GB167209A - Improvements in or relating to fuel supply systems for aircraft engines - Google Patents
Improvements in or relating to fuel supply systems for aircraft enginesInfo
- Publication number
- GB167209A GB167209A GB680820A GB680820A GB167209A GB 167209 A GB167209 A GB 167209A GB 680820 A GB680820 A GB 680820A GB 680820 A GB680820 A GB 680820A GB 167209 A GB167209 A GB 167209A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pipe
- float
- service tank
- fuel
- tank
- 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
- F02B1/00—Engines characterised by fuel-air mixture compression
-
- 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
- F02M2700/43—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
- F02M2700/4302—Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel whereby air and fuel are sucked into the mixture conduit
- F02M2700/438—Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters
- F02M2700/4388—Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters with fuel displacement by a pump
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Abstract
167,209. Vickers, Ltd., and Duncan, T. S. March 5, 1920. Liquid fuel, supplying.-Fuel for the engines of aircraft is delivered from the main tanks A to the service tank D by wind-driven pumps C, C', which are primed by a hand pump B. The flow is controlled by a float E, Fig. 2, in the service tank and surrounding the supply-pipe 6; the float valve is formed by a coned ring E<1> resiliently carried by the float and closing a number of outlet orifices F<1> from the pipe 6. The float has a vent-pipe E<4> extending to the bottom to enable any fuel that has leaked into the float to be forced out by the difference in pressure that may occur between the interior and exterior of the float. A vent-pipe F is provided for the service tank. An overflow pipe returns fuel from the service tank to the main tank and a second pipe through which fuel flows continually has an indicator 10<a> therein; the overflow pipe may act as the indicator pipe. The service tank supplies the carburettors through the valved pipes 8. The hand-pump is primed from the service tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB680820A GB167209A (en) | 1920-03-05 | 1920-03-05 | Improvements in or relating to fuel supply systems for aircraft engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB680820A GB167209A (en) | 1920-03-05 | 1920-03-05 | Improvements in or relating to fuel supply systems for aircraft engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB167209A true GB167209A (en) | 1921-08-05 |
Family
ID=9821128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB680820A Expired GB167209A (en) | 1920-03-05 | 1920-03-05 | Improvements in or relating to fuel supply systems for aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB167209A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111038712A (en) * | 2019-12-17 | 2020-04-21 | 石家庄飞机工业有限责任公司 | Intermediate oil supply device of fuel oil system |
-
1920
- 1920-03-05 GB GB680820A patent/GB167209A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111038712A (en) * | 2019-12-17 | 2020-04-21 | 石家庄飞机工业有限责任公司 | Intermediate oil supply device of fuel oil system |
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