发明名称 Air inlet cowl for a jet engine, provided with deicing means
摘要 Air inlet cowl for a jet engine, provided with deicing means. According to the invention, an air extraction opening (34) is made in the partition (20) to place the isolation volume (28) enclosing the pressurized hot air feedpipe (10) in communication with the internal peripheral chamber (21) of said leading edge (16), and the passage cross section of said extraction opening (34) is chosen to give the injector (12), in the event of damage to said feedpipe (10), a pressurized hot air flow rate at least equal to 50% of the hot air flow rate through said feedpipe (10).
申请公布号 US2002148929(A1) 申请公布日期 2002.10.17
申请号 US20020103716 申请日期 2002.03.25
申请人 ANDRE ROBERT;PORTE ALAIN 发明人 ANDRE ROBERT;PORTE ALAIN
分类号 B64D15/04;B64D33/02;F02C7/047;(IPC1-7):B64D15/00 主分类号 B64D15/04
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