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Side thruster valve and side thruster device

机译:侧推阀和侧推装置

摘要

A side thruster valve of an aerospace craft is improved to reduce torque of a servo-motor, etc. needed for nozzle opening and closing to thereby realize a compact and light weight device. The side thruster valve comprises a valve plug having its back directed to an axis of the aerospace craft and independently movable between a fully opened position and a fully closed position of the valve plug in a plane orthogonal to the axis of the aerospace craft, an actuating means for moving the valve plug in an axial direction of the valve plug and an elastic member for activating the valve plug in the axial direction of the valve plug. In a side thruster device comprising a plurality of the side thruster valves, the side thruster valves are arranged independently of each other to thereby broaden freedom of combustion control and improve fuel consumption.
机译:改进了航空器的侧推力阀,以减小喷嘴打开和关闭所需的伺服电动机等的扭矩,从而实现了紧凑且轻便的装置。侧向推进器阀包括阀塞,该阀塞的后部指向航空航天器的轴线,并且在正交于航空航天器的轴线的平面内可在阀塞的完全打开位置和完全关闭位置之间独立地移动。用于在阀塞的轴向上移动阀塞的装置和用于在阀塞的轴向上致动阀塞的弹性构件。在包括多个侧向推进器阀的侧向推进器装置中,侧向推进器阀彼此独立地布置,从而扩大了燃烧控制的自由度并改善了燃料消耗。

著录项

  • 公开/公告号US6986246B2

    专利类型

  • 公开/公告日2006-01-17

    原文格式PDF

  • 申请/专利权人 TOSHIHARU FUJITA;

    申请/专利号US20030441039

  • 发明设计人 TOSHIHARU FUJITA;

    申请日2003-05-20

  • 分类号F02K1/18;

  • 国家 US

  • 入库时间 2022-08-21 21:42:24

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