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DEVICE FOR PROTECTION OF AIRCRAFT ENGINE AGAINST BIRD COLLISION

机译:防止鸟撞的飞机发动机的装置

摘要

FIELD: aviation.;SUBSTANCE: protective device for an aircraft engine to protect the aircraft engine from suctioning large objects contains a generally cone-shaped body, the base section of the rear end of the protective device body and the cap section at the distal front end of the protective device body, at least three vertical walls extending along the periphery, located between the base and the cap section, the peripheral walls following each other have different peripheral sizes, are cylindrical along the periphery, with an increase in size from the base to the cap section. Plurality of air inlets are formed inside and between the peripheral walls, at least one overall dimension is sufficiently small to prevent the possibility of penetration of birds through a protective device in an aircraft engine.;EFFECT: maximum airflow and optimum protection against bird collisions is provided.;13 cl, 12 dwg
机译:领域:航空;物质:一种用于保护飞机发动机免于吸入大物体的飞机发动机的保护装置,包括大体呈圆锥形的主体,该保护装置主体的后端的基部和位于远端前部的盖部。在保护装置主体的端部,至少三个沿圆周延伸的垂直壁位于基座和盖部之间,彼此相邻的圆周壁具有不同的圆周尺寸,沿着圆周是圆柱形的,并且尺寸从盖帽部分。多个进气口形成在周壁内部和周壁之间,至少一个整体尺寸足够小,以防止飞鸟穿过飞机发动机保护装置的可能性。效果:最大的气流和对飞鸟碰撞的最佳保护是提供; 13 cl,12 dwg

著录项

  • 公开/公告号RU2680644C1

    专利类型

  • 公开/公告日2019-02-25

    原文格式PDF

  • 申请/专利权人 BOATENG WILLIAM BEKOE;

    申请/专利号RU20180118838

  • 发明设计人 BOATENG WILLIAM BEKOE (US);

    申请日2016-07-07

  • 分类号F02C7/055;B64D33/02;

  • 国家 RU

  • 入库时间 2022-08-21 11:46:23

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