Gas turbine fuel control apparatus.

摘要

In a turbine engine (10) having an operational control member (34) for regulating the flow rate of fuel supplied the turbine engine (10) as a function of atmospheric pressure and the temperature of air supplied to a compressor (16, 18) corresponding to movement of a power lever (36) by an operator to a desired operation of the turbine engine (10). The power lever (36) has an indicator member (66) fluidically connected to a follower member (78) linked to the operational control member (34). The fluidic connection (108) is responsive to operational parameters of the turbine engine (10) and limits the rotational input to the follower member (78) when the rate of fuel flow could cause stalling and the development of an unacceptable operating temperature or overspeed condition in the turbine engine (10).