GB700705A - Combustion chambers for jet propulsion engines, gas turbines or other prime movers - Google Patents
Combustion chambers for jet propulsion engines, gas turbines or other prime moversInfo
- Publication number
- GB700705A GB700705A GB704751A GB704751A GB700705A GB 700705 A GB700705 A GB 700705A GB 704751 A GB704751 A GB 704751A GB 704751 A GB704751 A GB 704751A GB 700705 A GB700705 A GB 700705A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet propulsion
- pieces
- end cover
- combustion chambers
- gas turbines
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
700,705. Generating combustion products under pressure. LUCAS (INDUSTRIES); Ltd., J. March 3, 1952 [March 27, 1951], No. 7047/51. Class 51 (1) The flame tube of an air jacketed type of combustion chamber for a gas turbine or jet propulsion engine comprises a tubular part a, a domed end cover b and an air deflector c enclosing the end cover, the larger end of the air deflector being formed with relatively radially displaced tongue pieces f, g. The tongue pieces f are secured by welding to the tubular part a and the pieces g are secured to the peripheral part of the end cover b. The tongue pieces f are made somewhat longer than the pieces g.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB704751A GB700705A (en) | 1951-03-27 | 1951-03-27 | Combustion chambers for jet propulsion engines, gas turbines or other prime movers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB704751A GB700705A (en) | 1951-03-27 | 1951-03-27 | Combustion chambers for jet propulsion engines, gas turbines or other prime movers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB700705A true GB700705A (en) | 1953-12-09 |
Family
ID=9825618
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB704751A Expired GB700705A (en) | 1951-03-27 | 1951-03-27 | Combustion chambers for jet propulsion engines, gas turbines or other prime movers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB700705A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4527397A (en) * | 1981-03-27 | 1985-07-09 | Westinghouse Electric Corp. | Turbine combustor having enhanced wall cooling for longer combustor life at high combustor outlet gas temperatures |
FR2887615A1 (en) * | 2005-06-22 | 2006-12-29 | Snecma Moteurs Sa | Circular fairing for combustion chamber of turbomachine, has slits on outer and inner edges, where edges are split between passage holes for passage of bolt, and slits are extended on entire width of edges above position of holes |
FR2896575A1 (en) * | 2006-01-26 | 2007-07-27 | Snecma Sa | Annular combustion chamber for e.g. turbo propeller, has chamber base arranged between inner and outer walls in region that is provided upstream to chamber, where chamber base and walls are made of ceramic material |
-
1951
- 1951-03-27 GB GB704751A patent/GB700705A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4527397A (en) * | 1981-03-27 | 1985-07-09 | Westinghouse Electric Corp. | Turbine combustor having enhanced wall cooling for longer combustor life at high combustor outlet gas temperatures |
FR2887615A1 (en) * | 2005-06-22 | 2006-12-29 | Snecma Moteurs Sa | Circular fairing for combustion chamber of turbomachine, has slits on outer and inner edges, where edges are split between passage holes for passage of bolt, and slits are extended on entire width of edges above position of holes |
FR2896575A1 (en) * | 2006-01-26 | 2007-07-27 | Snecma Sa | Annular combustion chamber for e.g. turbo propeller, has chamber base arranged between inner and outer walls in region that is provided upstream to chamber, where chamber base and walls are made of ceramic material |
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