GB700017A - Combustion chambers for prime movers - Google Patents
Combustion chambers for prime moversInfo
- Publication number
- GB700017A GB700017A GB523251A GB523251A GB700017A GB 700017 A GB700017 A GB 700017A GB 523251 A GB523251 A GB 523251A GB 523251 A GB523251 A GB 523251A GB 700017 A GB700017 A GB 700017A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sleeve
- air
- cylindrical parts
- apertures
- gap
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
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
700,017. Generating combustion products under pressure. LUCAS (INDUSTRIES), Ltd., J. Feb. 8, 1952 [March 5, 1951], No. 5232/51. Class 51 (1) In an air jacketed type of combustion chamber for a prime mover such as a gas turbine or jet propulsion engine, the flame tube comprises a pair of co-axial cylindrical parts a, b of substantially equal diameter which are spaced apart to form a gap c corresponding to a region on which soot is liable to be deposited. The gap is enclosed by a sleeve d of greater diameter than the cylindrical parts and the sleeve is secured at its ends to the cylindrical parts which it overlaps to form annular air passages e therebetween. Apertures f are formed near the ends of the sleeve for admission of air to the annular passages from the surrounding air jacket. Other apertures h may also be formed in the sleeve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB523251A GB700017A (en) | 1951-03-05 | 1951-03-05 | Combustion chambers for prime movers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB523251A GB700017A (en) | 1951-03-05 | 1951-03-05 | Combustion chambers for prime movers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB700017A true GB700017A (en) | 1953-11-25 |
Family
ID=9792194
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB523251A Expired GB700017A (en) | 1951-03-05 | 1951-03-05 | Combustion chambers for prime movers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB700017A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3735589A (en) * | 1970-06-02 | 1973-05-29 | Snecma | Walls of combustion chambers |
US4396368A (en) * | 1980-09-05 | 1983-08-02 | The United States Of America As Represented By The Secretary Of The Navy | Bi-planner swirl combustor |
US5094082A (en) * | 1989-12-22 | 1992-03-10 | Sundstrand Corporation | Stored energy combustor |
-
1951
- 1951-03-05 GB GB523251A patent/GB700017A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3735589A (en) * | 1970-06-02 | 1973-05-29 | Snecma | Walls of combustion chambers |
US4396368A (en) * | 1980-09-05 | 1983-08-02 | The United States Of America As Represented By The Secretary Of The Navy | Bi-planner swirl combustor |
US5094082A (en) * | 1989-12-22 | 1992-03-10 | Sundstrand Corporation | Stored energy combustor |
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