GB105309A - - Google Patents

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Publication number
GB105309A
GB105309A GB105309DA GB105309A GB 105309 A GB105309 A GB 105309A GB 105309D A GB105309D A GB 105309DA GB 105309 A GB105309 A GB 105309A
Authority
GB
United Kingdom
Prior art keywords
tube
nozzle
well
float chamber
fuel
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 GB105309A publication Critical patent/GB105309A/en
Active legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M7/00Carburettors with means for influencing, e.g. enriching or keeping constant, fuel/air ratio of charge under varying conditions
    • F02M7/06Means for enriching charge on sudden air throttle opening, i.e. at acceleration, e.g. storage means in passage way system

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)

Abstract

105,309. Fagard, J. Nov. 4, 1916. Spray carburettors.-In carburettors wherein an auxiliary " pick-up " nozzle is situated in the choke-tube and is fed from a well open to the atmosphere, the well is supplied from the float chamber through an upstanding tube the flow of fuel through which is automatically arrested as the suction increases and the main nozzle is brought into action. The main nozzle e is fed from the float chamber through the passage c and is surrounded by the auxiliary nozzle j fed from the bottom of the well a open to the atmosphere through a passage g and tube f and supplied from the float chamber through the upstanding tube b. A pilot nozzle m is also supplied from the well a through a tube n. As the throttle t is opened, the flow of fuel through the nozzle j lowers the level in the well a, and air is ultimately drawn through the tube f, which has the effect of arresting the flow of fuel through the tube b. In a modification, the tubes b, f are formed as a single tube with an orifice corresponding to the lower end of the tube f. In a further modification, the auxiliary nozzle enters the choke-tube at right-angles thereto. A restriction may be placed in the tube b, or in the passage c between the float chamber and tube b.
GB105309D Active GB105309A (en)

Publications (1)

Publication Number Publication Date
GB105309A true GB105309A (en)

Family

ID=1700170

Family Applications (1)

Application Number Title Priority Date Filing Date
GB105309D Active GB105309A (en)

Country Status (1)

Country Link
GB (1) GB105309A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4409698A (en) * 1979-12-10 1983-10-18 Toropov Gennady A Tap for pressing elastic thread profiles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4409698A (en) * 1979-12-10 1983-10-18 Toropov Gennady A Tap for pressing elastic thread profiles

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