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PORTABLE TEST BENCH FOR FIRE TESTING OF ROCKET ENGINES UNDER FIELD CONDITIONS

机译:野外条件下火箭发动机火力测试的便携式测试台

摘要

The invention relates to testing engineering. A portable stand for fire testing of rocket engines in field conditions has unit for installation and fixation of testing engine, force indicator and measurement-registration equipment. The force indicator is connected to the front (bottom) section of the engine by means of transition unit and is electrically connected to amplifier-transformer. According to the invention, the appliance for installation and fixation of testing engine is arranged as stand with holder pipe mounted with respect to the base of the stand on prescribed distance with possibility of placement of force indicator, and with possibility of installation of testing engine in the pipe with nozzle section upward, with prescribed gap and with possibility of centering it at the nozzle section by means of springy gaskets, and at the bottom one - by means of spherical head of the tip of transition unit resting on the hole of springy force-receiving element of force indicator. This invention provides increase of reliability of the stand, of safety and ease in operation, and prevention of side vibrations from transverse loads and sudden (not permitted) operation of the engine being tested.
机译:本发明涉及测试工程。用于在野外条件下对火箭发动机进行火力测试的便携式支架,具有用于安装和固定测试发动机,力指示器和测量配准设备的单元。力指示器通过过渡单元连接到发动机的前部(底部),并电连接到放大器-变压器。根据本发明,用于测试发动机的安装和固定的器具被布置成支架,该支架相对于支架的基座以预定距离安装有支架管,并且可以放置力指示器,并且可以将测试发动机安装在支架中。喷嘴部分朝上,具有预定间隙的管道,并可能通过弹性垫圈在喷嘴部分居中,并在底部使管道居中-通过过渡单元尖端的球形头置于弹性力孔上-力指示器的接收元件。本发明提高了机架的可靠性,安全性和操作的简便性,并防止了横向载荷引起的侧向振动以及被测发动机的突然(不允许)运行。

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