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AIRPLANE ENGINE BIRD STRIKE PROTECTION GUARD

机译:飞机发动机鸟撞防护装置

摘要

An aircraft engine guard for protecting an aircraft engine against ingestion of large objects includes a generally cone-shaped body a base section of the rear end of the guard body and a dome section at the distal forward end of the guard body at least three vertical peripherally extending walls located between the base and the dome section with successive ones of the peripheral walls having different peripheral dimensions peripherally cylindrical with the dimension increasing from the base toward the dome section. A plurality of air intake openings are defined in and between the peripheral walls with at least one dimensional size which is small enough to prevent having birds from being able to pass through the guard into the aircraft engine.
机译:用于保护飞机发动机免于摄入大物体的飞机发动机护罩包括大致圆锥形的主体,护罩主体的后端的基部和在护罩主体的远端的前端的,至少在垂直方向上垂直的三个圆顶部分延伸的壁位于基部和圆顶部分之间,连续的周壁具有不同的外围尺寸,其周向圆柱形,尺寸从基部朝向圆顶部分增大。在周壁内和周壁之间限定有多个进气口,该进气口具有至少一维尺寸,该尺寸足够小以防止鸟类能够穿过防护罩进入飞机发动机。

著录项

  • 公开/公告号IN201817020357A

    专利类型

  • 公开/公告日2018-09-28

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN201817020357

  • 发明设计人 BOATENG WILLIAM BEKOE;

    申请日2018-05-30

  • 分类号F02C7/55;B64D33/02;

  • 国家 IN

  • 入库时间 2022-08-21 12:51:51

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