US4380148A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Device for adjusting gas turbine engine fuel control system in accordance with engine parameter
Assignee: ZF International UK Ltd
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Filing: 1980-09-19
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Granted: 1983-04-19
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Expires: 2000-09-19
Abstract
Abstract A gas turbine engine fuel control system includes an hydromechanical speed governor fuel flow control with an electromechanical trim. The trim is controlled by a proportional-plus-integral controller in accordance with the error signal from an error amplifier comparing an engine parameter with a desired value of that parameter. A trim datum signal is produced by a suitable generator circuit and, if the error signal (or its rate of charge) exceeds a set maximum, the integrator is set to a new value.
Inventors
- 👤 Robert G. Burrage
- 👤 Michael J. Joby
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 17:46
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28; G; G05; G05B; G05B5/00; G05B5/01
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
194 words
A fuel control system for a gas turbine engine of the kind including a hydromechanical speed governor fuel control in which a fuel valve is movable under the influence of a control input element, operable for example by the pilot of an aircraft in which the engine is installed, and speed sensing means, the effect of said control input element on said fuel valve being variable through the intermediary of an electromechanical trim device controlled by an electronic control circuit sensitive to at least one engine parameter, wherein said electronic control circuit includes error signal generating means for producing an error signal representing the difference between the desired and actual values of said engine parameter, a proportional-plus-integral controller circuit for producing the output signal which is applied to said electromechanical trim device, means for generating a trim datum signal dependent on the control input and means for setting the integrator included in the proportional-plus-integral control circuit to a value corresponding to the difference between the trim datum signal and the output of the proportional part of the proportional-plus-integral control circuit when the magnitude of a function of the error signal exceeds a predetermined value.
Claim 2
Dependent Claim
194 words
A fuel control system for a gas turbine engine of the kind including a hydromechanical speed governor fuel control in which a fuel valve is movable under the influence of a control input element, operable for example by the pilot of an aircraft in which the engine is installed, and speed sensing means, the effect of said control input element on said fuel valve being variable through the intermediary of an electromechanical trim device controlled by an electronic control circuit sensitive to at least one engine parameter, wherein said electronic control circuit includes error signal generating means for producing an error signal representing the difference between the desired and actual values of said engine parameter, a proportional-plus-integral controller circuit for producing the output signal which is applied to said electromechanical trim device, means for generating a trim datum signal dependent on the control input and means for setting the integrator included in the proportional-plus-integral control circuit to a value corresponding to the difference between the trim datum signal and the output of the proportional part of the proportional-plus-integral control circuit when the magnitude of a function of the error signal exceeds a predetermined value.
Claim 3
Dependent Claim
150 words
A fuel control system as claimed in claim 1 including a closed loop circuit including a multiplier, a further integrator connected to integrate the difference between the output of the proportional-plus-integral circuit and the output of said multiplier, one input of the multiplier being connected to the output of said trim datum signal generating means and a function generator having an input connected to the output of said further integrator and its output connected to the other input of the multiplier, said function generator producing a relatively low level constant signal at low values of the output of the further integrator and a relatively high level constant signal at high values of the output of the further integrator, and the output of the multiplier being connected to an integrator setting circuit controlled by a comparator sensitive to the rate of change of the output of the error signal generating circuit.
Claim 4
Dependent Claim
21 words
A fuel control system as claimed in claim 1, wherein the function of the error signal is the error signal itself.
Claim 5
Dependent Claim
25 words
A fuel control system as claimed in claim 1, wherein the function of the error signal is the rate of change of the error signal.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-04-18 | 1986-10-18 | 1987-04-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-04-18 | 1990-10-18 | 1991-04-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-04-18 | 1994-10-18 | 1995-04-19 | $7700.00 | Window Closed / Lapsed |