US4411137A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Priming device for burner manifolds of gas turbine engine
Assignee: Rolls Royce PLC
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Filing: 1981-09-28
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Granted: 1983-10-25
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Expires: 2001-09-28
Abstract
Abstract A device for priming an empty or partially full burner manifold of a gas turbine engine with fuel before it is required to supply from the burner manifold to the associated burners comprises a fuel accumulator and a control valve. A fuel pressure signal supplied to the control valve terminates the supply of relatively high pressure fuel to the fuel accumulator via the control valve. A metered quantity of fuel is supplied via the control valve to the burner manifold from the fuel accumulator by the motive force of a spring acting on a piston in the accumulator. The metered quantity of fuel is supplied via the control valve to the burner manifold, to fill the burner manifold and to prevent undesireable drops in the quantity of fuel being supplied to other manifolds when the regulated fuel is supplied to the burner manifold.
Inventors
- 👤 Maurice N. Pearce
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 17:42
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/22; F02C7/232
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
181 words
A fuel priming device for gas turbine engine burner manifolds comprising a fuel accumulator, a control valve, a control valve operating means, a regulated fuel supply, a relatively high pressure fuel supply and at least one burner manifold, the fuel accumulator and the regulated fuel supply are arranged to supply fuel sequentially to the burner manifold through the control valve, and the relatively high pressure fuel supply is arranged to supply fuel to the fuel accumulator through the control valve, the control valve being moveable by the control valve operating means from a first position in which the fuel accumulator is connected to the relatively high pressure fuel supply to a second position in which the relatively high pressure fuel supply is disconnected from the fuel accumulator and the fuel accumulator is connected to the burner manifold to provide a metered quantity of fuel to the burner manifold against a pressure in the burner manifold and a third position in which the regulated fuel supply is connected to the burner manifold and the fuel accumulator is disconnected from the burner manifold.
Claim 2
Dependent Claim
181 words
A fuel priming device for gas turbine engine burner manifolds comprising a fuel accumulator, a control valve, a control valve operating means, a regulated fuel supply, a relatively high pressure fuel supply and at least one burner manifold, the fuel accumulator and the regulated fuel supply are arranged to supply fuel sequentially to the burner manifold through the control valve, and the relatively high pressure fuel supply is arranged to supply fuel to the fuel accumulator through the control valve, the control valve being moveable by the control valve operating means from a first position in which the fuel accumulator is connected to the relatively high pressure fuel supply to a second position in which the relatively high pressure fuel supply is disconnected from the fuel accumulator and the fuel accumulator is connected to the burner manifold to provide a metered quantity of fuel to the burner manifold against a pressure in the burner manifold and a third position in which the regulated fuel supply is connected to the burner manifold and the fuel accumulator is disconnected from the burner manifold.
Claim 3
Dependent Claim
52 words
A fuel priming device for gas turbine engine burner manifolds as claimed in claim 1 in which the metered quantity of fuel being supplied from the fuel accumulator to the burner manifold against a pressure in the burner manifold is terminated when the pressure in the burner manifold reaches a predetermined level.
Claim 4
Dependent Claim
112 words
A fuel priming device for gas turbine engine burner manifolds as claimed in claim 2 in which the fuel accumulator comprises a piston being enclosed in a cylinder and defining with the cylinder a first chamber and a second chamber, the piston being moveable through said first chamber by means of a spring positioned in said second chamber to supply fuel from said first chamber to the burner manifold against a pressure in the burner manifold, the motive force of the spring being overcome by the pressure in the burner manifold and terminates the supply of the metered quantity of fuel when the pressure in the burner manifold reaches a predetermined level.
Claim 5
Dependent Claim
63 words
A fuel priming device for gas turbine engine burner manifolds as claimed in claim 3 in which the fuel accumulator has an adjustable volume control extending into the first chamber to limit the movement of the piston, the adjustable volume control may be moved to control the metered quantity of fuel supplied to the burner manifold against a pressure in the burner manifold.
Claim 6
Dependent Claim
41 words
A fuel priming device for gas turbine engine burner manifolds as claimed in any of claims 1 to 4 in which the fuel accumulator supplies fuel to the burner manifold through a variable restrictor to permit adjustment of the priming time.
Claim 7
Dependent Claim
103 words
A fuel priming device for gas turbine engine burner manifolds as claimed in claim 1 in which the control valve operating means comprises a first and second pipe means to supply a pressure operating signal to the control valve, the second pipe means having a restrictor, the pressure operating signal being supplied via first and second pipe means to move the control valve from the first position to the second position, when the supply via first pipe means is disconnected and the pressure operating signal being supplied via second pipe means to move control valve from the second position to the third position.
Claim 8
Dependent Claim
62 words
A fuel priming device for gas turbine engine burner manifolds as claimed in claim 6 in which the control valve operating means also comprises a third pipe means with a non-return valve, the third pipe means releases the pressure in the control valve to the first pipe means when the pressure operating signal ceases and returns control valve to said first position.
Claim 9
Dependent Claim
48 words
A fuel priming device for gas turbine engine burner manifolds, as claimed in any of claims 1, 2, 3, 4, 6 or 7 in which the burner manifold is used to supply fuel to the main fuel burners in combustion chambers of gas turbine engines operating staged burning.
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 |