Patent US5116362A successfully refreshed from Google Patents.
US5116362A
Expired / Lapsed
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Fuel metering and actuation system
Assignee: RTX Corp
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Filing: 1990-12-03
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Granted: 1992-05-26
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Expires: 2010-12-03
Abstract
Abstract A fuel metering and actuation system includes a main centrifugal pump 16 supplying fuel to the combustor 18. Gear pump 50 takes suction from the main pump discharge and supplies actuators 42, 44, 45, 46 at high pressure. Variable set point pressure relief valve 56 operates to decrease the gear pump pressure level when high pressure is not required. Selection valve 21 directs discharge from the gear pump 50 to the combustor 18 when the main pump 16 supplied insufficient pressure for the fuel nozzles. Bypass line 30 around the selector valve with check valve 82 permits main pump 16 discharge fuel to be used for the actuator if the gear pump 50 becomes inoperative.
Inventors
- 👤 Samuel B. Arline
- 👤 Matthias Eder
- 👤 Jeffrey J. Dunlap
- 👤 Gary W. Douglas
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 09:06
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/22; F02C7/236
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
161 words
A fuel metering and actuation system for a gas turbine engine aircraft having a fuel tank comprising: a centrifugal boost fuel pump; a centrifugal main fuel pump; a combustor; a suction line from the discharge of said boost pump to the suction of said main pump; a discharge line free of additional pumps from the discharge of said main pump to said combustor; a plurality of actuators; a gear pump; a gear pump supply line from said discharge line to said gear pump; a gear pump exit line from said gear pump to said plurality of actuators; a pressure relief line from said exit line; a selector valve located in said discharge line downstream of said gear pump supply line connection; an alternate supply line from said exit line to said selector valve; and said selector valve in said discharge line connected to alternatively receive flow from said main pump or said gear pump, and in fluid communication with said combustor.
Claim 2
Dependent Claim
161 words
A fuel metering and actuation system for a gas turbine engine aircraft having a fuel tank comprising: a centrifugal boost fuel pump; a centrifugal main fuel pump; a combustor; a suction line from the discharge of said boost pump to the suction of said main pump; a discharge line free of additional pumps from the discharge of said main pump to said combustor; a plurality of actuators; a gear pump; a gear pump supply line from said discharge line to said gear pump; a gear pump exit line from said gear pump to said plurality of actuators; a pressure relief line from said exit line; a selector valve located in said discharge line downstream of said gear pump supply line connection; an alternate supply line from said exit line to said selector valve; and said selector valve in said discharge line connected to alternatively receive flow from said main pump or said gear pump, and in fluid communication with said combustor.
Claim 3
Dependent Claim
39 words
A fuel metering and actuation system as in claim 1: said pressure relief line including a pressure relief valve having an adjustable pressure set point; and means for adjusting said set point pressure as a function of flight conditions.
Claim 4
Dependent Claim
35 words
A fuel metering and actuation system as in claim 2: a filter located in said discharge line; and said gear pump supply line connected to said discharge line at a location downstream of said filter.
Claim 5
Dependent Claim
27 words
A fuel metering and actuation system as in claim 3: said pressure relief line from said pressure relief valve connected to a location upstream of said filter.
Claim 6
Dependent Claim
69 words
A fuel metering and actuation system as in claim 3: a wash filter in said exit line having a flowpath through the filter mesh for entrapping particles, and a flowpath along said filter mesh washing away filter particles; said exit line connected to pass flow to said actuators through said filter mesh; and said pressure relief line connected to carry flow across said filter to said pressure relief valve.
Claim 7
Dependent Claim
44 words
A fuel metering and actuation system as in claim 3: a bypass, line from said discharge line to said exit line; and a check valve located in said bypass line permitting flow only in the direction from said discharge line to said exit line.
Claim 8
Dependent Claim
49 words
A fuel metering and actuation system as in claim 6: said bypass line connected to said exit line at a location between said wash filter and said plurality of actuators, whereby flow passing through said bypass line need not pass through said wash filter en route to said actuators.
Claim 9
Dependent Claim
42 words
A fuel metering and actuation system as in claim 6: a heat exchanger located in said discharge line for accepting heat for cooling of other components; and a recirculating line downstream of said heat exchanger for returning fuel to the fuel tank.
Claim 10
Dependent Claim
31 words
A fuel metering and actuation system as in claim 8: an afterburner; and an afterburner supply line taking flow from said discharge line at a location upstream of said heat exchanger
Claim 11
Dependent Claim
69 words
A fuel metering and actuation system as in claim 1: a wash filter in said exit line having a flowpath through the filter mesh for entrapping particles, and a flowpath along said filter mesh washing away filter particles; said exit line connected to pass flow to said actuators through said filter mesh; and said pressure relief line connected to carry flow across said filter to said pressure relief valve.
Claim 12
Dependent Claim
44 words
A fuel metering and actuation system as in claim 1: a bypass line from said discharge line to said exit line; and a check valve located in said bypass line permitting flow only in the direction from said discharge line to said exit line.
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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) | 1995-05-26 | 1995-11-25 | 1996-05-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-05-26 | 1999-11-25 | 2000-05-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-05-26 | 2003-11-25 | 2004-05-26 | $7700.00 | Window Closed / Lapsed |