首页> 外国专利> SYSTEM FOR EVALUATING THE RELIABILITY OF THE HEAD UNIT OF A COMBUSTOR IN A LIQUID ROCKET ENGINE CAPABLE OF VERIFYING THE DURABILITY OF THE COMBUSTOR

SYSTEM FOR EVALUATING THE RELIABILITY OF THE HEAD UNIT OF A COMBUSTOR IN A LIQUID ROCKET ENGINE CAPABLE OF VERIFYING THE DURABILITY OF THE COMBUSTOR

机译:评估可验证燃烧器耐用性的液体火箭发动机中燃烧器前部单元可靠性的系统

摘要

PURPOSE: A system for evaluating the reliability of the head unit of a combustor in a liquid rocket engine is provided to evaluate the reliability of the head unit of the combustor by applying an impact internal pressure and loads at the same time during a burning test.;CONSTITUTION: A system for evaluating the reliability of the head unit of a combustor in a liquid rocket engine comprises a combustor head unit(100), a pressing unit(200), a load applying unit(300), and a controller(400). The reliability of the combustor head unit is evaluated. The pressing unit applies pressure to the combustor head unit. The load applying unit applies loads to the combustor head unit. The controller controls the pressing unit and the load applying unit.;COPYRIGHT KIPO 2012
机译:目的:提供一种用于评估液体火箭发动机中燃烧器主机的可靠性的系统,以通过在燃烧测试期间同时施加冲击内部压力和载荷来评估燃烧器主机的可靠性。组成:一种用于评估液体火箭发动机中燃烧器头部的可靠性的系统,包括燃烧器头部(100),加压单元(200),负载施加单元(300)和控制器(400) )。评估燃烧室机头单元的可靠性。加压单元向燃烧器头部单元施加压力。载荷施加单元将载荷施加到燃烧器头部单元。控制器控制加压单元和负载施加单元。COPYRIGHTKIPO 2012

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