GB717855A - Improvements in and relating to gas turbine installations - Google Patents
Improvements in and relating to gas turbine installationsInfo
- Publication number
- GB717855A GB717855A GB327552A GB327552A GB717855A GB 717855 A GB717855 A GB 717855A GB 327552 A GB327552 A GB 327552A GB 327552 A GB327552 A GB 327552A GB 717855 A GB717855 A GB 717855A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- cooling
- combustion chamber
- gas turbine
- feb
- 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
- F02C7/105—Heating air supply before combustion, e.g. by exhaust gases by means of regenerative heat-exchangers of the rotary type
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
717,855. Generating combustion products under pressure. PARSONS & CO., Ltd., C. A. Feb. 9, 1953 [Feb. 7, 1952], No. 3275/52. Class 51 (1). [Also in Group XIII] A combustion chamber 18 in a gas turbine plant is provided with a cooling jacket formed between walls 16, 17b, cooling air being supplied to the jacket through a duct 14. Air under pressure is preheated in a rotary regenerative heatexchanger (see Group XIII) and the coolest air i.e. that which passes through the coolest portion of the regenerator matrix is directed to the duct 14 and used for cooling the combustion chamber, the remaining air passing to the primary air cone 16b and the secondary air inlets 16c of the combustion chamber. ; The cooling jacket may be a continuity of a passage provided in the wall of the regenerator housing, Fig. 4 (not shown).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB327552A GB717855A (en) | 1952-02-07 | 1952-02-07 | Improvements in and relating to gas turbine installations |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB327552A GB717855A (en) | 1952-02-07 | 1952-02-07 | Improvements in and relating to gas turbine installations |
Publications (1)
Publication Number | Publication Date |
---|---|
GB717855A true GB717855A (en) | 1954-11-03 |
Family
ID=9755257
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB327552A Expired GB717855A (en) | 1952-02-07 | 1952-02-07 | Improvements in and relating to gas turbine installations |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB717855A (en) |
-
1952
- 1952-02-07 GB GB327552A patent/GB717855A/en not_active Expired
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