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本文根据四种涡喷发动机加力调节装置在油泵试验台和飞行试验中获得的数据,对落压比调节器和气压调节器的工作情况进行了研究。对此争论多年的问题提出了初步看法。
In this paper, according to the four types of turbojet afterburner in oil pump test bench and flight test data obtained, the work of the pressure ratio regulator and pressure regulator were studied. This issue of controversy for many years put forward a preliminary view.