An aircraft fuel tank access cover comprises an inner door, an outer door and a clamping arrangement for clamping the doors together about an access aperture in the skin of the fuel tank. The clamping arrangement comprises a bolt in-molded in a generally central part of the inner door and or external nut. The doors have reinforcing rib arrangements to spread the clamping load to the peripheral edges thereof.
Aircraft fuel tank access cover and an aircraft fuel tank
2015-11-24
Patent
Elektronische Ressource
Englisch
Outer fuel tank access cover, wing and aircraft description
Europäisches Patentamt | 2016
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