发明名称 Aircraft wing-to-body fairing panel assembly and method of making the same
摘要 An access door assembly for joining to a structure. The access door assembly has an access door with at least one access door nonlinear edge, a support structure with at least one support structure nonlinear edge, and a doubler element attached to an interior side of the support structure. The support structure nonlinear edge is designed to interlace with the access door nonlinear edge to form an access door assembly for joining to a structure, the access door assembly having an interlaced nonlinear edge interface. A diameter of the doubler element of the access door assembly is preferably reduced as compared to a diameter of a doubler element of an access door assembly having a linear or circular edge, such that the reduced diameter preferably results in an overall reduced weight of the access door assembly and the structure to which the access door assembly is joined.
申请公布号 EP2760733(B1) 申请公布日期 2016.10.05
申请号 EP20120766199 申请日期 2012.08.24
申请人 THE BOEING COMPANY 发明人 THABLE, GAGAN;BASCHAK, MICHAEL A.;BRAUN, RUDY;STOROZUK, MARC
分类号 B64C1/12;B64C1/06 主分类号 B64C1/12
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