发明名称 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions
摘要 <p>The jet engine has a sealing system for insulating a cavity from a vein of primary flow. The system has a joint (50) mounted at periphery of an upstream portion (12a) of an external case (12) of a diffuser grid. Blades of the joint (50) are in support on a free end of a spoiler (71). Another joint (60) is situated upstream of the joint (50), and whose blades are in support on an upstream end of a spoiler (72) and on a spoiler (76).</p>
申请公布号 KR101146402(B1) 申请公布日期 2012.05.17
申请号 KR20040071426 申请日期 2004.09.07
申请人 发明人
分类号 F02K1/80;F01D11/00;F01D25/24;F02C7/28;F02K1/00;F04D29/08;F16J15/08 主分类号 F02K1/80
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