发明名称 INTEGRATED ENGINE AIR PARTICLE FILTER ASSEMBLY
摘要 An engine air particle filter system in a helicopter having a support structure that is fixed to the helicopter. The support structure has a plurality of ribs. The plurality of ribs and the support structure form a plurality of openings. A plurality of trays, containing a filter media, each fit into each one of the plurality of openings in an airtight configuration. A connector releasably secures each one of the plurality of trays to the support structure so that each one of the plurality of trays can be selectively inserted and withdrawn from each one of the plurality of openings.
申请公布号 WO2006113388(A3) 申请公布日期 2007.06.21
申请号 WO2006US13976 申请日期 2006.04.13
申请人 SIKORSKY AIRCRAFT CORPORATION;BARNARD, RICHARD, S.;PETERS, JON, C. 发明人 BARNARD, RICHARD, S.;PETERS, JON, C.
分类号 B64D27/00 主分类号 B64D27/00
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