发明名称 CASE STRUCTURE INTERPOSED BETWEEN THE ENGINE AND THE NACELLE, HAVING A MOUNTING PLATE WITH SCREWS
摘要 An aircraft casing structure including a shroud surrounding the engine and made up of a plurality of sectors; a plurality of radial arms, each mounted between two adjacent shroud sectors and each having a base; and a plurality of fasteners for fastening the shroud sectors on the bases of the radial arms; the fasteners including a plurality of plates each mounted flush in a respective groove of corresponding shape in a shroud sector, and a set of headed bolts held captive in the plate by a difference of diameter between their shanks and their threads, a set of captive nuts being fastened to the bases to provide a secure connection between the shroud sectors and the radial arms by each nut receiving the thread of a respective captive bolt of the set of headed bolts.
申请公布号 EP3041741(A1) 申请公布日期 2016.07.13
申请号 EP20140786979 申请日期 2014.08.25
申请人 SNECMA 发明人 BELJAMBE, CEDDRIC;ROBIN, NOËL
分类号 B64D27/26;F01D25/16;F01D25/24 主分类号 B64D27/26
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