GB1204652A - Gas turbine engine combustion equipment - Google Patents
Gas turbine engine combustion equipmentInfo
- Publication number
- GB1204652A GB1204652A GB314569A GB314569A GB1204652A GB 1204652 A GB1204652 A GB 1204652A GB 314569 A GB314569 A GB 314569A GB 314569 A GB314569 A GB 314569A GB 1204652 A GB1204652 A GB 1204652A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- engine
- combustion equipment
- turbine engine
- heat exchanger
- 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
- 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
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
- F02C7/10—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
1,204,652. Gas turbine engine combustion equipment. ROLLS-ROYCE Ltd. Jan. 20, 1969, No.3145/69. Headings F1G and F1L. A gas turbine engine has combustion equipment comprising an outer chamber 16 having an inlet 17 for air from the engine compressor and surrounding an inner chamber 20 containing a flame tube 23 and a heat exchanger 22 having a path 21 through which the compressed air flows to the flame tube inlet 24. Gases leave the flame tube through an outlet 25 to drive the turbine 14. The heat exchanger 22 has a second path 26 receiving hot liquid sodium from a heat exchanger (31), Fig.1 (not shown), in the engine exhaust duct (15). The heat exchangers 22, (31) are connected in a closed circuit through which the sodium is circulated by a magnetic or other pump (33). An inner skin 35 defines a cooling air space 34 with the wall of the outer chamber 16. The engine may be provided with several such combustion units which are angularly spaced apart from each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB314569A GB1204652A (en) | 1969-01-20 | 1969-01-20 | Gas turbine engine combustion equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB314569A GB1204652A (en) | 1969-01-20 | 1969-01-20 | Gas turbine engine combustion equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1204652A true GB1204652A (en) | 1970-09-09 |
Family
ID=9752800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB314569A Expired GB1204652A (en) | 1969-01-20 | 1969-01-20 | Gas turbine engine combustion equipment |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1204652A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131095A (en) * | 1982-11-24 | 1984-06-13 | English Electric Co Ltd | Gas turbine plant |
-
1969
- 1969-01-20 GB GB314569A patent/GB1204652A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131095A (en) * | 1982-11-24 | 1984-06-13 | English Electric Co Ltd | Gas turbine plant |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1516041A (en) | Multistage axial flow compressor stators | |
| GB1344800A (en) | Gas turbine combustion chamber | |
| GB1150147A (en) | Improvements in Combinations of Gas Turbine Engines and Electric Generators | |
| GB1080860A (en) | Gas turbine engines with cooled nozzle vanes | |
| ES408033A1 (en) | Integral turbo-compressor wave engine | |
| GB1302036A (en) | ||
| GB585334A (en) | Improvements in or relating to internal-combustion turbines | |
| GB1147991A (en) | Improvements in or relating to intermeshing-screw type rotary engines | |
| US2621481A (en) | Closed cycle air turbine power plant having direct and indirect heat exchangers | |
| GB1178642A (en) | Improvements in Air-Cooled Steam Condensers | |
| US3095704A (en) | Pressure exchanger apparatus | |
| GB1479599A (en) | Aircraft gas turbine engine turbine blade cooling | |
| GB1204652A (en) | Gas turbine engine combustion equipment | |
| GB1487064A (en) | Wall structure for hot fluid streams | |
| US2641904A (en) | Apparatus for cooling combustion chambers of movable power plants with an oxidizing agent | |
| GB1497595A (en) | Recuperative heat exchangers | |
| GB578686A (en) | Improvements in regenerative gas turbine plant | |
| GB624273A (en) | Improvements in or relating to compressor systems | |
| US2417408A (en) | Flameproof screen for use in airconditioning conduits | |
| GB603112A (en) | Improvements in or relating to systems of heat exchange | |
| GB1073195A (en) | Pressure exchanger | |
| GB546275A (en) | Heat power plant for gaseous working media | |
| GB1280862A (en) | Improvements in or relating to gas turbine engines | |
| GB737648A (en) | Improvements in gas turbine power plants | |
| SU408587A1 (en) | Gas-turbine plant |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |