Patent US4528812A successfully refreshed from Google Patents.
US4528812A
Expired / Lapsed
US
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Fuel control system for a gas turbine engine
Assignee: Rolls Royce PLC
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Filing: 1983-07-14
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Granted: 1985-07-16
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Expires: 2003-07-14
Abstract
Abstract A fuel control system for a gas turbine engine comprises a main fuel controller and an overspeed limiter arranged to prevent overspeed of the engine in the case of a fault in the main controller. To ensure that the limiter is tested regularly, the logic capacity of the main controller (which is preferably a digital electronic unit) is used to vary the parameters of the limiter each time the engine is started up. This variation is such as to cause the limiter to operate and produce an observable reduction in the engine speed which is detected by the main controller and uses as an indication of correct limiter operation.
Inventors
- 👤 Hugh F. Cantwell
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 19:33
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28; F05; F05D; F05D2270/00; F05D2270/01; F05D2270/02; F05D2270/021; F05D2270/09; F05D2270/094
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
193 words
A fuel control system for a gas turbine engine comprising: transducer means for generating a signal corresponding to a value related to the thrust of the engine; a main fuel control including computing means connected to receive said thrust related signal and to generate a first control signal representative of the fuel required in said engine and a second limiter control signal; an overspeed limiter connected to receive said thrust related signal and connected to receive said second limiter control signal, said overspeed limiter having means for producing an overspeed control signal in response to said thrust related signal; and fuel control means for reducing the fuel flow in response to said overspeed control signal to prevent excessive oversupply of fuel to said engine in the event of failure of said main fuel control; said overspeed limiter being adapted to produce said overspeed control signal upon receipt of said second limiter control signal, said computing means including means for periodically generating said second limiter control signal and for determining in response to the variation of said thrust related signal whether said overspeed limiter is operating in response to said second limiter control signal.
Claim 2
Dependent Claim
193 words
A fuel control system for a gas turbine engine comprising: transducer means for generating a signal corresponding to a value related to the thrust of the engine; a main fuel control including computing means connected to receive said thrust related signal and to generate a first control signal representative of the fuel required in said engine and a second limiter control signal; an overspeed limiter connected to receive said thrust related signal and connected to receive said second limiter control signal, said overspeed limiter having means for producing an overspeed control signal in response to said thrust related signal; and fuel control means for reducing the fuel flow in response to said overspeed control signal to prevent excessive oversupply of fuel to said engine in the event of failure of said main fuel control; said overspeed limiter being adapted to produce said overspeed control signal upon receipt of said second limiter control signal, said computing means including means for periodically generating said second limiter control signal and for determining in response to the variation of said thrust related signal whether said overspeed limiter is operating in response to said second limiter control signal.
Claim 3
Dependent Claim
20 words
A fuel control system as claimed in claim 1 and in which the computing device comprises a digital electronic device.
Claim 4
Dependent Claim
30 words
A fuel control system as claimed in claim 1 and in which said computing device is programmed to output said second limiter control signal upon start up of the engine.
Claim 5
Dependent Claim
34 words
A fuel control system as defined in claim 2 wherein said computing device includes at least one engine modeling circuit and wherein thrust related parameters for generating said second limiter control signals are generated.
Claim 6
Dependent Claim
39 words
The fuel control system of claim 3 in which said computing device is programmed not to produce said second limiter control signal if the thrust demanded from the engine is greater than a predetermined value immediately after engine start-up.
Claim 7
Dependent Claim
37 words
The fuel control system of claim 1 wherein said second limiter control signal includes means for generating a control signal to said overspeed limiter to lower the threshold at which said overspeed limiter is set to operate.
Claim 8
Dependent Claim
44 words
The fuel control system of claim 1 further comprising means responsive to said second limiter control signal for minimizing said transducer signal output at a level indicating a false value of said thrust related parameter which indicates an oversupply of fuel to the engine.
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) | 1988-07-15 | 1989-01-14 | 1989-07-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-07-15 | 1993-01-14 | 1993-07-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-07-15 | 1997-01-14 | 1997-07-16 | $7700.00 | Window Closed / Lapsed |