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HELICOPTER ENGINE COMPARTMENT VENTILATING SYSTEM

机译:直升机发动机舱通风系统

摘要

A helicopter engine compartment ventilating system includes an ejector nozzle,four airscoops, two air plenums and two air slots. The ejector nozzle encompasses theengine exhaustpipe mouth and downstream flow of exhaust gas for drawing air into, throughand out of theengine compartment. Two air scoops are affixed to the helicopter fuselage atthe forwardperimeter of the engine compartment for supplying air to the two air plenumsthat direct theair through the engine and transmission oil heat exchangers into the enginecompartment.Two additional air scoops are attached to the upper forward perimeter of theenginecompartment for supplying air to the upper area of the engine compartment. Theair slots arelocated at the forward edge of each engine compartment door for allowing airto be drawninto the midsection of the engine compartment.
机译:直升机发动机舱通风系统,包括一个喷射器喷嘴,四个空气铲子,两个气室和两个气槽。喷射喷嘴包括发动机排气管口和废气下游流,用于将空气吸入并从发动机舱。直升机机身上固定了两个气铲前锋发动机舱的周边,用于向两个空气室供气指导空气通过发动机和变速箱油热交换器进入发动机隔间。两个额外的空气勺连接到机枪的前部上周边发动机用于向发动机舱上部提供空气的舱室。的空气槽位于每个发动机舱门的前缘,以允许空气进入被画进入发动机舱的中部。

著录项

  • 公开/公告号CA3055979A1

    专利类型

  • 公开/公告日2020-04-09

    原文格式PDF

  • 申请/专利权人 HENKE JAMES A.;

    申请/专利号CA20183055979

  • 发明设计人 HENKE JAMES A.;

    申请日2018-10-09

  • 分类号B64D33;B64D29;B64D33/08;F01P1;F01P5/08;

  • 国家 CA

  • 入库时间 2022-08-21 11:14:38

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