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DUAL REDUNDANT IN-FLIGHT EGRESS SYSTEM (IES) OF CANOPY SEVERANCE FOR FIGHTER AIRCRAFT

机译:战斗机机盖遣散的双重冗余飞行中整合系统

摘要

Dual Redundant In-flight Egress system (IES) of Canopy severance for Fighter Aircraft employs two rows of Shaped MDC pasted on canopy bubble of fighter aircraft which will sever the canopy bubble when pilot pulls the ejection handle. MDC fires and severs the canopy bubble thus providing an unobstructed path for the seat to egress through the transparency. Usage of two rows of MDC and two PAI greatly improves the reliability of the system as even if one PAI fails to ignite the canopy will be severed with the aid of Second PAI. In the present system even length of MDC increased in order to cover pilot thigh portion so as to reduce the risk of injury to the pilot.
机译:战斗机机盖遣散的双重冗余机上飞行出口系统(IES)在战斗机机盖泡沫上粘贴两排Shape MDC,当飞行员拉出弹射手柄时,该MDC会切断机盖泡沫。 MDC发射并切断顶篷气泡,从而为座椅提供了一条通畅的通道,使其可以通过透明通道。使用两排MDC和两个PAI可以极大地提高系统的可靠性,即使一个PAI无法点火也无法通过第二个PAI来切断机盖。在本系统中,MDC的长度甚至增加以覆盖飞行员的大腿部分,从而降低了飞行员受伤的风险。

著录项

  • 公开/公告号IN2013CH02353A

    专利类型

  • 公开/公告日2016-06-10

    原文格式PDF

  • 申请/专利权人

    申请/专利号IN2353/CHE/2013

  • 发明设计人 PREM RAJ V;A JEEVAN PRAKASH;C KUPPURAJ;

    申请日2013-05-30

  • 分类号B64C1/32;

  • 国家 IN

  • 入库时间 2022-08-21 14:25:42

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