GB655871A - Improvements in or relating to internal combustion turbine power plants - Google Patents
Improvements in or relating to internal combustion turbine power plantsInfo
- Publication number
- GB655871A GB655871A GB1159/44A GB115944A GB655871A GB 655871 A GB655871 A GB 655871A GB 1159/44 A GB1159/44 A GB 1159/44A GB 115944 A GB115944 A GB 115944A GB 655871 A GB655871 A GB 655871A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- blades
- compressed
- internal combustion
- turbine power
- 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
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
-
- 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)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
655,871. Gas turbine plant. SHARMA, D. N. April 24, 1948, No. 1159. '[Class 110(iii)] An internal combustion turbine power plant comprises a hollow cylindrical shaft 1, two multi-stage compressors 8, 10 associated with and surrounding said shaft which is coupled with a multi-stage turbine rotor 2, mounted on another shaft coaxially placed within the hollow shaft by means of compressor blades 3, the hollow shaft driving a propellor or shaft for traction purposes through gearing 11. The arrangement is such that part of the incoming cold air is first compressed by the blades 3 then used to cool the bearings 14 and finally compressed, before entering the combustion chambers 13, by the compressor 8. The remaining part of the incoming air is compressed by the blades 10 and supplied direct to the combustion chambers for cooling and combustion purposes. The turbine exhaust gases pass through the opening 4. The air entering through the shaft takes up heat from the rotating parts.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1159/44A GB655871A (en) | 1948-04-24 | 1948-04-24 | Improvements in or relating to internal combustion turbine power plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1159/44A GB655871A (en) | 1948-04-24 | 1948-04-24 | Improvements in or relating to internal combustion turbine power plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB655871A true GB655871A (en) | 1951-08-08 |
Family
ID=9717203
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1159/44A Expired GB655871A (en) | 1948-04-24 | 1948-04-24 | Improvements in or relating to internal combustion turbine power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB655871A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2605679A1 (en) * | 1986-10-24 | 1988-04-29 | Culica Georges Francois | Multi-spool multi-bypass turbo jet engine with a drum rotor |
GB2289504A (en) * | 1994-05-11 | 1995-11-22 | British Aerospace | Gas turbine propulsion unit |
-
1948
- 1948-04-24 GB GB1159/44A patent/GB655871A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2605679A1 (en) * | 1986-10-24 | 1988-04-29 | Culica Georges Francois | Multi-spool multi-bypass turbo jet engine with a drum rotor |
GB2289504A (en) * | 1994-05-11 | 1995-11-22 | British Aerospace | Gas turbine propulsion unit |
GB2289504B (en) * | 1994-05-11 | 1998-01-14 | British Aerospace | Gas turbine propulsion unit |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB588096A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB713839A (en) | Improvements in or relating to internal combustion turbines | |
GB586570A (en) | Improvements in internal combustion turbine plant for propulsion | |
GB581217A (en) | Improvements in or relating to power plants for helicopters | |
GB655871A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB649639A (en) | Improvements in thermal power plants | |
GB436709A (en) | Improvements in internal combustion turbines | |
GB615680A (en) | Improvements in or relating to gas turbines | |
GB706841A (en) | Improvements relating to turbine jet propulsion power units | |
GB610939A (en) | Improvements in or relating to internal combustion turbines | |
GB693682A (en) | Improvements in or relating to internal combustion turbine motors | |
GB588097A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB592615A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB593403A (en) | Power plant for the propulsion of aircraft | |
GB600608A (en) | Improvements in or relating to internal combustion turbine power plants | |
GB687104A (en) | Improvements in and relating to gas turbine installations | |
GB659714A (en) | Improvements in units comprising a gas turbine driving an electric generator | |
GB586555A (en) | Improvements in internal combustion gas turbine plant, supercharger plant, air conditioning plant and the like | |
GB685988A (en) | Improvements relating to the propulsion of vehicles | |
GB716145A (en) | Improvements in aircraft jet propulsion engines including a ducted fan | |
GB636132A (en) | Improved internal combustion turbine | |
GB778690A (en) | Improvements relating to power producing equipment incorporating gas turbine plant | |
GB645588A (en) | Improvements in or relating to gas turbine power plants | |
GB447855A (en) | Improvements in or relating to internal combustion engine plants with an exhaust gas turbine and compressors driven thereby | |
GB617152A (en) | Improvements in or relating to the propulsion of aircraft |