首页> 外国专利> ENGINE INTAKE SHUTTER TO BE MOUNTED AT AIRCRAFT ENGINE AIR INTAKE AND AIRCRAFT ENGINE WITH SUCH INTAKE SHUTTER AND AIRCRAFT SYSTEM

ENGINE INTAKE SHUTTER TO BE MOUNTED AT AIRCRAFT ENGINE AIR INTAKE AND AIRCRAFT ENGINE WITH SUCH INTAKE SHUTTER AND AIRCRAFT SYSTEM

机译:带有这种进气门和飞机系统的发动机进气门将安装在飞机进气口和飞机发动机上

摘要

FIELD: transport.;SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft engine air intake shutter. Intake shutter K has first end E1 and second end E2 arranged spaced therefrom and opposite thereto and along its lengthwise axis L. Note here that lengthwise axis L in this configuration is directed across direction D of air flow fed to the engine. Sutter K has main case 1 with hinged to connect main case 1 to air intake case or air intake duct extending along second end E2 with hinge pin A, elongated part 2 of said shutter integrated in main case 1 and has and second side part 5, 6. Side parts 5, 6 extend from main case 1 to two side edges 1a, 1b of the shutter K and to oppose each other in lengthwise direction L, and multiple transverse rods 11 or lengthwise rods.;EFFECT: optimised inlet airflow, prevented air intake icing.;15 cl, 5 dwg
机译:技术领域本发明涉及飞机工程,即飞机发动机进气百叶窗。进气百叶窗K具有第一端E1和第二端E2,第一端E1和第二端E2沿其纵向轴线L与其隔开并相对设置。在此,纵向轴线L在此构造中指向输送到发动机的空气流的方向D。开闭器K具有主箱1,该主箱1具有铰链以将主箱1连接到具有铰链销A的沿第二端E2延伸的进气箱或进气管道,所述百叶窗的细长部分2集成在主箱1中,并具有第二侧部5, 6.侧面部件5、6从主机壳1延伸到百叶窗K的两个侧边缘1a,1b,并在长度方向L上彼此相对,并形成了多个横向杆11或纵向杆。进气口结冰; 15 cl,5 dwg

著录项

  • 公开/公告号RU2490178C2

    专利类型

  • 公开/公告日2013-08-20

    原文格式PDF

  • 申请/专利权人 EHRBUS OPEREJSHNS GMBKH;

    申请/专利号RU20100135968

  • 发明设计人 BOLENDER LARS (DE);VANON SEBASTEN (CH);

    申请日2009-02-04

  • 分类号B64D33/02;

  • 国家 RU

  • 入库时间 2022-08-21 16:22:52

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