US4437303A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel control system for a gas turbine engine
Assignee: Rolls Royce PLC
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Filing: 1981-11-10
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Granted: 1984-03-20
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Expires: 2001-11-10
Abstract
Abstract 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.
Inventors
- 👤 Hugh F. Cantwell
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 06:11
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/02; F05D2270/021; F05D2270/05; F05D2270/051; F05D2270/70; F05D2270/71
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
177 words
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.
Claim 2
Dependent Claim
177 words
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.
Claim 3
Dependent Claim
55 words
A fuel control system as claimed in claim 1 in which said trimmer device includes means for determining a second trim setting in accordance with the error between an actual value of a second thrust-related parameter of the engine and a desired value calculated from the throttle lever setting and other parameters of the engine.
Claim 4
Dependent Claim
65 words
A fuel control system as claimed in claim 2 in which said trimmer device further includes a model of the performance of the engine in which the value of said first thrust-related parameter corresponding with the other engine parameters and throttle lever setting is calculated and from which value said predicted value of the first thrust-related parameter is subtracted to produce said first trim setting.
Claim 5
Dependent Claim
40 words
A fuel control system as claimed in claim 1 and including means for operating said main fuel control unit as a closed loop system in which the actual value of the first thrust-related parameter is compared with the demanded value.
Claim 6
Dependent Claim
30 words
A fuel control system as claimed in claim 1 and including means for operating said trimmer device in a closed loop fashion by comparing the actual trim with that demanded.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-03-20 | 1987-09-19 | 1988-03-20 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-03-20 | 1991-09-19 | 1992-03-20 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-03-20 | 1995-09-19 | 1996-03-20 | $7700.00 | Window Closed / Lapsed |