GB656012A - Improvements relating to liquid fuel combustion chambers - Google Patents
Improvements relating to liquid fuel combustion chambersInfo
- Publication number
- GB656012A GB656012A GB3069948A GB3069948A GB656012A GB 656012 A GB656012 A GB 656012A GB 3069948 A GB3069948 A GB 3069948A GB 3069948 A GB3069948 A GB 3069948A GB 656012 A GB656012 A GB 656012A
- Authority
- GB
- United Kingdom
- Prior art keywords
- liquid fuel
- fuel combustion
- combustion chambers
- improvements relating
- supported
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
- Spray-Type Burners (AREA)
Abstract
656,012. Generating combustion products under pressure. LUCAS, Ltd., J. Nov. 26, 1948. No. 30699. [Class 51(i)] In an air-jacketed liquid fuel combustion chamber for jet propulsion or turbine plants, the flame tube j is supported within the outer casing d by radially arranged spring-loaded plungers f mounted in cylindrical housings a supported on the casing d, the feet i of the plungers bearing on the outer circumferential surface of the flame tube.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3069948A GB656012A (en) | 1948-11-26 | 1948-11-26 | Improvements relating to liquid fuel combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3069948A GB656012A (en) | 1948-11-26 | 1948-11-26 | Improvements relating to liquid fuel combustion chambers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB656012A true GB656012A (en) | 1951-08-08 |
Family
ID=10311742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3069948A Expired GB656012A (en) | 1948-11-26 | 1948-11-26 | Improvements relating to liquid fuel combustion chambers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB656012A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6216442B1 (en) | 1999-10-05 | 2001-04-17 | General Electric Co. | Supports for connecting a flow sleeve and a liner in a gas turbine combustor |
US20150089954A1 (en) * | 2012-08-17 | 2015-04-02 | Dürr Systems GmbH | Burners having fuel plenums |
DE102015226079A1 (en) * | 2015-12-18 | 2017-06-22 | Dürr Systems Ag | Combustion chamber device and gas turbine device |
-
1948
- 1948-11-26 GB GB3069948A patent/GB656012A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6216442B1 (en) | 1999-10-05 | 2001-04-17 | General Electric Co. | Supports for connecting a flow sleeve and a liner in a gas turbine combustor |
US20150089954A1 (en) * | 2012-08-17 | 2015-04-02 | Dürr Systems GmbH | Burners having fuel plenums |
US9982891B2 (en) * | 2012-08-17 | 2018-05-29 | Dürr Systems Ag | Burners having fuel plenums |
DE102015226079A1 (en) * | 2015-12-18 | 2017-06-22 | Dürr Systems Ag | Combustion chamber device and gas turbine device |
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