Invention Grant
US08573539B2 Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials 失效
用于使用由非金属复合材料制成的三角形配件在飞行器中连接扭转箱的结构

Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metallic composite materials
Abstract:
The invention comprises a triform fitting 1, essentially made from non-metallic composite materials including several strengthening cross ribs 4 for joining symmetrical flanges 3 and a longitudinal flange 2. The symmetrical flanges 3 include cross slots 8 for receiving the run-out 16 of the webs 11 of several T-shaped internal stringers 9 that form part of the torsion boxes 6. The feet 10 of the stringers 9 are joined along one of their faces to the skins 7 of the torsion boxes 6, while the end zones of the free faces of said feet 10 are placed against the outer face of the symmetrical flanges 3 of the triform fitting 1. This ensures that the symmetrical flanges 3 of the triform fitting 1 remain inside the torsion boxes 6. Alternatively, the fitting 1 may not include the cross slots 8.
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