METHOD FOR REGULATING TURBOMACHINE COMPRISING TEMPORARY POWER-INCREASING DEVICE

Method for regulating a turbomachine (10) comprising a temporary power-increasing device (26), said regulating method comprising a step (E3) in which the injected refrigerant fluid flow rate is adjusted as a function of the atmospheric pressure (P0) and/or of the ambient temperature (T0) and/or of at least one parameter such as the rotational speed (N1) of a gas generator, the rotational speed (N2) of a low-pressure turbine or of a free turbine, the pressure (P3) of the gases at the outlet of a compressor stage, the temperature (T45) at the inlet of the low-pressure turbine or of the free turbine, the driving torque (TQ), and/or the collective pitch (XPC) of a helicopter rotor or the pitch of a propeller of a turboprop. 用于调节包括临时功率增加装置(26)的涡轮机(10)的方法，所述调节方法包括步骤(E3)，在该步骤中，根据以下调节注射的制冷流体流率，即大气压力(P0)和/或环境温度(T0)和/或诸如气体发生器的转速(N1)、低压涡轮或自由涡轮的转速(N2)、在压缩机级的出口处的气体压力(P3)、在低压涡轮或自由涡轮的入口处的温度(T45)、驱动扭矩(TQ)中的至少一个参数和/或直升机转子的总距(XPC)或涡轮螺旋桨发动机的螺距。