US4411133A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel circuits for fuel controls
Assignee: RTX Corp
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Filing: 1980-09-29
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Granted: 1983-10-25
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Expires: 2000-09-29
Abstract
Abstract The fuel flow for a turboprop or turboshaft engine is provided by a plurality of parallel circuits each of which supplies a portion of the fuel to the engine with different valves controlling the flow through each of the separate circuits. In the turboprop engine there is imposed on the parallel flow circuits a sensing device that determines the pressures in certain of the circuits and selects the appropriate pressure for signalling a pressure regulating valve whereby to vary the pressure drop through the fuel control.
Inventors
- 👤 Charles F. Stearns
- 👤 Herbert W. Tutherly
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 06:29
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/28
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
95 words
A hydromechanical fuel control for controlling fuel flow to a gas turbine engine including: three parallel flow circuits between an inlet and an outlet to the engine; a first circuit including a motor valve responsive to engine power requirements dividing into one branch with a first throttle valve window and another branch with a servo valve window; a second circuit including a second throttle valve window in parallel with the servo valve window of said first circuit; and a third circuit including valve means providing fuel flow as a function of a compressor discharge pressure.
Claim 2
Dependent Claim
95 words
A hydromechanical fuel control for controlling fuel flow to a gas turbine engine including: three parallel flow circuits between an inlet and an outlet to the engine; a first circuit including a motor valve responsive to engine power requirements dividing into one branch with a first throttle valve window and another branch with a servo valve window; a second circuit including a second throttle valve window in parallel with the servo valve window of said first circuit; and a third circuit including valve means providing fuel flow as a function of a compressor discharge pressure.
Claim 3
Dependent Claim
25 words
A fuel control as in claim 1 in which the motor valve of the first circuit is actuated by a motor sensitive to engine requirements.
Claim 4
Dependent Claim
33 words
A fuel control as in claim 1 in which an electrical control operates in conjunction with the hydromechanical control and the motor valve of the first circuit is responsive to said electronic control.
Claim 5
Dependent Claim
20 words
A fuel control as in claim 1 in which a pressure control valve is in parallel with the motor valve.
Claim 6
Dependent Claim
119 words
A hydromechanical fuel control for controlling the fuel flow to a gas turbine engine of a turboprop or turboshaft configuration including: three parallel flow circuits between a fuel inlet port and an outlet port to the engine; a first circuit including a motor valve and branch lines from said valve to the outlet, one branch line having a servo window and the other branch line having two throttle valve windows in series, one of said two windows being open at all normal operating speeds; a second circuit including a throttle valve window in series with said one of said two windows in the first circuit; and a third circuit including a servo valve window responsive to an engine parameter.
Claim 7
Dependent Claim
119 words
A hydromechanical fuel control for controlling the fuel flow to a gas turbine engine of a turboprop or turboshaft configuration including: three parallel flow circuits between a fuel inlet port and an outlet port to the engine; a first circuit including a motor valve and branch lines from said valve to the outlet, one branch line having a servo window and the other branch line having two throttle valve windows in series, one of said two windows being open at all normal operating speeds; a second circuit including a throttle valve window in series with said one of said two windows in the first circuit; and a third circuit including a servo valve window responsive to an engine parameter.
Claim 8
Dependent Claim
23 words
A hydromechanical fuel control as in claim 5 in which the motor is a torque motor sensitive to torque requirements of the engine.
Claim 9
Dependent Claim
21 words
A fuel control as in claim 5 including a pressure relief valve to maintain a selected pressure across the motor valve.
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) | 1986-10-24 | 1987-04-25 | 1987-10-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-10-24 | 1991-04-25 | 1991-10-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-10-24 | 1995-04-25 | 1995-10-25 | $7700.00 | Window Closed / Lapsed |