Access panel assembly for aircraft fuel tank
作者： Frederick J. Gorges
DOI:
关键词: Clamping 、 Edge (geometry) 、 Bearing (mechanical) 、 Wire mesh 、 Gasket 、 Seal (mechanical) 、 Engineering 、 Fuel tank 、 Composite material
摘要: An improved gasket (16, 100) for a panel assembly (10) to close an access opening (22) the wall (24) of wing mounted fuel tank in aircraft. The comprises lubricant impregnated wire mesh material (102), having at its edge portions annular seal members (104, 106), with being elements (107) material. is positioned between clamping ring (18) which bearing relationship against (12) and portion (26) tank.
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