GB720464A - Improvements relating to combustion chambers - Google Patents
Improvements relating to combustion chambersInfo
- Publication number
- GB720464A GB720464A GB2667150A GB2667150A GB720464A GB 720464 A GB720464 A GB 720464A GB 2667150 A GB2667150 A GB 2667150A GB 2667150 A GB2667150 A GB 2667150A GB 720464 A GB720464 A GB 720464A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wall
- rods
- supported
- splitter
- combustion chamber
- 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)
Abstract
720,464. Generating combustion products under pressure. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. Oct. 23, 1951, [Nov. 1, 1950.] No. 26671/50. Addition to 582,978, [Group XXVI]. Class 51 (1). A combustion chamber comprises an outer wall co-axially surrounding an inner wall which is supported on rods which extend across the annular duct to the outer wall at each end, the rods being disposed normally to the longitudinal axis of the chamber in intersecting directions, and being a free fit so that they together form a structure ensuring co-axial and positive relative location of the walls whilst permitting radial relative expansions. The outer wall 1 is cylindrical and the inner wall comprises a flow splitter which is supported by a pair of rods 6 arranged diametrically and at right angles to each other. The flow splitter comprises a body 5 and an inner body 8, some air from the inlet 2 passing between the two bodies to have a cooling effect on the wall 5. The support rods are enclosed by fairings 9 which may swivel so as to take up a neutral incidence relative to the gas flow. Gaseous fuel is supplied into the air stream from the volute 3 through swirl vanes 4. The splitter is supported at the upstream end by three radial struts 7, and the combustion space is covered by lagging 10. The invention may be applied for supporting the flame tube of a gas turbine combustion chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2667150A GB720464A (en) | 1950-11-01 | 1950-11-01 | Improvements relating to combustion chambers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2667150A GB720464A (en) | 1950-11-01 | 1950-11-01 | Improvements relating to combustion chambers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB720464A true GB720464A (en) | 1954-12-22 |
Family
ID=10247342
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2667150A Expired GB720464A (en) | 1950-11-01 | 1950-11-01 | Improvements relating to combustion chambers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB720464A (en) |
-
1950
- 1950-11-01 GB GB2667150A patent/GB720464A/en not_active Expired
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