Abstract A fuel control system has a positive displacement gear pump for supplying a metered fuel flow to a gas turbine engine. A variable speed drive mechanism, as constituted by a hysteresis type of electro-magnetic clutch driven by the engine, is operatively connected to the pump for varying the speed of the pump in accordance with a commanded pump speed signal. A scheduling device, which senses various engine parameters, generates a signal indicative of a scheduled fuel flow. The fuel flow signal is, in turn, applied to a function generator which supplies the commanded pump speed signal in accordance with a predetermined relationship between pump speed and fuel flow for the engine sought to be controlled. The relationship between pump speed and fuel flow may be calculated for a wide range of flight conditions since the pressure rise or head across the pump is basically a function of fuel flow. This arrangement obviates the use of a head regulator for highly accurate fuel metering.
Inventors
👤 Dennis G. A. Burnell
Bibliographic Details
Application Number—
JurisdictionUS
Data Sourcegoogle_patents
Last Synchronized2026-10-27 08:31
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/30
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
252 words
A fuel control system for a gas turbine engine having burner nozzles comprising: a scheduling computer to sense selected engine parameters and calculate a scheduled fuel flow, the scheduling computer being adapted to generate a requested fuel flow signal; a positive displacement metering pump for pumping a metered flow of fuel to the burner nozzles such that both fuel flow and the pressure head across the pump increase with the speed of the metering pump; a variable speed drive mechanism drivingly connected to the metering pump to run the metering pump at the commanded speed; a speed sensing device operatively connected to the metering pump for generating a feedback signal indicative of the actual speed of the metering pump; means responsive to the scheduled fuel flow to generate a commanded pump speed signal which compensates for the affect on fuel flow of the variation in pressure head with pump speed such that the commanded pump speed signal requests a pump speed which delivers the scheduled fuel flow to the burner nozzles, the scheduled fuel flow responsive means comprising: a function generator for receiving the requested fuel flow signal and generating the commanded pump speed signal in approximate accordance with the following equation: N.sub.p = K W.sub.f.sup.2 + K' W.sub.f - K" wherein: N p is pump speed; W f is fuel flow; K, k', and K" are constants; and means to sum the commanded pump speed signal and the feedback signal for directing an error signal to the variable speed drive mechanism.
Claim 2
Dependent Claim
252 words
A fuel control system for a gas turbine engine having burner nozzles comprising: a scheduling computer to sense selected engine parameters and calculate a scheduled fuel flow, the scheduling computer being adapted to generate a requested fuel flow signal; a positive displacement metering pump for pumping a metered flow of fuel to the burner nozzles such that both fuel flow and the pressure head across the pump increase with the speed of the metering pump; a variable speed drive mechanism drivingly connected to the metering pump to run the metering pump at the commanded speed; a speed sensing device operatively connected to the metering pump for generating a feedback signal indicative of the actual speed of the metering pump; means responsive to the scheduled fuel flow to generate a commanded pump speed signal which compensates for the affect on fuel flow of the variation in pressure head with pump speed such that the commanded pump speed signal requests a pump speed which delivers the scheduled fuel flow to the burner nozzles, the scheduled fuel flow responsive means comprising: a function generator for receiving the requested fuel flow signal and generating the commanded pump speed signal in approximate accordance with the following equation: N.sub.p = K W.sub.f.sup.2 + K' W.sub.f - K" wherein: N p is pump speed; W f is fuel flow; K, k', and K" are constants; and means to sum the commanded pump speed signal and the feedback signal for directing an error signal to the variable speed drive mechanism.