GB578769A - Internal-combustion turbine plant - Google Patents
Internal-combustion turbine plantInfo
- Publication number
- GB578769A GB578769A GB1382242A GB1382242A GB578769A GB 578769 A GB578769 A GB 578769A GB 1382242 A GB1382242 A GB 1382242A GB 1382242 A GB1382242 A GB 1382242A GB 578769 A GB578769 A GB 578769A
- Authority
- GB
- United Kingdom
- Prior art keywords
- abstraction
- turbine plant
- internal
- combustion chambers
- combustion turbine
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pipeline Systems (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
578,769. Gas turbines. ARMSTRONG SIDDELEY MOTORS, Ltd., CLARK, T., and LINDSEY, W. H. Oct. 2, 1942, No. 13822. Drawings to Specification. [Class 110 (iii)] [Also in Group XXXIII] In a gas turbine plant for aircraft, formation of ice in the compressor is prevented by the abstraction of a small quantity, up to 2 per cent. of the burning mixture beyond the combustion chambers and injecting it into the compressor inlet. When there is an annular series, of combustion chambers, an abstraction is made from each and the pipes conveying the gases to the compressor inlet are connected by a ring pipe which equalizes the pressures. The abstraction is controlled by normally closed valves.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1382242A GB578769A (en) | 1942-10-02 | 1942-10-02 | Internal-combustion turbine plant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1382242A GB578769A (en) | 1942-10-02 | 1942-10-02 | Internal-combustion turbine plant |
Publications (1)
Publication Number | Publication Date |
---|---|
GB578769A true GB578769A (en) | 1946-07-11 |
Family
ID=10030015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1382242A Expired GB578769A (en) | 1942-10-02 | 1942-10-02 | Internal-combustion turbine plant |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB578769A (en) |
-
1942
- 1942-10-02 GB GB1382242A patent/GB578769A/en not_active Expired
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