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Energy-Deposition Systems, Equipment and Methods for Modifying and Controlling Shock Waves and Supersonic Flow

机译:改变和控制冲击波和超音速流的能量沉积系统,设备和方法

摘要

Systems, equipment, and methods to deposit energy to modify and control shock waves and hypersonic or supersonic fluid flow, including systems for controlling, mitigating, and/or effecting air flow in relation to air vehicles, wind tunnels, or other assets, or the like, as well as systems, equipment, and methods for disrupting the shock structure at the inlet for the engine of an air vehicle traveling at supersonic or hypersonic speed; mitigating blast effects on vehicles; mitigating heating of throats in supersonic and hypersonic wind tunnels, as well as control the flow parameters and Mach number in their test sections.
机译:沉积能量以修改和控制冲击波以及高超音速或超音速流体流的系统,设备和方法,包括用于控制,缓解和/或影响与航空器,风洞或其他资产有关的空气流的系统,或者破坏以超音速或高音速行驶的飞行器的发动机入口处的冲击结构的系统,设备和方法;减轻爆炸对车辆的影响;减轻超音速和高音速风洞中的喉咙加热,并控制其测试区域的流量参数和马赫数。

著录项

  • 公开/公告号US2015292532A1

    专利类型

  • 公开/公告日2015-10-15

    原文格式PDF

  • 申请/专利权人 KEVIN KREMEYER;

    申请/专利号US201514601742

  • 发明设计人 KEVIN KREMEYER;

    申请日2015-01-21

  • 分类号F15D1;F15D1/12;G01M9/06;

  • 国家 US

  • 入库时间 2022-08-21 15:27:30

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