GB437095A - Improvements in or relating to reciprocating piston compressors - Google Patents
Improvements in or relating to reciprocating piston compressorsInfo
- Publication number
- GB437095A GB437095A GB11853/35A GB1185335A GB437095A GB 437095 A GB437095 A GB 437095A GB 11853/35 A GB11853/35 A GB 11853/35A GB 1185335 A GB1185335 A GB 1185335A GB 437095 A GB437095 A GB 437095A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- receiver
- main
- valve
- pipe
- 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
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
437,095. Combustion-product plant. SULZER FRERES SOC. ANON., Winterthur, Switzerland. April 17, 1935, No. 11853. Convention date, April 24, 1934. [Class 7 (i)] [See also Group XXVIII] To facilitate the starting of a direct-acting motor-compressor delivering air or a mixture air and combustion products, the motor-compressor delivers to a receiver 12 which can be connected at will either to a main pipe 14 delivering to a turbine &c., or (at starting) to an auxiliary low-pressure pipe 16 which may be open to atmosphere. Fig. 1 shows the compressor comprising cylinders 2 delivering compressed air through a pipe 7 and ports 8 to the combustion space 3, which exhausts through ports 10 to the receiver 12, which can be connected to either of the pipes 14, 16 by valves 13, 15. Alternatively, part of the compressed air may be delivered direct to the receiver. Fig. 2 shows apparatus in which a manual valve 20 controls communication of the receiver with the low-pressure main 16, while communication with the main 14 is controlled by a valve 19 carrying a plunger 21 working in a cylinder having oil supply and discharge ports controlled by a piston 32 subject on its faces to the pressures in compressor delivery pipe and the supply main 14. The valve 20 may alternatively be controlled in accordance with the fuel supply to the compressor or with its end-ofstroke positions. In a modification, a single valve may control the two conduits 14, 16.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH437095X | 1934-04-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB437095A true GB437095A (en) | 1935-10-23 |
Family
ID=4515094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11853/35A Expired GB437095A (en) | 1934-04-24 | 1935-04-17 | Improvements in or relating to reciprocating piston compressors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB437095A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2612751A (en) * | 1945-12-27 | 1952-10-07 | Rolls Royce | Control means for gas-turbine or jet engines which facilitates starting of the engine |
-
1935
- 1935-04-17 GB GB11853/35A patent/GB437095A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2612751A (en) * | 1945-12-27 | 1952-10-07 | Rolls Royce | Control means for gas-turbine or jet engines which facilitates starting of the engine |
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