首页> 外国专利> Thrust measurement apparatus of rocket engine, and thrust measurement method, and thrust calibration method using the same

Thrust measurement apparatus of rocket engine, and thrust measurement method, and thrust calibration method using the same

机译:火箭发动机的推力测量装置,推力测量方法以及使用该方法的推力校准方法

摘要

The present invention relates to a thrust measuring apparatus for a rocket engine and a thrust measuring method and a thrust correcting method using the thrust measuring apparatus and a rocket engine equipped with the rocket engine. And the load 33 is connected to the engine 11 via the table 21 and the rod 33 and the force that the table 21 is pushed by the reaction force generated in the combustion test of the rocket engine 11 (41) for correcting the load cell (31) by adding a load to the load cell (31), and a control unit (41) for storing the thrust measured by the load cell And a control measuring section (63) for controlling the operation of the correcting means (41). The present invention is capable of measuring the thrust force simultaneously with the combustion test of the rocket engine, and real-time thrust compensation is possible, so that there is an advantage that the accurate thrust of the rocket engine can be obtained by performing the combustion test.
机译:火箭发动机的推力测量装置,使用该推力测量装置的推力测量方法和推力校正方法技术领域本发明涉及一种火箭发动机的推力测量装置,使用该推力测量装置的推力测量方法和推力校正方法。并且负载33经由工作台21和杆33连接至发动机11,并且工作台21受到在火箭发动机11(41)的燃烧测试中产生的反作用力推动的力,以校正测力传感器(通过将载荷施加到称重传感器(31)和用于存储由称重传感器测得的推力的控制单元(41)和用于控制校正装置(41)的操作的控制测量部分(63)来实现图31)。本发明能够在火箭发动机的燃烧试验的同时测量推力,并且可以进行实时的推力补偿,因此具有通过执行燃烧能够获得火箭发动机的精确推力的优点。测试。

著录项

  • 公开/公告号KR101473981B1

    专利类型

  • 公开/公告日2014-12-18

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20130038769

  • 发明设计人 이재원;

    申请日2013-04-09

  • 分类号G01L5/12;F02K9/96;G01M15/14;

  • 国家 KR

  • 入库时间 2022-08-21 15:01:07

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