GB128260A - Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines. - Google Patents

Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines.

Info

Publication number
GB128260A
GB128260A GB965017A GB965017A GB128260A GB 128260 A GB128260 A GB 128260A GB 965017 A GB965017 A GB 965017A GB 965017 A GB965017 A GB 965017A GB 128260 A GB128260 A GB 128260A
Authority
GB
United Kingdom
Prior art keywords
tank
vessel
liquid fuel
fuel
valve
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
Application number
GB965017A
Inventor
Hugh Oswald Short
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB965017A priority Critical patent/GB128260A/en
Publication of GB128260A publication Critical patent/GB128260A/en
Expired legal-status Critical Current

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
    • F02M2700/4383—Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters with fuel displacement by gas pressure working on the fuel
    • F02M2700/4385—Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters with fuel displacement by gas pressure working on the fuel the pressure being an overpressure

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

128,260. Short, H. O. July 4,1917. Direct air-pressure apparatus, automatic. - Liquid fuel is raised by air pressure from a main tank 1 to another tank 7, whence it can flow to the engine of an aerial machine, and to avoid making the tank 1 heavy enough to withstand the air pressure, a small strong vessel 3 is employed which receives the fuel through a pipe 4 and non-return valve 5. The fuel is expelled from the vessel 3 by air supplied by a pump 9 through a valve 10 and pipe 8. The valve 10 is worked mechanically and puts the vessel 3 into communication alternately with the pump 9 and the top of the tank 1. The vessel 3 and the sump 15 of the tank 7 may be bullet-proof. The tank 1 may be divided into compartments each of which is separately connected to the vessel 3.
GB965017A 1917-07-04 1917-07-04 Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines. Expired GB128260A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB965017A GB128260A (en) 1917-07-04 1917-07-04 Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB965017A GB128260A (en) 1917-07-04 1917-07-04 Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines.

Publications (1)

Publication Number Publication Date
GB128260A true GB128260A (en) 1919-06-26

Family

ID=32343847

Family Applications (1)

Application Number Title Priority Date Filing Date
GB965017A Expired GB128260A (en) 1917-07-04 1917-07-04 Improvements in and Means for Supplying Liquid Fuel to Internal Combustion Engines.

Country Status (1)

Country Link
GB (1) GB128260A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2442639A (en) * 1943-03-08 1948-06-01 Curtis Pump Co Aircraft booster pump and tank assembly

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2442639A (en) * 1943-03-08 1948-06-01 Curtis Pump Co Aircraft booster pump and tank assembly

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