GB155082A - Improvements in supplementary liquid fuel tanks of the vacuum gravity type - Google Patents
Improvements in supplementary liquid fuel tanks of the vacuum gravity typeInfo
- Publication number
- GB155082A GB155082A GB2586219A GB2586219A GB155082A GB 155082 A GB155082 A GB 155082A GB 2586219 A GB2586219 A GB 2586219A GB 2586219 A GB2586219 A GB 2586219A GB 155082 A GB155082 A GB 155082A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- container
- fuel
- pipe
- vacuum
- 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
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/02—Feeding by means of suction apparatus, e.g. by air flow through carburettors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
155,082. Paterson, T. W. Oct. 22, 1919. Vacuum apparatus.-A vacuum fuel-feed apparatus comprises an outer fixed container 1 open to the atmosphere, a fixed intermediate container 2 connected by a pipe 15 to suction, and an inner movable container 3, balanced by the weights 8 and provided with a valve 10, the stem 11 of which carries a valve controlling the admission of fuel to the container 2. When the fuel rises. in the container 2 and overflows into the container 3, the latter falls and opens the atmospheric valve 7, so as to break the vacuum, and at the same time opens the valve 10 and a diskvalve 6, and closes the inlet valve 11. The fuel then flows into the container 1, which is connected to the carburettor. When the containers 2, 3 are empty, the latter rises, thereby closing the valves 6, 7, 10, and opening the valve 11, and the cycle is repeated. The valve 6 carries a tube 13 which is depressed when the container 3 falls. A stand-pipe 18 may be mounted on the delivery pipe 17 to indicate the rate of feed. A valve under the pressure of the lubricating system, as described in Specification 142,049, [Class 122 (iv), Steam-engines, Regulating &c.], may be arranged in the pipe 15, so that, if the lubricating system fails, the valve cuts off the suction and the fuel supply to the engine stops.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2586219A GB155082A (en) | 1919-10-22 | 1919-10-22 | Improvements in supplementary liquid fuel tanks of the vacuum gravity type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2586219A GB155082A (en) | 1919-10-22 | 1919-10-22 | Improvements in supplementary liquid fuel tanks of the vacuum gravity type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB155082A true GB155082A (en) | 1920-12-16 |
Family
ID=10234551
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2586219A Expired GB155082A (en) | 1919-10-22 | 1919-10-22 | Improvements in supplementary liquid fuel tanks of the vacuum gravity type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB155082A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102378855A (en) * | 2009-03-31 | 2012-03-14 | 斯奈克玛 | Rotating inlet cowl for a turbine engine, including an eccentric front end |
-
1919
- 1919-10-22 GB GB2586219A patent/GB155082A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102378855A (en) * | 2009-03-31 | 2012-03-14 | 斯奈克玛 | Rotating inlet cowl for a turbine engine, including an eccentric front end |
CN102378855B (en) * | 2009-03-31 | 2014-03-12 | 斯奈克玛 | Rotating inlet cowl for turbine engine, including eccentric front end |
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