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Protection device for the air inlet of a jet engine which is provided with an anti-icing system

机译:用于喷气发动机进气口的保护装置,其具有防冰系统

摘要

The cowling has an inner shell (27) which cooperates with the two partitions (20, 24) and the engine casing outer wall (9E) to form a chamber (28) enclosing the pipe (10). The outer wall also has air intake and outlet holes (34, 35), and the inner shell is detachable and fitted to the forward partition with an elastic seal (32). The ring cowling (9) is equipped with a de-icing system for its hollow leading edge (16), which has a peripheral chamber (21) formed by a partition and having one or more holes linked to the outside atmosphere. The de-icing system has a pipe (10) with its rear end passing through an additional inner partition and connected to a pressurized hot air circuit (14), and equipped at its forward end with an injector (12) delivering hot air to the chamber.
机译:整流罩具有内壳(27),该内壳(27)与两个隔板(20、24)和发动机壳体外壁(9E)协作以形成包围管道(10)的腔室(28)。外壁还具有进气孔和出气孔(34、35),内壳是可拆卸的,并通过弹性密封件(32)安装到前隔板上。环形整流罩(9)为其中空的前缘(16)配备有除冰系统,该系统具有由隔板形成的外围腔室(21),该外围腔室具有一个或多个与外部大气相连的孔。除冰系统的管道(10)的后端穿过一个附加的内部隔板并连接到加压的热空气回路(14),并在其前端配备了一个喷射器(12),将喷射的热空气输送到除冰系统。室。

著录项

  • 公开/公告号EP0918149A1

    专利类型

  • 公开/公告日1999-05-26

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号EP19980402856

  • 发明设计人 PORTE ALAIN;

    申请日1998-11-18

  • 分类号F02C7/047;B64D15/04;

  • 国家 EP

  • 入库时间 2022-08-22 02:18:53

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