Fuel tank access door for aircraft
AssigneeCanadair Limited
InventorPaul Lamoureux
Life of this patent
Estimating the term…
Abstract
A fluid tight closure for an aperture, more particularly adapted to form a fuel tank access door for an aircraft, preferably made of composite material and providing fail-safe features and resistance to lightning strikes; and further characterized by its light weight, relatively low cost of manufacture, and flexibility to bend from a flat to a curved configuration defined by the curvature of a wing. This fluid tight closure comprises an inner door panel and an outer door panel having each a rim portion complementarily shaped relative to each other and to the edge portion of an aperture, and clamping against the opposite sides of the edge portion with an interposed sealing ring and with nuts and screws sealingly extending through the rim portion and holding the same in clamping position.
Claims10
A fluid tight closure for an access aperture in a fuel tank or the like enclosure and comprising a non-conductive inner door panel, an outer door panel, and fasteners operatively securing said door panels in fluid tight closing position relative to the access aperture, said door panels being of bendable material and having each a rim portion operatively overlapping an edge portion of said access aperture, with said rim portions operatively clamping said edge portion upon engagement with an inner and an outer faces thereof respectively, and sealing means sealingly interposed peripherally of said edge portion intermediate the latter and at least one of said rim portions upon operative fastening of the inner and outer door panels in said fluid tight closing position.
A fuel tank access door for an aircraft comprising an inner door panel, an outer door panel, a plurality of nuts secured to the inner door panel, screws engaging through the outer door panel and threadably into said nuts with operative sealing of the screws and nuts against leakage thereat, each of the door panels defining a rim portion operatively overlapping an edge portion of an access aperture in a fuel tank of the aircraft, a sealing ring secured along the periphery of the rim portion of the inner door panel operatively intermediate the latter and the edge portion of the access aperture, and said door panels being of bendable graphite/epoxy material with said rim portions operatively clamping said edge portion upon engagement with an inner and an outer faces thereof respectively upon tightening of said screws into said nuts.
Dependencies are inferred from the claim text.