Electronic fuel control system
First Claim
1. A fuel control system for gas turbine engines, comprising:
- a hydromechanical fuel section for providing fuel flow to the engine at commanded power settings and including means for augmenting said fuel flow in response to a fuel flow modifying signal, andsignal processing means for providing said fuel flow modifying signal in response to signals applied thereto, said signals reflecting power setting, engine speed and ambient and engine conditions,characterized in that said processing means comprises means for providing a correction signal which is summed with an engine speed signal, said correction signal being selected from a plurality of signals each reflecting a maximum engine speed, at least one of said signals being related to the power setting, engine speed and any difference between engine speed and a scheduled engine speed for the particular power setting in such a way as to reflect the required change, if any, in engine speed in order to produce, between actual engine speed and maximum engine speed, a ratio which is the same as the ratio between the actual power setting and the maximum power setting.
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Abstract
Fuel flow to a gas turbine engine is controlled in response to power lever position and CDP by a hydromechanical section. The hydromechanical section includes a torque motor which may be activated to modify the fuel flow to the engine in response to a control signal produced by an electronic control section. The electronic control section senses a number of engine and ambient parameters and generates engine operating limits from these parameters. The limit corresponding to the lowest maximum engine speed is selected and referenced to actual engine speed for generating the control signal, thereby providing a closed loop engine speed control. At least one of the computed limits is an actual maximum engine speed for steady state engine operation and is used to recompute the engine scheduled speed so that the actual maximum engine speed is obtained at the maximum power lever advance position; in this way power lever dead band is eliminated. The electronic control also modifies fuel flow to the engine for speed synchronization with another identically controlled engine.
48 Citations
7 Claims
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1. A fuel control system for gas turbine engines, comprising:
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a hydromechanical fuel section for providing fuel flow to the engine at commanded power settings and including means for augmenting said fuel flow in response to a fuel flow modifying signal, and signal processing means for providing said fuel flow modifying signal in response to signals applied thereto, said signals reflecting power setting, engine speed and ambient and engine conditions, characterized in that said processing means comprises means for providing a correction signal which is summed with an engine speed signal, said correction signal being selected from a plurality of signals each reflecting a maximum engine speed, at least one of said signals being related to the power setting, engine speed and any difference between engine speed and a scheduled engine speed for the particular power setting in such a way as to reflect the required change, if any, in engine speed in order to produce, between actual engine speed and maximum engine speed, a ratio which is the same as the ratio between the actual power setting and the maximum power setting. - View Dependent Claims (2, 3, 4, 5)
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6. A fuel control system comprising:
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a hydromechanical fuel section for providing fuel flow to the engine at commanded power settings and including means for augmenting said fuel flow in response to a fuel flow modifying signal, and signal processing means for providing said fuel flow modifying signal in response to signals applied thereto, said signals reflecting power setting, engine speed and ambient and engine conditions, characterized in that said processing means comprises means for providing a correction signal which is summed with an engine speed signal, said correction signal being selected from a plurality of signals each reflecting a maximum engine speed, at least one of said signals being related to the power setting, engine speed and any difference between engine speed and a scheduled engine speed for the particular power setting in such a way as to reflect the required change, if any, in engine speed in order to produce between actual engine speed and maximum engine speed a ratio which is the same as the ratio between the actual power setting and the maximum power setting, and in that said signal processing means further comprises means responsive to an engine operating speed signal and a speed signal of a second remote engine for providing a signal for modifying said speed correction in relation to an asynchronization parameter having a magnitude manifesting a difference, if any, in speed between the two engines. - View Dependent Claims (7)
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Specification