GB420295A - Improvements relating to carburetors for internal combustion engines - Google Patents

Improvements relating to carburetors for internal combustion engines

Info

Publication number
GB420295A
GB420295A GB13239/33A GB1323933A GB420295A GB 420295 A GB420295 A GB 420295A GB 13239/33 A GB13239/33 A GB 13239/33A GB 1323933 A GB1323933 A GB 1323933A GB 420295 A GB420295 A GB 420295A
Authority
GB
United Kingdom
Prior art keywords
arm
venturi
tube
nozzle
cast
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
GB13239/33A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB420295A publication Critical patent/GB420295A/en
Expired 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
    • F02M7/08Means for enriching charge on sudden air throttle opening, i.e. at acceleration, e.g. storage means in passage way system using pumps
    • 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
    • F02M7/12Other installations, with moving parts, for influencing fuel/air ratio, e.g. having valves
    • F02M7/133Auxiliary jets, i.e. operating only under certain conditions, e.g. full power
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S261/00Gas and liquid contact apparatus
    • Y10S261/81Percolation control

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

420,295. Spray carburetters. BENDIX AVIATION CORPORATION, 105, West Adams Street, Chicago, U.S.A. May 6, 1933, No. 13239. Convention date, May 7, 1932. [Class 7 (iii)] A carburetter body formed in two sections has a float chamber and a double Venturi cast integral with one of the sections. A downdraught carburetter comprises an upper body portion 8, preferably of aluminium alloy and formed by die casting, and a lower body portion 9 preferably of cast iron and formed as a plain tube with relatively thin walls and separated from the upper portion by a non- conducting gasket 10. A choke valve 13 mounted on a shaft 14 is provided with a poppet valve 15. The upper section is cast with a float chamber 21 and also with an inner Venturi 36 and an outer Venturi 34, this being made possible by a fin 38 which contains the nozzle in the form of a tubular member 45 held in place by a metering plug 53. Tube 45 is cut away on its outer surface at 54 to provide an air-bleed passage, which communicates at one end with the bore of the tube through ports 56, and at the other end with the main air passage through a duct 60. The tube is also cut away circumferentially at 62 to provide communication with an idling duct 64, 66 which leads, through passage 72, Fig. 4, to a nozzle 76 beyond the throttle valve 19. The throttle is actuated through a lever 82 and the other end of the spindle has an arm 88, Fig. 5, connected to one arm 92 of a jointed lever the other arm 93 of which is connected to the rod 98, Fig. 4, of an accelerating pump. The members of the jointed lever turn about a pin 94, Fig. 3, and are normally held by a spring 97 so that the arm 92 is in contact with a stop 96 on the arm 93. On rapid opening of the throttle 19, the lever arms are relatively displaced against the tension of the spring with the result that the plunger of the accelerating pump has a slow and prolonged movement. The cylinder 102 of the accelerating pump is cast with the upper body section 8 and communicates with the float chamber through a port 103, Fig. 5. The lower end of the cylinder is connected through a port 111 with an accelerating-fuel nozzle 112, Fig. 4. In a modification, Fig. 8, (not shown) a second fin is provided in alignment with the fin 38, and the inner Venturi is provided at its upper end with a cap which constitutes the main nozzle. The cap is recessed on its outer surface to form a chamber registering with the fuel passage and communicating with the Venturi through holes in the cap.
GB13239/33A 1932-05-07 1933-05-06 Improvements relating to carburetors for internal combustion engines Expired GB420295A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US609931A US2042770A (en) 1932-05-07 1932-05-07 Carburetor

Publications (1)

Publication Number Publication Date
GB420295A true GB420295A (en) 1934-11-29

Family

ID=24442935

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13239/33A Expired GB420295A (en) 1932-05-07 1933-05-06 Improvements relating to carburetors for internal combustion engines

Country Status (4)

Country Link
US (1) US2042770A (en)
DE (1) DE645433C (en)
FR (1) FR755106A (en)
GB (1) GB420295A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE846634C (en) * 1940-07-26 1952-08-14 Bendix Aviat Corp Carburetor

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2603466A (en) * 1948-10-27 1952-07-15 Thompson Prod Inc Mounting for supplementary feed device for internal-combustion engines
US2782073A (en) * 1953-10-30 1957-02-19 Stephen C Shadegg Nebulizers
US3210054A (en) * 1962-04-09 1965-10-05 Eugene R Gettell Carburetor accelerator pump lockout
DE3604715A1 (en) * 1986-02-14 1987-08-20 Joseph Plannerer CARBURETOR FOR COMBUSTION ENGINES AND IDLE INSTALLATION COMPONENT HERE

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE846634C (en) * 1940-07-26 1952-08-14 Bendix Aviat Corp Carburetor

Also Published As

Publication number Publication date
DE645433C (en) 1937-05-27
US2042770A (en) 1936-06-02
FR755106A (en) 1933-11-20

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