发明名称 ANTIFREEZE STRUCTURE IN ENGINE FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To improve the performance of an engine for an aircraft by reducing the energy loss in accompany with the operation of an antifreeze structure 25 in the engine for the aircraft. SOLUTION: In this antifreeze structure 25 in the engine for the aircraft, preventing the freezing of an intake duct 9 in the engine for the aircraft, a lip part of the intake duct 9 is composed of an expandable and contractible rubber tube 9a, and expanding and contracting means 27, 29, 33 are mounted for alternately expanding and contracting the rubber tube 9a. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004019643(A) 申请公布日期 2004.01.22
申请号 JP20020180486 申请日期 2002.06.20
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 NARUKAWA MASAHIRO
分类号 B64D15/16;F02C7/042;F02C7/047;(IPC1-7):F02C7/042 主分类号 B64D15/16
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