GB190612735A - Improvements in or relating to Air Compressors of the Turbine Type, specially applicable for use in Internal Combustion Turbine Systems. - Google Patents
Improvements in or relating to Air Compressors of the Turbine Type, specially applicable for use in Internal Combustion Turbine Systems.Info
- Publication number
- GB190612735A GB190612735A GB190612735DA GB190612735A GB 190612735 A GB190612735 A GB 190612735A GB 190612735D A GB190612735D A GB 190612735DA GB 190612735 A GB190612735 A GB 190612735A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- valve
- relating
- internal combustion
- hot
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
12,735. Fullagar, H. F. May 31. Hinged valves; casings.-An arrangement for varying a mixture of hot and cold air supplied to a turbo-compressor is shown in Fig. 1. A rod i operated by hand, or automatically, actuates simultaneously two disk valves f, e, the valve f controlling the hot air and the valve e the co!d air, the air being mixed in the inlet pipe b of the compressor. The casing d<2> of the cold-air valve has a spherical shape to allow the valve to have a long period of closure, the hot-air valve at the same time being moved to vary the admission of hot air.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190612735T | 1906-05-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190612735A true GB190612735A (en) | 1907-03-14 |
Family
ID=32545787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190612735D Expired GB190612735A (en) | 1906-05-31 | 1906-05-31 | Improvements in or relating to Air Compressors of the Turbine Type, specially applicable for use in Internal Combustion Turbine Systems. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190612735A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434777A (en) * | 1942-09-30 | 1948-01-20 | English Electric Co Ltd | Power plant comprising a gas turbine and an internal-combustion engine compressor serving as a gas generator thereto |
US2508288A (en) * | 1944-12-08 | 1950-05-16 | Bristol Aeroplane Co Ltd | Gas turbine power plant for aircraft |
US2633698A (en) * | 1948-02-05 | 1953-04-07 | Nettel Frederick | Turbosupercharger means to heat intake of compression-ignition engine for starting |
US2652685A (en) * | 1948-05-13 | 1953-09-22 | United Aricraft Corp | Starting device for compressorturbine units |
-
1906
- 1906-05-31 GB GB190612735D patent/GB190612735A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2434777A (en) * | 1942-09-30 | 1948-01-20 | English Electric Co Ltd | Power plant comprising a gas turbine and an internal-combustion engine compressor serving as a gas generator thereto |
US2508288A (en) * | 1944-12-08 | 1950-05-16 | Bristol Aeroplane Co Ltd | Gas turbine power plant for aircraft |
US2633698A (en) * | 1948-02-05 | 1953-04-07 | Nettel Frederick | Turbosupercharger means to heat intake of compression-ignition engine for starting |
US2652685A (en) * | 1948-05-13 | 1953-09-22 | United Aricraft Corp | Starting device for compressorturbine units |
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