Electronic fuel control for a gas turbine engine

• US 4,018,044 A
• Filed: 07/07/1975
• Issued: 04/19/1977
• Est. Priority Date: 07/09/1974
• Status: Expired due to Term

• Current Assignee: Lucas Industries Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Original Assignee: Lucas Industries Limited (Zeppelin - Stiftung der Stadt Friedrichshafen)
• Inventors: Maker, Paul Manwaring, Joby, Michael John
• Primary Examiner(s): Freeh, William L.
• Assistant Examiner(s): Garrett, Robert E.
• Application Number:
  US05/593,388
• Time in Patent Office: 652 Days
• Field of Search: 60/39.28 R, 60/39.16 R
• US Class Current: 60/791
• CPC Class Codes: F02C 9/32 characterised by throttling of fuel F02C9/38 takes precedence
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An electronic fuel control for a gas turbine engine having a gas generator and a separate power turbine includes gas generator and power turbine actual speed transducers, gas generator and power turbine desired speed signal generators, error amplifiers connected to the respective transducers and generators, a "low wins" gate for selecting the lower error, an acceleration control limiter passing the selected signal from the gate to an integrator and an output difference amplifier producing an output signal determined by the difference between the integrator output and that of the gas generator transducer to control the fuel flow to the engine.

Claims

1. An electronic fuel control for a gas turbine engine having a gas turbine gas generator and a separate power turbine driven by the gas generator, the control comprising means for generating a gas generator speed demand signal, a first difference amplifier for comparing said gas generator speed demand signal with a gas generator actual speed signal to produce a gas generator speed error signal, means for generating a power turbine speed demand signal, a second difference amplifier for comparing the power turbine speed demand signal with a power turbine actual speed signal to produce a power turbine speed error signal, an error signal selection circuit connected to said difference amplifiers and arranged to pass forward the lower of said error signals, an acceleration control connected to limit the magnitude of the selected error signal, an integrator for integrating the selected error signal, an output difference amplifier for comparing the output of the integrator with the gas generator actual speed signal to produce a fuel error signal and a fuel flow control device sensitive to said fuel error signal to vary the flow of fuel to the engine.

2. An electronic fuel control as claimed in claim 1 in which said acceleration control is sensitive only to the output of the output difference amplifier to determine the limit applied to the selected error signal.

3. An electronic fuel control as claimed in claim 1 including means sensitive to the gas generator actual speed signal for disconnecting the fuel flow control device from the output difference amplifier when the gas generator actual speed signal is below a predetermined value.

4. An electronic fuel control as claimed in claim 1 in which the means for generating the gas generator speed demand signal comprises a manual control element, and a pair of scheduling devices operated by said manual control element one of said scheduling devices providing an output which is constant over an initial part of the range of movement of the manual control element and rises thereafter and which provides a signal to the first difference amplifier, and the other of said scheduling devices provides an output which rises in said initial part of the range of movement of the manual control element and is constant thereafter, and means sensitive to the sign of the error signal from the first difference amplifier for connecting said second scheduling device to the second difference amplifier instead of the means for generating the power turbine speed demand signal when the output of the first difference amplifier is positive during starting of the engine.

5. An electronic fuel control as claimed in claim 4 further comprising a first summing amplifier connected to the output terminal of the other scheduling device and arranged to add a fixed offset signal to the output of the other scheduling device, and a further summing amplifier connected to the output of the other scheduling device and to the gas generator actual speed signal via a resistance network, and a selector device sensitive to the gas generator actual speed signal for determining which of said summing amplifiers is connected to said sign-sensitive means during starting.