GB320323A - Improvements in methods and apparatus for producing mixtures of liquids and gases - Google Patents

Improvements in methods and apparatus for producing mixtures of liquids and gases

Info

Publication number
GB320323A
GB320323A GB1926628A GB1926628A GB320323A GB 320323 A GB320323 A GB 320323A GB 1926628 A GB1926628 A GB 1926628A GB 1926628 A GB1926628 A GB 1926628A GB 320323 A GB320323 A GB 320323A
Authority
GB
United Kingdom
Prior art keywords
fuel
capillary
nozzle
passage
air
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
GB1926628A
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 GB1926628A priority Critical patent/GB320323A/en
Publication of GB320323A publication Critical patent/GB320323A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/08Throttle valves specially adapted therefor; Arrangements of such valves in conduits
    • F02D9/10Throttle valves specially adapted therefor; Arrangements of such valves in conduits having pivotally-mounted flaps
    • F02D9/1005Details of the flap
    • F02D9/101Special flap shapes, ribs, bores or the like
    • 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
    • F02M19/00Details, component parts, or accessories of carburettors, not provided for in, or of interest apart from, the apparatus of groups F02M1/00 - F02M17/00

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)

Abstract

320,323. Chambers, E. T. July 3, 1928. Mixing fluids in flow.- Liquids are fed into gaseous fluids in motion through an inverted capillary nozzle, the head of liquid above the nozzle being made less than that required to balance the capillary and surface tension effects by a considerable margin. The method is generally applicable, but the particular applications mentioned are carburetting-apparatus, oil fuel vaporizers or atomizers and blow lamps. A carburettor based on this method comprises a float chamber 2 supplying fuel to a chamber 20 surrounding a sleeve 4 which carries the fuel nozzle and is mounted on the air intake conduit 5. The fuel nozzle comprises either a series of capillary passages or an annular capillary passage 9 formed between a sleeve 6 and an inner member 7, the lower ends of the parts 6, 7 being made thin or knife edged. The member 7 is provided with a fuel controlling restriction 10 forming part of a larger fuel inlet passage 16 and opening into an annular passage 11 communicating with the passage 9. Preferably the upper edges of the sleeve 6 and member 7 are above the fuel level 3, and a siphon cap 12 is provided dipping into the fuel. The area of capillary passage 9 is greater than that of the restriction 10, and its dimensions and the shape of the lower edges of the parts 6, 7 are such that the head necessary to overcome the capillary and surface tension effects is considerably greater than the distance of the fuel level above the lower edge of the nozzle. The fuel nozzle is situated above the top of the intake passage 5 and the outlet is provided with a baffle 15 open on the engine side only. A butterfly throttle 13 is provided and may be formed with two orifices, which may be adjustable, one adjacent the baffle 15 and one remote therefrom, rich mixture and air being respectively supplied through these orifices for slow-running when the throttle is closed. When applied to an oil fuel vaporizer or atomizer, air under pressure is supplied by a blower to an apparatus as described above, the top of the fuel tank and float chamber being connected to the conduit 5 between the blower and the throttle valve. When applied to a blow lamp, the compressed air may pass through a valve of definite proportions and weight and part of the air on the supply side of this valve may be led to the float chamber.
GB1926628A 1928-07-03 1928-07-03 Improvements in methods and apparatus for producing mixtures of liquids and gases Expired GB320323A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1926628A GB320323A (en) 1928-07-03 1928-07-03 Improvements in methods and apparatus for producing mixtures of liquids and gases

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1926628A GB320323A (en) 1928-07-03 1928-07-03 Improvements in methods and apparatus for producing mixtures of liquids and gases

Publications (1)

Publication Number Publication Date
GB320323A true GB320323A (en) 1929-10-03

Family

ID=10126519

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1926628A Expired GB320323A (en) 1928-07-03 1928-07-03 Improvements in methods and apparatus for producing mixtures of liquids and gases

Country Status (1)

Country Link
GB (1) GB320323A (en)

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