首页> 外国专利> PISTON RELEASE VALVE FOR FREE PISTON SHOCK TUBE/TUNNEL

PISTON RELEASE VALVE FOR FREE PISTON SHOCK TUBE/TUNNEL

机译:活塞释放阀免费活塞冲击管/隧道

摘要

PROBLEM TO BE SOLVED: To expose a high pressure reservoir to the rear end of a piston immediately at the valve release time by providing a high speed piston release valve, in the free piston shock tube/tunnel for generating an aerodynamic test state for the tip cone of a rocket and ultrasonic passenger plane. ;SOLUTION: In a shock tube/tunnel, having a slender compression chamber 10, to whose right end the slender shock tube is properly connected through a connection collar, inside the compression tube 10 provided from a piston end 18 to a diaphragm end 19, a drive gas such as helium capable of a nearly constant adiabatic expansion is filled during the moving of a piston 11. A closed head 24 and the valve assembly 25 with a high speed are provided on the piston end 18. The valve assembly 25 has a valve sleeve assembly and valve body assembly and by expediting the high pressure flow from a high pressure reservoir 20 to the rear zone of the piston 11, the piston 11 is released and the shot of the piston 11 is started.;COPYRIGHT: (C)1996,JPO
机译:解决的问题:通过在自由活塞减震管/通道中提供一个高速活塞释放阀,在释放阀时立即将高压油箱暴露在活塞的后端,以产生尖端的空气动力学测试状态锥的火箭和超声客机。解决方案:在具有细长压缩室10的冲击管/隧道中,细长的冲击管通过连接套环正确地连接到其右端,该压缩管10位于活塞端18和隔膜端19之间的压缩管10内,在活塞11的移动过程中,填充了能够几乎恒定地进行绝热膨胀的驱动气体,例如氦气。在活塞端部18上设置有封闭的头部24和高速的阀组件25。阀组件25具有阀芯25。阀套组件和阀体组件,并通过加快从高压储存器20到活塞11后部区域的高压流,释放活塞11并开始活塞11的喷射。版权所有:(C) 1996年

著录项

  • 公开/公告号JPH08178092A

    专利类型

  • 公开/公告日1996-07-12

    原文格式PDF

  • 申请/专利权人 AERO SYSTEMS ENG INC;

    申请/专利号JP19950235447

  • 发明设计人 LACEY JR JOHN J;LINDAHL BRUCE C;

    申请日1995-09-13

  • 分类号F16K3/24;

  • 国家 JP

  • 入库时间 2022-08-22 04:03:19

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