发明名称 AIRCRAFT FLUID CHECK VALVE ASSEMBLY WITH INDEXING
摘要 An aircraft check valve assembly where the fluid check valve is indexed in rotational position relative to a first duct flange and to a second opposed duct flange and to a clamping band where the check valve includes an annular check valve flange having at least one index tab extending therefrom. The index tab formed in the check valve annular flange engages a void area formed in an outer annular ridge formed in the first and second duct flanges. A clamping band holds the first duct flange to the check valve flange and to the second duct flange where the clamping band is rotationally indexed to the check valve by index fingers formed on the index tab which and extends to occupy a gap formed in a hinge point of the band clamp.
申请公布号 EP2449298(A2) 申请公布日期 2012.05.09
申请号 EP20100794705 申请日期 2010.06.30
申请人 EATON CORPORATION 发明人 MURRAY, JONATHAN, DAVID
分类号 F16K15/03;B64D33/00;F16K37/00 主分类号 F16K15/03
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