发明名称 Enteisungsvorrichtung für die Verkleidung des Lufteinlaufs eines Strahltriebwerkes
摘要 The system has an airtight coupling (22) for a pipe delivering hot air under pressure to an injector (12) located inside the engine ring cowling to de-ice its leading edge. The coupling between the forward end (10A) of the pipe and the injector is in the form of a ball and socket joint with a cylindrical chamber (23) open at both ends (23A, 23B) and connected by its forward end to the injector, and a hollow pivot (24) on the forward end of the pipe, engaging by with the inside of the chamber through its rear end. The inner wall of the chamber has an anti-friction coating (28), e.g. of carbon or tungsten carbide, and the hollow pivot is made from a slightly elastic metal, or a rigid metal with an elastic coating (27).
申请公布号 DE69803741(T2) 申请公布日期 2002.09.26
申请号 DE1998603741T 申请日期 1998.11.19
申请人 AEROSPATIALE MATRA, PARIS 发明人 PORTE, ALAIN
分类号 F02C7/047;F16L27/12 主分类号 F02C7/047
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