GB660775A - An improved combustion and ignition apparatus for a gas turbine engine - Google Patents
An improved combustion and ignition apparatus for a gas turbine engineInfo
- Publication number
- GB660775A GB660775A GB32183/49A GB3218349A GB660775A GB 660775 A GB660775 A GB 660775A GB 32183/49 A GB32183/49 A GB 32183/49A GB 3218349 A GB3218349 A GB 3218349A GB 660775 A GB660775 A GB 660775A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- igniter
- combustion
- gas turbine
- turbine engine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
- F02C7/266—Electric
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray-Type Burners (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
660,775. Lighting vapour burners. WILLIAMS, F. D. M. Dec. 15, 1949 [Dec. 24, 1948], No. 32183/49. Classes 75(i) and 75(iii) Combustion and ignition apparatus for a gas turbine engine comprises a fuel injector head 9, Fig. 1, located at the upstream end of a flame tube 6, and including an igniter jet 11, Fig. 3, whereby an igniting flame may be directed substantially along the longitudinal axis of the flame tube 6 and applied to longitudinally extending vaporizing tubes 7, each having an inlet exposed to the air stream through the combustion chamber and an outlet end discharging into the flame tube 6, an igniter 13 situated in front of the jet 11, and a plurality of fuel supply jets 10 arranged around the jet 11 and directed into the inlet ends of the vaporizing tubes 7. The jet 11 is of an atomizing type and is supplied with fuel through a pipe 16 extending coaxially through a pipe 18 which supplies the jets 10. The igniter comprises a sparking electrode 12 mounted directly on the head 9 and a sparking electrode 13 connected by a high-tension lead through a tube 14 to a terminal mounted outside the combustion chamber.. When combustion has been established the current to the igniter is switched off and the fuel supply to the igniter jet 11 is discontinued.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US67118A US2541900A (en) | 1948-12-24 | 1948-12-24 | Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB660775A true GB660775A (en) | 1951-11-14 |
Family
ID=22073825
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32183/49A Expired GB660775A (en) | 1948-12-24 | 1949-12-15 | An improved combustion and ignition apparatus for a gas turbine engine |
Country Status (4)
Country | Link |
---|---|
US (1) | US2541900A (en) |
DE (1) | DE804504C (en) |
FR (1) | FR1006966A (en) |
GB (1) | GB660775A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1015271B (en) * | 1955-04-05 | 1957-09-05 | Armstrong Siddeley Motors Ltd | Main combustion chamber for gas turbines with ignition chamber |
US5761906A (en) * | 1995-01-13 | 1998-06-09 | European Gas Turbines Limited | Fuel injector swirler arrangement having a shield means for creating fuel rich pockets in gas-or liquid-fuelled turbine |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3273621A (en) * | 1966-09-20 | Burner assembly | ||
US2735633A (en) * | 1956-02-21 | Jet propelled aircraft | ||
US2646664A (en) * | 1949-02-24 | 1953-07-28 | A V Roe Canada Ltd | Annular fuel vaporizer for gas turbine engines |
US2706889A (en) * | 1949-08-18 | 1955-04-26 | Armstrong Siddeley Motors Ltd | Combustion chambers of gas turbine engines |
US2678535A (en) * | 1950-04-12 | 1954-05-18 | A V Roe Canada Ltd | Liquid fuel injecting burner |
US2655786A (en) * | 1950-09-18 | 1953-10-20 | Phillips Petroleum Co | Method of operating jet engines with fuel reforming |
US2699648A (en) * | 1950-10-03 | 1955-01-18 | Gen Electric | Combustor sectional liner structure with annular inlet nozzles |
US2781637A (en) * | 1950-12-15 | 1957-02-19 | Gen Motors Corp | Combustion chamber with fuel vaporizer |
US2674846A (en) * | 1950-12-18 | 1954-04-13 | Lummus Co | Combustion chamber with baffle means to control secondary air |
US2648197A (en) * | 1951-01-06 | 1953-08-11 | A V Roe Canada Ltd | Vaporizer tube system |
US2828605A (en) * | 1951-03-19 | 1958-04-01 | Power Jets Res & Dev Ltd | Method of generating combustion gases by burning a gaseous combustible mixture |
US2693676A (en) * | 1951-06-11 | 1954-11-09 | Westinghouse Electric Corp | Combustion apparatus with multipleoutlet fuel vaporizing tubes |
US2805547A (en) * | 1952-02-01 | 1957-09-10 | Sherry Peter | Temperature responsive control for fuel and water vaporizers in combustion chamber |
US2727358A (en) * | 1952-03-27 | 1955-12-20 | A V Roe Canada Ltd | Reverse-flow vaporizer with single inlet and plural outlets |
US2982098A (en) * | 1953-04-22 | 1961-05-02 | Power Jets Res & Dev Ltd | Liquid fuel vaporizing combustion systems |
GB798474A (en) * | 1955-03-16 | 1958-07-23 | Bristol Aero Engines Ltd | Improvements in or relating to combustion chambers |
US2941364A (en) * | 1955-04-05 | 1960-06-21 | Armstrong Siddeley Motors Ltd | Igniter chamber for a gas turbine engine |
US3018626A (en) * | 1960-02-02 | 1962-01-30 | Gen Electric | Vapor combustion system |
US3287913A (en) * | 1962-07-09 | 1966-11-29 | Aerojet General Co | Igniter |
US3398528A (en) * | 1965-10-05 | 1968-08-27 | Ishikawajima Harima Heavy Ind | Evaporation type burner |
US3548592A (en) * | 1969-06-13 | 1970-12-22 | Gen Electric | Combination fuel nozzle and spark plug for a gas turbine |
GB1429677A (en) * | 1973-03-20 | 1976-03-24 | Rolls Royce | Gas turbine engine combustion equipment |
US5127822A (en) * | 1987-08-14 | 1992-07-07 | Toa Nenryo Kogyo Kabushiki Kaisha | Combustion apparatus with atomizer and method of controlling same |
US5163287A (en) * | 1989-12-22 | 1992-11-17 | Sundstrand Corporation | Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion |
CN103343984B (en) * | 2013-06-24 | 2016-01-06 | 北京航空航天大学 | A kind of burner for living beings replacing fuel oil combustion test |
US11692488B2 (en) | 2020-11-04 | 2023-07-04 | Delavan Inc. | Torch igniter cooling system |
US11608783B2 (en) | 2020-11-04 | 2023-03-21 | Delavan, Inc. | Surface igniter cooling system |
US11473505B2 (en) | 2020-11-04 | 2022-10-18 | Delavan Inc. | Torch igniter cooling system |
US11635027B2 (en) | 2020-11-18 | 2023-04-25 | Collins Engine Nozzles, Inc. | Fuel systems for torch ignition devices |
US11421602B2 (en) | 2020-12-16 | 2022-08-23 | Delavan Inc. | Continuous ignition device exhaust manifold |
US11226103B1 (en) | 2020-12-16 | 2022-01-18 | Delavan Inc. | High-pressure continuous ignition device |
US11486309B2 (en) | 2020-12-17 | 2022-11-01 | Delavan Inc. | Axially oriented internally mounted continuous ignition device: removable hot surface igniter |
US11635210B2 (en) | 2020-12-17 | 2023-04-25 | Collins Engine Nozzles, Inc. | Conformal and flexible woven heat shields for gas turbine engine components |
US11754289B2 (en) | 2020-12-17 | 2023-09-12 | Delavan, Inc. | Axially oriented internally mounted continuous ignition device: removable nozzle |
US11680528B2 (en) | 2020-12-18 | 2023-06-20 | Delavan Inc. | Internally-mounted torch igniters with removable igniter heads |
US11286862B1 (en) | 2020-12-18 | 2022-03-29 | Delavan Inc. | Torch injector systems for gas turbine combustors |
US11209164B1 (en) | 2020-12-18 | 2021-12-28 | Delavan Inc. | Fuel injector systems for torch igniters |
CN112963273B (en) * | 2021-03-03 | 2022-07-01 | 中国人民解放军空军工程大学 | Self-air-entraining kerosene pre-combustion cracking activation device and method for concave cavity flame stabilizer |
CN114234237B (en) * | 2021-12-20 | 2023-03-31 | 中国人民解放军总参谋部第六十研究所 | Head preparation method for wide-envelope starting of evaporating tube combustion chamber |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL70682C (en) * | 1939-12-09 | |||
GB603485A (en) * | 1946-02-23 | 1948-06-16 | Armstrong Siddeley Motors Ltd | Liquid fuel combustion chamber |
-
1948
- 1948-12-24 US US67118A patent/US2541900A/en not_active Expired - Lifetime
-
1949
- 1949-12-15 GB GB32183/49A patent/GB660775A/en not_active Expired
- 1949-12-16 FR FR1006966D patent/FR1006966A/en not_active Expired
- 1949-12-22 DE DEC336A patent/DE804504C/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1015271B (en) * | 1955-04-05 | 1957-09-05 | Armstrong Siddeley Motors Ltd | Main combustion chamber for gas turbines with ignition chamber |
US5761906A (en) * | 1995-01-13 | 1998-06-09 | European Gas Turbines Limited | Fuel injector swirler arrangement having a shield means for creating fuel rich pockets in gas-or liquid-fuelled turbine |
Also Published As
Publication number | Publication date |
---|---|
US2541900A (en) | 1951-02-13 |
FR1006966A (en) | 1952-04-29 |
DE804504C (en) | 1951-04-23 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB660775A (en) | An improved combustion and ignition apparatus for a gas turbine engine | |
US5085040A (en) | Torch igniters | |
US4342551A (en) | Ignition method and system for internal burner type ultra-high velocity flame jet apparatus | |
US2958196A (en) | Flame igniter for gas turbine combustor | |
US11543130B1 (en) | Passive secondary air assist nozzles | |
GB693846A (en) | Vaporizer-type combustion apparatus for gas turbine engines | |
US2480147A (en) | Firing device for combustion apparatus | |
US2398611A (en) | Igniting means for burners | |
GB621789A (en) | Improved ignition system for gas turbine engines | |
US2274573A (en) | Oil burner | |
GB686131A (en) | Improvements in or relating to ignition arrangements for gas-turbine engines | |
GB675092A (en) | Improvements relating to combustion systems of gas-turbine engines | |
US4628832A (en) | Dual fuel pilot burner for a furnace | |
GB1499959A (en) | Oil burner assembly | |
GB747593A (en) | Improvements in or relating to igniters for gas turbine engines and combustion heaters | |
GB1131042A (en) | Improvements in or relating to ignition torches | |
US2835110A (en) | Injector igniter plug | |
US2968152A (en) | Air separator for monofuel burner | |
US2136727A (en) | Gas-generating oil burner | |
GB862148A (en) | Igniter and ignition system | |
RU71732U1 (en) | ELECTROSTATIC FUEL INJECTOR | |
JPS584022Y2 (en) | gas burner | |
GB715197A (en) | Jet propulsion engines | |
RU527933C (en) | Burner for combustion chamber of gas-turbine engine | |
GB738966A (en) | Improvements in combined fuel injectors and igniter plugs particularly for gas turbine engines |