GB636623A - Improvements in or relating to combustion apparatus - Google Patents
Improvements in or relating to combustion apparatusInfo
- Publication number
- GB636623A GB636623A GB22240/47A GB2224047A GB636623A GB 636623 A GB636623 A GB 636623A GB 22240/47 A GB22240/47 A GB 22240/47A GB 2224047 A GB2224047 A GB 2224047A GB 636623 A GB636623 A GB 636623A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ports
- combustion chamber
- relating
- combustion apparatus
- shield
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
636,623. Generating combustion products under pressure. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and BROWN, J. Aug. 11, 1947, No. 22240. [Class 51 (i)] Secondary air is admitted to a combustion chamber for a gas turbine through ports 25 which are covered by a cylindrical shield 15 so that the air passes over the shield to its downstream end and flows upstream in the space 16 to reach the ports 25. Other details of the combustion chamber are as described in Specification 636,624. Reference has been directed by the Comptroller to Specification 594,285.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22240/47A GB636623A (en) | 1947-08-11 | 1947-08-11 | Improvements in or relating to combustion apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB22240/47A GB636623A (en) | 1947-08-11 | 1947-08-11 | Improvements in or relating to combustion apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB636623A true GB636623A (en) | 1950-05-03 |
Family
ID=10176176
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22240/47A Expired GB636623A (en) | 1947-08-11 | 1947-08-11 | Improvements in or relating to combustion apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB636623A (en) |
-
1947
- 1947-08-11 GB GB22240/47A patent/GB636623A/en not_active Expired
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