GB215603A - Improvements in gas turbines - Google Patents
Improvements in gas turbinesInfo
- Publication number
- GB215603A GB215603A GB1478223A GB1478223A GB215603A GB 215603 A GB215603 A GB 215603A GB 1478223 A GB1478223 A GB 1478223A GB 1478223 A GB1478223 A GB 1478223A GB 215603 A GB215603 A GB 215603A
- Authority
- GB
- United Kingdom
- Prior art keywords
- duct
- gas turbines
- mackirdy
- proportions
- june
- 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
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
215,603. MacKirdy, W. June 5, 1923. Working fluid supply.- Cooling air is supplied through openings 12 at a contracted outlet 8 from a combustion chamber 7 and the mixed air and combustion products pass to a duct 9 which expands for a short distance and thereafter tapers to to a nozzle 10 delivering towards a turbine wheel 15. The duct 9 may be covered with heat insulating material. The Specification describes proportions for the various parts.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1478223A GB215603A (en) | 1923-06-05 | 1923-06-05 | Improvements in gas turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1478223A GB215603A (en) | 1923-06-05 | 1923-06-05 | Improvements in gas turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB215603A true GB215603A (en) | 1924-05-15 |
Family
ID=10047383
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1478223A Expired GB215603A (en) | 1923-06-05 | 1923-06-05 | Improvements in gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB215603A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2624290A (en) * | 1948-08-04 | 1953-01-06 | John B Mclean | Propelling system for locomotives and other vehicles |
US2635421A (en) * | 1949-10-24 | 1953-04-21 | Felix A Blum | Pulse jet convertible to ram jetpropulsion means |
-
1923
- 1923-06-05 GB GB1478223A patent/GB215603A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2624290A (en) * | 1948-08-04 | 1953-01-06 | John B Mclean | Propelling system for locomotives and other vehicles |
US2635421A (en) * | 1949-10-24 | 1953-04-21 | Felix A Blum | Pulse jet convertible to ram jetpropulsion means |
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