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TRACTION DEVICE FOR LOW-THRUST LIQUID-PROPELLANT ROCKET ENGINES IN PULSED OPERATION MODES

机译:脉冲运行模式下低推力火箭发动机的牵引装置

摘要

FIELD: test equipment.;SUBSTANCE: invention relates to test benches for low-thrust liquid-propellant rocket engines (LTLPRE). Traction device consists of housing made in form of circular beam, resilient elements representing radially oriented lobes of rectangular section, connecting the device housing and the process flange, on which the tested engine is attached, and their number, length and profile parameters provide the required natural frequency of the structure, which is not less than ten times higher than the frequency of the measured thrust pulses, in addition, the device employs high-precision laser displacement sensors which, during operation of the engine, can be installed either in a pressure chamber in a sealed housing or outside it.;EFFECT: invention provides higher accuracy of pulsed thrust measurements.;4 cl, 2 dwg
机译:用于低推力液体推进剂火箭发动机的试验台技术领域本发明涉及用于低推力液体推进火箭发动机(LTLPRE)的试验台。牵引装置包括以圆形梁形式制成的壳体,代表径向截面的矩形凸角的弹性元件,它们连接装置壳体和过程法兰,测试发动机安装在该过程法兰上,它们的数量,长度和轮廓参数提供了所需的该结构的固有频率不小于测得的推力脉冲频率的十倍,此外,该设备还采用了高精度的激光位移传感器,该传感器在发动机运行期间可以安装在压力较大的位置效果:本发明提供了更高的脉冲推力测量精度; 4 cl,2 dwg

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