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Blanking-cap system for an orifice of a conduit, in particular for an orifice of an air-intake duct into the combustion chamber of a ramjet

机译:用于导管孔口的盲盖系统,特别是用于冲压冲压机燃烧室中的进气管孔口的盲盖系统

摘要

Blanking-cap system for an orifice of a duct, in particular for an orifice of an air-intake duct into the combustion chamber of a ramjet.;The blanking-cap system (16) includes a glass blanking cap (15) and a destruction device (17) which comprises a projectile (18) capable of destroying the blanking cap (15), and a controllable projection means (19), which is capable of projecting the said projectile (18) and which is arranged outside the conduit (7) while being oriented in such a way as to be able to project the said projectile (18) onto the said blanking cap (15).
机译:用于导管孔口的盲孔盖系统,特别是用于冲压喷气机燃烧室的进气管孔口的盲孔盖系统。盲孔盖系统( 16 )包括玻璃盲孔盖( 15 )和破坏装置( 17 ),该装置包括能够破坏落料盖( 15 )和可控的投射装置( 19 ),该投射装置能够投射所述弹丸( 18 ),并布置在导管外部( 7 ),同时以能够将所述射弹( 18 )投射到所述盲孔盖( 15 )上的方式进行定向。

著录项

  • 公开/公告号US6557339B2

    专利类型

  • 公开/公告日2003-05-06

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE MATRA MISSILES;

    申请/专利号US20010924457

  • 发明设计人 JEAN-PAUL DEMAY;LAURENT CARTON;

    申请日2001-08-09

  • 分类号F02K71/80;

  • 国家 US

  • 入库时间 2022-08-22 00:04:52

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