GB585343A - Combustion chambers of internal-combustion turbine plant - Google Patents
Combustion chambers of internal-combustion turbine plantInfo
- Publication number
- GB585343A GB585343A GB13631/42A GB1363142A GB585343A GB 585343 A GB585343 A GB 585343A GB 13631/42 A GB13631/42 A GB 13631/42A GB 1363142 A GB1363142 A GB 1363142A GB 585343 A GB585343 A GB 585343A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- secondary air
- tubes
- combustion
- passes
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Fuel Cell (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
585,343. Gas turbines. ARMSTRONG SIDDELEY MOTORS, Ltd., and HEPPNER, F. A. M. Sept. 29, 1942, Nos. 13631/42, 15665/42 and 822/43. [Class 110 (iii)] In a contra-rotational gas turbine plant, primary air from the compressor 11 is diverted by centrifugally acting blade portions 19, and passes through an annular space 22, past swirlproducing blades 24 into a combustion chamber 16. The fuel is thrown in a radial sheet, transverse to the current of primary air, from a valve 23 which is opened by the pressure of the fuel supply. Ignition is started by a heater 30 which withdraws into a covering tube when the airpressure on piston 31 overcomes a spring 33. Secondary air passes from the compressor into a chamber 12 and surrounds the tubes 14 which lead from the combustion chamber to the turbine 17. The secondary air enters through perforations 15 and mixes with the combustion products. In the construction shown in Fig., 6, the primary air passes through the space 59 and blades 62 and the secondary air passes through the chamber 65 and holes 64 in tubes 14. In a third form the chamber 65 is continued by a sheet metal extension and the tubes 58 are replaced by an annular passage between annular walls which are corrugated where they reach the sheet metal extension and thereby provide passages for the secondary air to enter the main gas flow. Specifications 561,246, [Group XXXIV], 585,340, 585,342 and 585,346 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13631/42A GB585343A (en) | 1942-09-29 | 1942-09-29 | Combustion chambers of internal-combustion turbine plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB13631/42A GB585343A (en) | 1942-09-29 | 1942-09-29 | Combustion chambers of internal-combustion turbine plant |
Publications (1)
Publication Number | Publication Date |
---|---|
GB585343A true GB585343A (en) | 1947-02-05 |
Family
ID=10026533
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13631/42A Expired GB585343A (en) | 1942-09-29 | 1942-09-29 | Combustion chambers of internal-combustion turbine plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB585343A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2604510A (en) * | 1949-11-30 | 1952-07-22 | Gen Electric | Automatically retractable spark plug for gas turbines |
DE944690C (en) * | 1948-11-30 | 1956-06-21 | Joseph Szydlowski | Combustion chamber arrangement |
US2856755A (en) * | 1953-10-19 | 1958-10-21 | Szydlowski Joseph | Combustion chamber with diverse combustion and diluent air paths |
US3011311A (en) * | 1955-10-24 | 1961-12-05 | Williams Res Corp | Gas turbine |
US3077076A (en) * | 1960-01-20 | 1963-02-12 | Williams Res Corp | Gas turbine combustion chamber |
US3086396A (en) * | 1960-09-22 | 1963-04-23 | Homer T Armstrong | High-temperature probe assembly |
US3118278A (en) * | 1959-06-26 | 1964-01-21 | Gas turbine power plant | |
US3169369A (en) * | 1963-06-19 | 1965-02-16 | Gen Electric | Combustion system |
-
1942
- 1942-09-29 GB GB13631/42A patent/GB585343A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE944690C (en) * | 1948-11-30 | 1956-06-21 | Joseph Szydlowski | Combustion chamber arrangement |
US2604510A (en) * | 1949-11-30 | 1952-07-22 | Gen Electric | Automatically retractable spark plug for gas turbines |
US2856755A (en) * | 1953-10-19 | 1958-10-21 | Szydlowski Joseph | Combustion chamber with diverse combustion and diluent air paths |
US3011311A (en) * | 1955-10-24 | 1961-12-05 | Williams Res Corp | Gas turbine |
US3118278A (en) * | 1959-06-26 | 1964-01-21 | Gas turbine power plant | |
US3077076A (en) * | 1960-01-20 | 1963-02-12 | Williams Res Corp | Gas turbine combustion chamber |
US3086396A (en) * | 1960-09-22 | 1963-04-23 | Homer T Armstrong | High-temperature probe assembly |
US3169369A (en) * | 1963-06-19 | 1965-02-16 | Gen Electric | Combustion system |
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