GB480236A - Improvements in or relating to charging blowers of the internal combustion engines on aircraft - Google Patents
Improvements in or relating to charging blowers of the internal combustion engines on aircraftInfo
- Publication number
- GB480236A GB480236A GB2341037A GB2341037A GB480236A GB 480236 A GB480236 A GB 480236A GB 2341037 A GB2341037 A GB 2341037A GB 2341037 A GB2341037 A GB 2341037A GB 480236 A GB480236 A GB 480236A
- Authority
- GB
- United Kingdom
- Prior art keywords
- liquid
- byepass
- clutches
- delivery
- action
- 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
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D9/00—Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2700/00—Mechanical control of speed or power of a single cylinder piston engine
- F02D2700/02—Controlling by changing the air or fuel supply
- F02D2700/0217—Controlling by changing the air or fuel supply for mixture compressing engines using liquid fuel
- F02D2700/0225—Control of air or mixture supply
- F02D2700/0246—Control of air or mixture supply for engines with compressor
- F02D2700/0256—Control of air or mixture supply for engines with compressor by changing the speed of the compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
480,236. Regulating. TUGWOOD, R. J. (Daimler-Benz Akt.-Ges.) Aug. 26, 1937, No. 23410. [Class 7 (vi)] Two or more charging pumps 17, 18 of an aircraft engine are driven through liquid clutches 15, 16 which are brought into action in succession by liquid from a single pump 26. A multi-way cock-valve 29 is operated by a barometric device 35 so that as the atmospheric pressure lessens on ascending, the valve 29 causes : (a) delivery through the branched passage 27 to return to a supply tank 24 by a branched byepass 33, the' clutches being then both out of action ; (b) delivery to pipe 32 only, port 31 still returning liquid to the byepass ; (c) delivery to both pipes 32, 34, the byepass being entirely closed. The pipes 32, 34 lead to the clutches 15, 16 which are thus brought into action in succession, liquid returning to the supply tank 24 by a pipe 23. The device 35 may be under the influence of the external air or the air delivered by the pump 18. A hand-operated valve may be arranged in the liquid return pipe 23.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2341037A GB480236A (en) | 1937-08-26 | 1937-08-26 | Improvements in or relating to charging blowers of the internal combustion engines on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2341037A GB480236A (en) | 1937-08-26 | 1937-08-26 | Improvements in or relating to charging blowers of the internal combustion engines on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB480236A true GB480236A (en) | 1938-02-18 |
Family
ID=10195168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2341037A Expired GB480236A (en) | 1937-08-26 | 1937-08-26 | Improvements in or relating to charging blowers of the internal combustion engines on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB480236A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444456A (en) * | 1943-08-19 | 1948-07-06 | Jarvis C Marble | Supercharging system for internal-combustion engines |
US2526409A (en) * | 1945-01-09 | 1950-10-17 | Lockheed Aircraft Corp | Turbo-propeller type power plant having radial flow exhaust turbine means |
US2540991A (en) * | 1942-03-06 | 1951-02-06 | Lockheed Aircraft Corp | Gas reaction aircraft power plant |
-
1937
- 1937-08-26 GB GB2341037A patent/GB480236A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2540991A (en) * | 1942-03-06 | 1951-02-06 | Lockheed Aircraft Corp | Gas reaction aircraft power plant |
US2444456A (en) * | 1943-08-19 | 1948-07-06 | Jarvis C Marble | Supercharging system for internal-combustion engines |
US2526409A (en) * | 1945-01-09 | 1950-10-17 | Lockheed Aircraft Corp | Turbo-propeller type power plant having radial flow exhaust turbine means |
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