US6065281A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Liquid fuel injector and injector system for a small gas turbine engine
Assignee: Capstone Green Energy Corp
•
Filing: 1999-07-19
•
Granted: 2000-05-23
•
Expires: 2019-07-19
Abstract
Abstract The liquid fuel injector includes continuous air assist with both the liquid fuel injector tube and the surrounding air assist tube constrained or reduced in diameter at the discharge ends thereof. The associated gas turbine engine compressor provides combustion air to the combustor and also air for continuous air assist with a separate air pump. The air assist air may be cooled in a heat exchanger either before or after the separate air pump. The liquid fuel injector may be mounted within an annular air blast tube and directed tangentially at the inner wall of the combustor. A solenoid valve controlled purge line, together with solenoid valves in the liquid fuel and air assist lines can be utilized to purge any liquid fuel in the liquid fuel injector and manifold upon shutdown of the combustor. The liquid fuel injector can also be insulated and liquid fuel can be used to cool the fuel injector.
Inventors
- 👤 Jack R. Shekleton
- 👤 Curtis C. Martin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 23:46
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/22; F02C7/232; F02C7/236; F23; F23R; F23R3/00; F23R3/42; F23R3/50; F05; F05D; F05D2260/00; F05D2260/60; F05D2260/602; F23D; F23D2209/00; F23D2209/30
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
179 words
A liquid fuel injector purge system for a gas turbine engine, comprising: an annular combustor having an outer wall, an inner wall, a closed upstream end, and an open discharge end; a plurality of liquid fuel injectors spaced around the periphery of the closed end of said combustor to direct liquid fuel/air into said combustor; a liquid fuel inlet conduit to each of said plurality of liquid fuel injectors, said liquid fuel inlet conduit having a liquid fuel control valve and a liquid fuel on/off solenoid valve; an air assist conduit to each of said plurality of liquid fuel injectors, and a liquid fuel purge conduit extending from said liquid fuel conduit, disposed between said liquid fuel on/off solenoid valve and said plurality of liquid fuel injectors, and having a purge line solenoid valve and a restrictive orifice, so that when said gas turbine engine is shut down and said liquid fuel inlet or/off solenoid valve is closed, liquid fuel is sucked through the liquid fuel purge line restrictive orifice with the liquid fuel purge line solenoid valve open.
Claim 2
Dependent Claim
179 words
A liquid fuel injector purge system for a gas turbine engine, comprising: an annular combustor having an outer wall, an inner wall, a closed upstream end, and an open discharge end; a plurality of liquid fuel injectors spaced around the periphery of the closed end of said combustor to direct liquid fuel/air into said combustor; a liquid fuel inlet conduit to each of said plurality of liquid fuel injectors, said liquid fuel inlet conduit having a liquid fuel control valve and a liquid fuel on/off solenoid valve; an air assist conduit to each of said plurality of liquid fuel injectors, and a liquid fuel purge conduit extending from said liquid fuel conduit, disposed between said liquid fuel on/off solenoid valve and said plurality of liquid fuel injectors, and having a purge line solenoid valve and a restrictive orifice, so that when said gas turbine engine is shut down and said liquid fuel inlet or/off solenoid valve is closed, liquid fuel is sucked through the liquid fuel purge line restrictive orifice with the liquid fuel purge line solenoid valve open.
Claim 3
Dependent Claim
27 words
The liquid fuel injector purge system of claim 1 wherein each of said liquid fuel injectors generally directs fuel/air tangentially towards the inner wall of said combustor.
Claim 4
Dependent Claim
64 words
The liquid fuel injector purge system of claim 1 wherein each of said plurality of liquid fuel injectors comprise: a cylindrical liquid fuel tube having a reduced diameter discharge end; and a cylindrical air assist tube concentrically disposed around said cylindrical liquid fuel tube and having a reduced diameter discharge end disposed around the reduced diameter discharge end of said cylindrical liquid fuel tube.
Claim 5
Dependent Claim
20 words
The liquid fuel injector purge system of claim 3 wherein the exterior of said cylindrical air assist tube is insulated.
Claim 6
Dependent Claim
71 words
The liquid fuel injector purge system of claim 3 wherein each of said plurality of liquid fuel injectors additionally includes a cylindrical air blast tube disposed around the reduced diameter discharge ends of said cylindrical liquid fuel tube and said cylindrical air assist tube and having a plurality of radial spider supports extending from said air blast tube to support the reduced diameter discharge end of said cylindrical air assist tube.
Claim 7
Dependent Claim
62 words
The liquid fuel injector purge system of claim 3 wherein said air assist conduit to continuously deliver compressed air from the gas turbine engine compressor to said cylindrical air assist tube during operation of said liquid fuel combustion system includes a pump disposed in said air assist conduit to raise the pressure of the compressed air delivered to said air assist tube.
Claim 8
Dependent Claim
31 words
The liquid fuel injector purge system of claim 6 and in addition a heat exchanger in said air assist conduit upstream of said pump to remove heat from said compressed air.
Claim 9
Dependent Claim
32 words
The liquid fuel injector purge system of claim 6 and in addition a heat exchanger in said air assist conduit downstream of said pump to remove heat from said pumped compressed air.
Claim 10
Dependent Claim
288 words
A liquid fuel injector purge system for a gas turbine engine, comprising: an annular combustor having an outer wall, an inner wall, a closed upstream end, and an open discharge end; a plurality of liquid fuel injectors spaced around the periphery of the closed end of said combustor to direct liquid fuel/air tangentially towards the inner wall of said combustor, each of said plurality of liquid fuel injectors including a cylindrical liquid fuel tube having a reduced diameter discharge end, a cylindrical air assist tube concentrically disposed around said cylindrical liquid fuel tube and having a reduced diameter discharge end disposed around the reduced diameter discharge end of said cylindrical liquid fuel tube, and a cylindrical air blast tube disposed around the reduced diameter discharge ends of said cylindrical liquid fuel tube and said cylindrical air assist tube and having a plurality of radial spider supports extending from said air blast tube to support the reduced diameter discharge end of said cylindrical air assist tube; a liquid fuel inlet conduit to each of said plurality of liquid fuel injectors, said liquid fuel inlet conduit having a liquid fuel control valve and a liquid fuel on/off solenoid valve; an air assist conduit to each of said plurality of liquid fuel injectors; and a liquid fuel purge conduit extending from said liquid fuel conduit, disposed between said liquid fuel on/off solenoid valve and said plurality of liquid fuel injectors, and having a purge line solenoid valve and a restrictive orifice, so that when said gas turbine engine is shut down and said liquid fuel inlet on/off solenoid valve is closed, liquid fuel is purged through said liquid fuel purge line restrictive orifice with the liquid fuel line solenoid valve open.
Claim 11
Dependent Claim
288 words
A liquid fuel injector purge system for a gas turbine engine, comprising: an annular combustor having an outer wall, an inner wall, a closed upstream end, and an open discharge end; a plurality of liquid fuel injectors spaced around the periphery of the closed end of said combustor to direct liquid fuel/air tangentially towards the inner wall of said combustor, each of said plurality of liquid fuel injectors including a cylindrical liquid fuel tube having a reduced diameter discharge end, a cylindrical air assist tube concentrically disposed around said cylindrical liquid fuel tube and having a reduced diameter discharge end disposed around the reduced diameter discharge end of said cylindrical liquid fuel tube, and a cylindrical air blast tube disposed around the reduced diameter discharge ends of said cylindrical liquid fuel tube and said cylindrical air assist tube and having a plurality of radial spider supports extending from said air blast tube to support the reduced diameter discharge end of said cylindrical air assist tube; a liquid fuel inlet conduit to each of said plurality of liquid fuel injectors, said liquid fuel inlet conduit having a liquid fuel control valve and a liquid fuel on/off solenoid valve; an air assist conduit to each of said plurality of liquid fuel injectors; and a liquid fuel purge conduit extending from said liquid fuel conduit, disposed between said liquid fuel on/off solenoid valve and said plurality of liquid fuel injectors, and having a purge line solenoid valve and a restrictive orifice, so that when said gas turbine engine is shut down and said liquid fuel inlet on/off solenoid valve is closed, liquid fuel is purged through said liquid fuel purge line restrictive orifice with the liquid fuel line solenoid valve open.
Claim 12
Dependent Claim
60 words
The liquid fuel injector purge system of claim 9 wherein said air assist conduit to continuously deliver compressed air from the gas turbine engine compressor to said cylindrical air assist tube during operation of said liquid fuel combustion system includes a pump disposed in said conduit to raise the pressure of the compressed air delivered to said air assist tube.
Claim 13
Dependent Claim
31 words
The liquid fuel injector purge system of claim 10 and in addition a heat exchanger in said air assist conduit upstream of said pump to remove heat from said compressed air.
Claim 14
Dependent Claim
31 words
The liquid fuel injector purge system of claim 10 and in addition a heat exchanger in said air assist conduit downstream of said pump to remove heat from said compressed air.
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) | 2003-05-23 | 2003-11-22 | 2004-05-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2007-05-23 | 2007-11-22 | 2008-05-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2011-05-23 | 2011-11-22 | 2012-05-23 | $7700.00 | Window Closed / Lapsed |