초록 ▼

A fuel control system for a gas turbine engine comprises a main steady-state fuel control unit which adjusts the fuel flow to the engine to produce an approximation to a desired thrust and a trimmer device which trims the fuel flow demanded by the main unit to produce a closer approximation to the d

A fuel control system for a gas turbine engine comprises a main steady-state fuel control unit which adjusts the fuel flow to the engine to produce an approximation to a desired thrust and a trimmer device which trims the fuel flow demanded by the main unit to produce a closer approximation to the desired thrust. During transients such as accelerations a trimmer suitable for steady operation will apply zero trim until the desired thrust is almost attained, when an amount of trim may have to be applied rapidly. This can lead to overshoots. To mitigate the problem the trimmer is provided with a model of the main control unit which derives an approximation to the trim which will be required when the steady state is reached. This is applied to the main unit throughout the transients, and when the desired thrust is achieved only second-order changes need to be made.

대표청구항 ▼

A fuel control system for a gas turbine engine comprising transducers for producing signals related to parameters of the engine, including at least one thrust-related parameter, a throttle lever on which a desired engine thrust may be set, a main steady-state fuel control unit which determines a val

A fuel control system for a gas turbine engine comprising transducers for producing signals related to parameters of the engine, including at least one thrust-related parameter, a throttle lever on which a desired engine thrust may be set, a main steady-state fuel control unit which determines a value of a first said thrust-related parameter corresponding with the setting of the throttle lever and controls the fuel flow to the engine to maintain the actual value of the first thrust-related parameter determined from a transducer signal at least approximately equal to the value determined by the fuel control unit, and a trimmer device which provides a more accurate control of engine thrust by trimming the fuel flow demanded by the main fuel control unit, the trimmer incorporating a model of said main fuel control unit in which the predicted value of said first thrust-related parameter determined by said main fuel control unit in accordance with the setting of the throttle lever is calculated and used to produce a first trim setting during non-steady state operation of the engine.