GB591761A - Improvements in and relating to aircraft supercharging arrangements - Google Patents
Improvements in and relating to aircraft supercharging arrangementsInfo
- Publication number
- GB591761A GB591761A GB1341841A GB1341841A GB591761A GB 591761 A GB591761 A GB 591761A GB 1341841 A GB1341841 A GB 1341841A GB 1341841 A GB1341841 A GB 1341841A GB 591761 A GB591761 A GB 591761A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- compressors
- pipe
- valves
- aircraft
- 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
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/33—Compressors for piston combustion engines
- F02M2700/331—Charging and scavenging compressors
- F02M2700/336—Arrangements thereof on the engine
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
591,761. Centrifugal compressors. BRITISH THOMSON-HOUSTON CO., Ltd. (General Electric Co.). Oct. 17, 1941, No. 13418. [Class 110 (i)] In a multi-stage compressor or a number of compressors 14, 15 for supplying supercharged air to the cabin 11 of an aircraft, means are provided for switching the stages or compressors from parallel to series in accordance with changes in the operating conditions. When working in parallel, valve 20 in the pipe 18 connecting the delivery of 14 to the intake of 15 is closed, valve 21 in the delivery pipe 19 is open, and valve 23 in the intake pipe 22 of 15 is open, and when working in series the opposite arrangement obtains. The change-over of the valves may be controlled by a pneumatic pressure device 32 in the cabin adapted to close the switch 31 of an electric circuit comprising relays 26, 27 connected to the valves.
Publications (1)
Publication Number | Publication Date |
---|---|
GB591761A true GB591761A (en) | 1947-08-28 |
Family
ID=1727573
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1341841A Expired GB591761A (en) | 1941-10-17 | Improvements in and relating to aircraft supercharging arrangements |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB591761A (en) |
-
1941
- 1941-10-17 GB GB1341841A patent/GB591761A/en not_active Expired
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