US4473999A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel control system for a gas turbine engine
Assignee: ZF International UK Ltd
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Filing: 1981-11-16
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Granted: 1984-10-02
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Expires: 2001-11-16
Abstract
Abstract A fuel control system for a gas turbine engine comprises a variable metering device and a flow limiting valve arranged in series. The limiting valve is servo pressure operated to reduce fuel flow in response to unacceptably high levels of certain engine operating conditions and is additionally movable to a fully shut condition when the engine is stopped. The servo operating pressure is controlled by an electrically actuated pilot valve which can be energized to a first level to provide flow limitation, and to a second, higher level to effect shut down. The pilot valve can also be energized in a reverse direction to open the limiting valve when starting the engine.
Inventors
- 👤 Trevor S. Smith
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 13:41
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
280 words
A fuel control system for a gas turbine engine, comprising a variable metering device and a flow limiting valve in series with said metering device, said limiting valve including a flow control element, means for applying a servo pressure and a biasing pressure to said control element to urge the latter in respective opposite directions, a first pilot valve for regulating said servo pressure, means for biasing said first pilot valve in dependence on the operating position of said control element, an electrical actuating device for urging said first pilot valve against said biasing means, means for energising said actuating device in a first direction at a first level at which the force exerted thereby is balanced by said biasing means at an intermediate position of said control element, means for energising said actuating device in said first direction at a second level at which the force exerted thereby overcomes said biasing means in all operating positions of said control element to set said servo pressure at a level at which said flow control element is urged to a shut position, valve means operable by said control element in said shut position thereof for modifying one of said pressures to maintain said control element in said shut position, and a second pilot valve operable by energisation of said actuating device in a second direction to restore said one pressure to its unmodified state, whereby operation of said valve means causes said control element to be maintained in its shut position independently of the operating position of said first pilot valve, and operation of said second pilot valve renders said control element responsive to subsequent operation of said first pilot valve.
Claim 2
Dependent Claim
280 words
A fuel control system for a gas turbine engine, comprising a variable metering device and a flow limiting valve in series with said metering device, said limiting valve including a flow control element, means for applying a servo pressure and a biasing pressure to said control element to urge the latter in respective opposite directions, a first pilot valve for regulating said servo pressure, means for biasing said first pilot valve in dependence on the operating position of said control element, an electrical actuating device for urging said first pilot valve against said biasing means, means for energising said actuating device in a first direction at a first level at which the force exerted thereby is balanced by said biasing means at an intermediate position of said control element, means for energising said actuating device in said first direction at a second level at which the force exerted thereby overcomes said biasing means in all operating positions of said control element to set said servo pressure at a level at which said flow control element is urged to a shut position, valve means operable by said control element in said shut position thereof for modifying one of said pressures to maintain said control element in said shut position, and a second pilot valve operable by energisation of said actuating device in a second direction to restore said one pressure to its unmodified state, whereby operation of said valve means causes said control element to be maintained in its shut position independently of the operating position of said first pilot valve, and operation of said second pilot valve renders said control element responsive to subsequent operation of said first pilot valve.
Claim 3
Dependent Claim
48 words
A system as claimed in claim 1 in which said actuating device has two energisable elements, said energising means comprising means energising one of said elements to provide said first level of energisation, and for energising both of said energisable elements to provide said second level of energisation.
Claim 4
Dependent Claim
46 words
A system as claimed in claim 1 in which said actuating device has two energisable elements, said energising means comprising means for energising both of said elements at said first level of energisation, and for energising both of said elements at said second level of energisation.
Claim 5
Independent Claim
52 words
A system as claimed in any preceding claim in which said limiting valve includes first and second parallel orifices through which fuel can flow from said metering device to said engine, said biassing means being settable so that said second orifice remains open in said intermediate position of said flow control element.
Claim 6
Dependent Claim
28 words
A system as claimed in claim 1 in which said first pilot valve is in a fuel flow path to the engine from upstream of said metering device.
Claim 7
Dependent Claim
44 words
A system as claimed in claim 1 in which said variable metering device comprising a control member responsive to a second servo pressure, said system including means for maintaining a substantially constant pressure difference between an inlet and an outlet of said metering device.
Claim 8
Dependent Claim
38 words
A system as claimed in claim 1 in which said energising means comprises a circuit responsive to a speed of the engine to provide an energising signal at said first level when said speed exceeds a predetermined limit.
Claim 9
Dependent Claim
46 words
A system as claimed in claim 7 in which said energising means comprises means for supplying an electrical signal indicative of a requirement to shut off fuel flow to the engine, said circuit being responsive to said shut-off signal to provide said second level energising signal.
Claim 10
Dependent Claim
48 words
A system as claimed in claim 1, in which said limiting valve flow control element includes means, operable in said end position of the control element, for maintaining said first servo pressure at a level which causes said flow control element to be held in said end position.
Claim 11
Dependent Claim
16 words
A system as claimed in claim 1 in which said one pressure is said servo pressure.
Claim 12
Dependent Claim
16 words
A system as claimed in claim 1 in which said one pressure is said biasing pressure.
References Cited (Backward Citations)
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Cited
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Cited
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Cited
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Cited
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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) | 1987-10-02 | 1988-04-02 | 1988-10-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-10-02 | 1992-04-02 | 1992-10-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-10-02 | 1996-04-02 | 1996-10-02 | $7700.00 | Window Closed / Lapsed |