摘要
为了改善某型发动机加速性，进行了大量的试验研究，采取了多种技术措施。其中最有效的就是适当加大“Ｃ”节流器的流量和改变放油针油槽的结构设计。
In order to improve the acceleration characteristics of a given aeroengine,a great deal of experimental investigations have been carried out and various technical measures have been taken.The most effective measures are enlarging the discharge of the 'C' throttle unit and modifying the structure of the metering pin oil groove.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1995年第4期412-414,共3页
Journal of Aerospace Power
