabilizer comprises a box portion (120), comprising at least one spar (132) and an outer skin (130) coupled to the at least one spar. The wing or stabilizer also comprises at least one panel (134), comprising an outer face-shee...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | A wing (114) or stabilizer (116, 118) of an aircraft (100). The wing or stabilizer comprises a box portion (120), comprising at least one spar (132) and an outer skin (130) coupled to the at least one spar. The wing or stabilizer also comprises at least one panel (134), comprising an outer face-sheet (150) and an inner face-sheet (152). In a fore-aft direction the outer face-sheet terminates at an outer free edge (180). In the fore-aft direction the inner face-sheet terminates at an inner free edge (158). The at least one panel also includes a core (178) sandwiched between the outer face-sheet and the inner face-sheet. The inner face-sheet comprises a cantilevered portion (154). The cantilevered portion defines the inner free edge. The cantilevered portion is fastened to the outer skin of the box portion. |
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