发明名称 Fan case strut for turbomachine
摘要 An axial flow turbomachine's engine core (16) and radially outwardly disposed fan case (18) are joined together with a radially extending segmented fan case strut (10). The strut (10) is segmented into a radially inner portion (20) and a radially outer portion (20) at a midspanly disposed strut joint (14). The strut joint (14) has an axially extending tapered tongue (26) which slidably engages with a mating axially extending groove (46). A radially extending flange (36) disposed proximate to the trailing edge (35) of the inner portion (20) is bolted to the radially extending flange (56) disposed proximate to the trailing edge (55) of the outward portion (40) when the tongue (26) is fully engaged with the groove (46) to releasably secure the strut joint (14). Another embodiment shows a pair of interlocked axially extending channels (60) each having a U-shaped cross-section replacing the interlocked tongue and groove (26,46) of the first embodiment. Radially extending flanges (36,56) disposed proximate to the portions' (20,40) trailing edges 935,55) are likewise bolted together to releasably secure the strut joint (14) when the channels' three corresponding pairs of contact surfaces (62) are fully slidably engaged.
申请公布号 US5161947(A) 申请公布日期 1992.11.10
申请号 US19910696885 申请日期 1991.05.08
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ECKFELDT, GRANT;WEISSE, MICHAEL A.;KASPROW, ROBERT F.;DEMBECK, KURT M.;LILLIBRIDGE, HERBERT J.
分类号 F02C7/20 主分类号 F02C7/20
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