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GB135557A - - Google Patents

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Publication number
GB135557A
GB135557A GB135557DA GB135557A GB 135557 A GB135557 A GB 135557A GB 135557D A GB135557D A GB 135557DA GB 135557 A GB135557 A GB 135557A
Authority
GB
United Kingdom
Prior art keywords
air
pressure
plug
choke tube
sensitive
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.)
Active
Application number
Publication of GB135557A publication Critical patent/GB135557A/en
Active legal-status Critical Current

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
    • F02M7/00—Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/12—Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Means For Warming Up And Starting Carburetors (AREA)

Abstract

135,557. Rateau, A. Nov. 6, 1917, [Convention date]. Spray carburettors.-To maintain the proportion of air to fuel constant, the air supply is controlled by devices sensitive respectively to the pressure and temperature of the surrounding air. The choke tube a of the carburettor encloses, at its constricted portion b, a smaller choke tube c to which fuel is supplied through a pipe d. The air inlet of the smaller choke tube is controlled by a plug f actuated through linkages i, j, k, h by a pressure-sensitive device m and temperaturesensitive device n. The plug f may be at the outlet end of the tube c, or the latter may be moved bodily by the sensitive devices. The air may be supplied under pressure by a fan. In a modification, the plug is replaced by a butterfly valve in a branch of the choke tube b. In a further modification, the pressure and temperature sensitive devices are formed in one etructure.
GB135557D Active GB135557A (en)

Publications (1)

Publication Number Publication Date
GB135557A true GB135557A (en)

Family

ID=1728872

Family Applications (1)

Application Number Title Priority Date Filing Date
GB135557D Active GB135557A (en)

Country Status (1)

Country Link
GB (1) GB135557A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457171A (en) * 1944-04-22 1948-12-28 Bendix Aviat Corp Charge forming device
US2482528A (en) * 1945-06-08 1949-09-20 Wright Aeronautical Corp Double-boost venturi construction
US2491548A (en) * 1945-07-24 1949-12-20 Robertshaw Fulton Controls Co Device responsive to variable density
US2502602A (en) * 1944-07-20 1950-04-04 Niles Bement Pond Co Flow restricting device
US2626789A (en) * 1944-11-28 1953-01-27 Bendix Aviat Corp Charge-forming device
US2662757A (en) * 1944-03-01 1953-12-15 Bendix Aviat Corp Density responsive device
US2687122A (en) * 1952-07-18 1954-08-24 Francis P Hareslak Fuel-level control apparatus for model airplanes

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2662757A (en) * 1944-03-01 1953-12-15 Bendix Aviat Corp Density responsive device
US2457171A (en) * 1944-04-22 1948-12-28 Bendix Aviat Corp Charge forming device
US2502602A (en) * 1944-07-20 1950-04-04 Niles Bement Pond Co Flow restricting device
US2626789A (en) * 1944-11-28 1953-01-27 Bendix Aviat Corp Charge-forming device
US2482528A (en) * 1945-06-08 1949-09-20 Wright Aeronautical Corp Double-boost venturi construction
US2491548A (en) * 1945-07-24 1949-12-20 Robertshaw Fulton Controls Co Device responsive to variable density
US2687122A (en) * 1952-07-18 1954-08-24 Francis P Hareslak Fuel-level control apparatus for model airplanes

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