US1757514A - Oil pump for internal-combustion engines - Google Patents

Oil pump for internal-combustion engines Download PDF

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Publication number
US1757514A
US1757514A US139884A US13988426A US1757514A US 1757514 A US1757514 A US 1757514A US 139884 A US139884 A US 139884A US 13988426 A US13988426 A US 13988426A US 1757514 A US1757514 A US 1757514A
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United States
Prior art keywords
oil
air
pump
internal
slot
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Expired - Lifetime
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US139884A
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Joseph C Coulombe
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Individual
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Priority to US139884A priority Critical patent/US1757514A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01MLUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
    • F01M1/00Pressure lubrication
    • F01M1/02Pressure lubrication using lubricating 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
    • F02M41/00Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor
    • F02M41/08Fuel-injection apparatus with two or more injectors fed from a common pressure-source sequentially by means of a distributor the distributor and pumping elements being combined
    • 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
    • F02M2700/13Special devices for making an explosive mixture; Fuel pumps
    • F02M2700/1317Fuel pumpo for internal combustion engines
    • F02M2700/1329Controlled rotary fuel pump with parallel pistons or with a single piston in the extension of the driving shaft

Definitions

  • Fig. 4 is a sectional view through line g
  • the rotor 1 is eccentrically disposed in pump body 2 and has a shaft 3 extending into bearing 4 of the pump.
  • the blades 5 rotate in the pum body and are driven by the rotor in whic they reciprocate.
  • il intake port 6 terminates in a series of holes 7.
  • Air intake port 8 terminates in the pump body in a crescent-shaped slot 9.
  • the outlet port 14 terminates in the saw slot 15.
  • annular groove 10 Near the extremity of rotor shaft 3 is an annular groove 10 which collects the surplus oil from the shaft bearing. From the groove 10 to its extremity the shaft diameter is reduced to form a thin annular space 11, to al low admission of air to air port 8, together with the oil collected in the groove 10.
  • An air line 12 is connected to air port 8 and may be extended to any chamber that it is desired toevacuate of air.
  • the intermittent flow of air. to the pump is obtained by the slide-valve action of the rotor 1 over the slot 9, through connecting slot 13..
  • the length of slot 9 and its relative location to oil intake 7 will vary the roportion of air and oil pumped. Instead 0t allowing the oil port 6 to breakthrough into the pump bore, it is sometimes preferable to use a number of holes placed in a line parallel with the pump bore, in order to allow for a longer slot 9. Due to inertiaythe slot 9 may. be arranged to slightly overlap the opening of oil intake 7 to advantage.
  • a rotary pump having two inlets, means for continuously creating a suction through one inlet and means for creating a suction at intervals through the other inlet, the suction from the second inlet being segregated from pump for the remainder of ,that of the first.
  • a rotary pump having two segregated inlets and a common outlet, rotating means for closing one of said inlets at equal intervals and continuously drawing from the other of said inlets.

Description

7 May 6, 1930. J. c. COULOMBE OIL PUMP FOR INTERNAL COMBUSTION ENGINES Filed Oct. 6, 1926 I N VEN TOR.
FIG- 2 Patented 6, 1930 JOSEPH O. CGULOMBE, F KOKOMO, INDIANA.
OIL'LPUMP FOR INTERNAL-COMBUSEEION ENGINES Application flied October 6, 1926. Serial No. 1.393%.
Fig. 4 is a sectional view through line g The rotor 1 is eccentrically disposed in pump body 2 and has a shaft 3 extending into bearing 4 of the pump. The blades 5 rotate in the pum body and are driven by the rotor in whic they reciprocate.
il intake port 6 terminates in a series of holes 7.
Air intake port 8 terminates in the pump body in a crescent-shaped slot 9.
Slots 13, in the rotor behind the blades 5, connect the slot 9 to the pump.
The outlet port 14 terminates in the saw slot 15.
Near the extremity of rotor shaft 3 is an annular groove 10 which collects the surplus oil from the shaft bearing. From the groove 10 to its extremity the shaft diameter is reduced to form a thin annular space 11, to al low admission of air to air port 8, together with the oil collected in the groove 10.
An air line 12 is connected to air port 8 and may be extended to any chamber that it is desired toevacuate of air.
My prior patents No. 1,424,? 15, issued Aug. -1 1922, and No. 1,408,801, issued Mar.7,l922, show oil pumps in which air is added to the circulating oil. In these patents the proportion of air and oil pumped is governed by metering the ports and the flow of air to the pumps 1s continuous. Whereas in the present application the flow of air to the pump is intermittent and the timing of this intermittent action assists in proportioning the air and oil'pumped. I
The intermittent flow of air. to the pump is obtained by the slide-valve action of the rotor 1 over the slot 9, through connecting slot 13.. The length of slot 9 and its relative location to oil intake 7 will vary the roportion of air and oil pumped. Instead 0t allowing the oil port 6 to breakthrough into the pump bore, it is sometimes preferable to use a number of holes placed in a line parallel with the pump bore, in order to allow for a longer slot 9. Due to inertiaythe slot 9 may. be arranged to slightly overlap the opening of oil intake 7 to advantage.
The operation is as follows:
After each blade passes dead center, air will be drawn into the pump from annular space 11 and airline 12, throughports 8 and slots 9 and 13, until slot 9 is closed by slot 13 passing beyond its extremity. After the closing of slot 9, or shortly before, the blade 5 will pass the oil holes 7 allowing oil to be I drawn into the the intake cycle.
I claim:
1. A rotary pump having two inlets, means for continuously creating a suction through one inlet and means for creating a suction at intervals through the other inlet, the suction from the second inlet being segregated from pump for the remainder of ,that of the first.
2. A rotary pump having two segregated inlets and a common outlet, rotating means for closing one of said inlets at equal intervals and continuously drawing from the other of said inlets.
I JOSEPH C. COULOMBE.
US139884A 1926-10-06 1926-10-06 Oil pump for internal-combustion engines Expired - Lifetime US1757514A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US139884A US1757514A (en) 1926-10-06 1926-10-06 Oil pump for internal-combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US139884A US1757514A (en) 1926-10-06 1926-10-06 Oil pump for internal-combustion engines

Publications (1)

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US1757514A true US1757514A (en) 1930-05-06

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US139884A Expired - Lifetime US1757514A (en) 1926-10-06 1926-10-06 Oil pump for internal-combustion engines

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2455647A (en) * 1942-07-29 1948-12-07 Leslie W Beaven Engine construction
US2918009A (en) * 1957-02-01 1959-12-22 Dieny & Lucas Soc Nouv Injection-compressor apparatus
US3094707A (en) * 1961-01-10 1963-06-25 American Corp Combination toilet and chemical treating facility
US3285180A (en) * 1963-12-20 1966-11-15 Nat Union Electric Corp Oil burner pump
US3936246A (en) * 1974-06-28 1976-02-03 Chromalloy American Corporation Mixing pump and method of mixing using same

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2455647A (en) * 1942-07-29 1948-12-07 Leslie W Beaven Engine construction
US2918009A (en) * 1957-02-01 1959-12-22 Dieny & Lucas Soc Nouv Injection-compressor apparatus
US3094707A (en) * 1961-01-10 1963-06-25 American Corp Combination toilet and chemical treating facility
US3285180A (en) * 1963-12-20 1966-11-15 Nat Union Electric Corp Oil burner pump
US3936246A (en) * 1974-06-28 1976-02-03 Chromalloy American Corporation Mixing pump and method of mixing using same

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