US1408322A - Auxiliary liquid-forcing device for carburetors - Google Patents

Auxiliary liquid-forcing device for carburetors Download PDF

Info

Publication number
US1408322A
US1408322A US311893A US31189319A US1408322A US 1408322 A US1408322 A US 1408322A US 311893 A US311893 A US 311893A US 31189319 A US31189319 A US 31189319A US 1408322 A US1408322 A US 1408322A
Authority
US
United States
Prior art keywords
auxiliary
pump
carburetor
fuel
carburetors
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 - Lifetime
Application number
US311893A
Inventor
Weymann Charles Terres
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 US311893A priority Critical patent/US1408322A/en
Application granted granted Critical
Publication of US1408322A publication Critical patent/US1408322A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04HBUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H12/00Towers; Masts or poles; Chimney stacks; Water-towers; Methods of erecting such structures
    • E04H12/22Sockets or holders for poles or posts
    • E04H12/2207Sockets or holders for poles or posts not used
    • E04H12/2215Sockets or holders for poles or posts not used driven into the ground
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • 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
    • F02M2700/00Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
    • F02M2700/43Arrangements for supplying air, fuel or auxiliary fluids to a combustion space of mixture compressing engines working with liquid fuel
    • F02M2700/4302Arrangements 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
    • F02M2700/438Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters
    • F02M2700/4388Supply of liquid to a carburettor reservoir with limitation of the liquid level; Aerating devices; Mounting of fuel filters with fuel displacement by a pump
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/85978With pump
    • Y10T137/86131Plural
    • Y10T137/86163Parallel

Definitions

  • This invention relates to an auxiliary or emergency apparatus intended to form a temporary substitute for the main feed of an aviation engine, for example, when for any reason, such as a perforation caused by a rojectile, the said main feed fails.
  • he invention mainly comprises a centrifugal pump operated by hand from a distance and immersed in the main feed tank, which pump forces into an auxiliary tank a quantity of petrol intended to replace that which is failing, in order to enable the engine to continue to work until the time when the aviator is out of danger.
  • the accompanying drawing shows diagrammatically, by way of example, a construction according to the invention, which comprises a centrifugal pump d immersed in the main tank 6 and operated by means of a gearing m driven by hand and constituted by a series of gear wheels, one of which operated by the crank handle a imparts a movement of rotation of 1:20 for instance, to a s indle b to which is connected one end of a exible shaft 0. The other end of the said flexible shaft is connected to the spindle of the centrifugal pump 03.
  • the discharge pipe f of the said pump terminates at an auxiliary tank 1' supply ing, by difference in head, or with constant level, the carburetor g.
  • the centrifugal pump 03 does not comprise any fiap valve or other obstacle, owing to which, the discharge piping f of the said pump can be used, if necessary, for an auxiliary main feed piping, even if the said pipin is under suction.
  • This device can be used for forcing any other liquid besides petrol, that is to say, for pumping water out of the bilges of ships, etc.
  • a combination as defined in claim 1 in which the means for forcing the fuel through said passage includes a centrifugal pump arranged in the hydrocarbon reservoir to feed the auxiliary passage and the carburetor, and means for actuating the centrifugal pump when normal feed of the carburetor ceases.
  • a combination as defined in claim 1 in which the means for forcing the fuel through said passage includes a centrifugal pump arr. nged in the hydrocarbon reservolr to feed the auxiliary passage and the carburetor, a flexible transmission shaft to rotate said centrifugal pump, a speed multiplying gear, and a crank for actuating the speed multiplyin gear.
  • apparatus for furnishing hydrocarbons to a carburetor when the main feed for said carburetor is disabled comprising in combination with the main fuel reservolr of the carburetor, an auxiliary reservoir functioning independently of the main feed, an auxiliary pump independent of the carburetor pump for furnishing fuel to the auxiliary reservoir, and auxiliary plping ndependent of the main feed piping of the carburetor for conveying fuel from the auxiliary pump to said auxiliary reservoir.
  • auxiliary pump is of the valveless centrifugal type and is subforcing fuel through said piping, an auxiliary piping for conveying fuel from the main reservoir to the carburetor when the main feed piping or pump is out of operation, said auxiliary piping functioning independently of the main feed iping, an auxiliary pump for circulating Fuel through the auxiliary piping, and means for actuating the auxiliary pump.

Landscapes

  • Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

C. T. WEYMANN.
AUXILIARY LIQUID FORCING DEVICE FOR CARBURETORS.
APPLICATION FILED JULY I8, I919.
Patented Feb. 28, 1922.
UNITED STATES- PATENT OFFICE.
CHARLES TERRES WEYMANN, OF NEUILL'Y-SUR-SEINE, FRANCE.
AUXILIARY LIQUID-FORCING DEVICE FOR CARBURETOBS. I
Specification of Letters Patent.
Patented Feb. 28, 1922.
Application filed July 18, 1919. Serial No. 311,893.
-11'1ents in Auxiliar Li uid-Forcin Devices for Carburetors, (for which I have filed application in France, Sept. 26, 1917, Patent 0. 515,020,) of which the following is a specification.
This invention relates to an auxiliary or emergency apparatus intended to form a temporary substitute for the main feed of an aviation engine, for example, when for any reason, such as a perforation caused by a rojectile, the said main feed fails.
he invention mainly comprises a centrifugal pump operated by hand from a distance and immersed in the main feed tank, which pump forces into an auxiliary tank a quantity of petrol intended to replace that which is failing, in order to enable the engine to continue to work until the time when the aviator is out of danger.
The accompanying drawing shows diagrammatically, by way of example, a construction according to the invention, which comprises a centrifugal pump d immersed in the main tank 6 and operated by means of a gearing m driven by hand and constituted by a series of gear wheels, one of which operated by the crank handle a imparts a movement of rotation of 1:20 for instance, to a s indle b to which is connected one end of a exible shaft 0. The other end of the said flexible shaft is connected to the spindle of the centrifugal pump 03.
The discharge pipe f of the said pump terminates at an auxiliary tank 1' supply ing, by difference in head, or with constant level, the carburetor g. The centrifugal pump 03 does not comprise any fiap valve or other obstacle, owing to which, the discharge piping f of the said pump can be used, if necessary, for an auxiliary main feed piping, even if the said pipin is under suction.
oreover the pump (1 being completely shapes, dimensions, etc., may be varied without departing from the invention.
This device can be used for forcing any other liquid besides petrol, that is to say, for pumping water out of the bilges of ships, etc.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is 1. The combination with an internal combustion engine carburetor, a fuel reservoir,
fuel conducting means connecting the reservoir and carburetor and a main feed pump arranged in the fuel conducting means, of an auxiliary passage functioning independently of the fuel conducting means for conveying fuel from the reservoir to the carburetor, and means for forcing fuel through said auxiliary passage. l
2. A combination as defined in claim 1 in which the means for forcing the fuel through said passage includes a centrifugal pump arranged in the hydrocarbon reservoir to feed the auxiliary passage and the carburetor, and means for actuating the centrifugal pump when normal feed of the carburetor ceases.
3. A combination as defined in claim 1 in which the means for forcing the fuel through said passage includes a centrifugal pump arr. nged in the hydrocarbon reservolr to feed the auxiliary passage and the carburetor, a flexible transmission shaft to rotate said centrifugal pump, a speed multiplying gear, and a crank for actuating the speed multiplyin gear.
4. n apparatus for furnishing hydrocarbons to a carburetor when the main feed for said carburetor is disabled, comprising in combination with the main fuel reservolr of the carburetor, an auxiliary reservoir functioning independently of the main feed, an auxiliary pump independent of the carburetor pump for furnishing fuel to the auxiliary reservoir, and auxiliary plping ndependent of the main feed piping of the carburetor for conveying fuel from the auxiliary pump to said auxiliary reservoir.
5. An apparatus of the kind defined by claim 4 in which the auxiliary pump is submerged in the liquid in the main reservoir.
.6. An apparatus of the kind defined by claim 4 in which the auxiliary pump is of the valveless centrifugal type and is subforcing fuel through said piping, an auxiliary piping for conveying fuel from the main reservoir to the carburetor when the main feed piping or pump is out of operation, said auxiliary piping functioning independently of the main feed iping, an auxiliary pump for circulating Fuel through the auxiliary piping, and means for actuating the auxiliary pump.
In testimony whereof I afiix my signature.
CHARLES TERRES WEYMANN.
US311893A 1919-07-18 1919-07-18 Auxiliary liquid-forcing device for carburetors Expired - Lifetime US1408322A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US311893A US1408322A (en) 1919-07-18 1919-07-18 Auxiliary liquid-forcing device for carburetors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US311893A US1408322A (en) 1919-07-18 1919-07-18 Auxiliary liquid-forcing device for carburetors

Publications (1)

Publication Number Publication Date
US1408322A true US1408322A (en) 1922-02-28

Family

ID=23208972

Family Applications (1)

Application Number Title Priority Date Filing Date
US311893A Expired - Lifetime US1408322A (en) 1919-07-18 1919-07-18 Auxiliary liquid-forcing device for carburetors

Country Status (1)

Country Link
US (1) US1408322A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438311A (en) * 1944-05-15 1948-03-23 Carter Carburetor Corp Pump discharge fitting
US2527615A (en) * 1944-03-29 1950-10-31 Alan Muntz & Co Ltd Fuel injection system for internalcombustion engines
US20090080983A1 (en) * 2007-08-14 2009-03-26 Richard Donovan Short Methods and devices for ground stabilization

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2527615A (en) * 1944-03-29 1950-10-31 Alan Muntz & Co Ltd Fuel injection system for internalcombustion engines
US2438311A (en) * 1944-05-15 1948-03-23 Carter Carburetor Corp Pump discharge fitting
US20090080983A1 (en) * 2007-08-14 2009-03-26 Richard Donovan Short Methods and devices for ground stabilization
US7811032B2 (en) 2007-08-14 2010-10-12 Richard Donovan Short Methods and devices for ground stabilization

Similar Documents

Publication Publication Date Title
US1181634A (en) Auxiliary marine motor.
US1408322A (en) Auxiliary liquid-forcing device for carburetors
US1329997A (en) Means for supplying fuel to internal-combustion engines
US1842858A (en) Hydroplane
US2440262A (en) Fuel supply system for aircraft
US2310361A (en) System and apparatus for propelling boats
US1152567A (en) Propelling apparatus for vessels.
US1138667A (en) Hydraulic power transmission.
US1402408A (en) Fuel control for semi-diesel engines
US1549305A (en) Lubricating mechanism for internal-combustion engines
DE326144C (en) Fuel pump drive for internal combustion engines, especially those for aircraft
US1201594A (en) Mechanism for priming and operating centrifugal pumps.
US1306762A (en) higginson and h
US1459330A (en) Pump for boat-propelling devices
US1299128A (en) Fuel-feed system for aerial machines.
GB463881A (en) Improvements in or relating to dirigible craft such as ships, aircraft and the like
US1880674A (en) Scavenging mechanism for two-cycle engines
US1437265A (en) Aircraft engine
DE861971C (en) Device for engaging friction clutches, especially for piston steam engines with exhaust turbines for ship propulsion
DE528553C (en) Submarine with external fuel oil containers
US2401583A (en) Method of sea water foam suppression and apparatus
GB598654A (en) Improvements in and relating to ship propulsion
DE517633C (en) Fluid control for internal combustion engines
GB124808A (en) Improvements in Fuel Feed Systems for use on Aeroplanes and the like.
US1275482A (en) Torpedo.