US2251783A - Fuel pump for engines - Google Patents
Fuel pump for engines Download PDFInfo
- Publication number
- US2251783A US2251783A US195859A US19585938A US2251783A US 2251783 A US2251783 A US 2251783A US 195859 A US195859 A US 195859A US 19585938 A US19585938 A US 19585938A US 2251783 A US2251783 A US 2251783A
- Authority
- US
- United States
- Prior art keywords
- fuel
- pump
- plunger
- pumping plunger
- engines
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/20—Varying fuel delivery in quantity or timing
- F02M59/24—Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke
- F02M59/243—Varying fuel delivery in quantity or timing with constant-length-stroke pistons having variable effective portion of stroke caused by movement of cylinders relative to their pistons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/13—Special devices for making an explosive mixture; Fuel pumps
- F02M2700/1317—Fuel pumpo for internal combustion engines
- F02M2700/1382—Fuel pump with control of the cylinder relative to non-rotary piston
Definitions
- My present invention relates to a fuel pump for engines, and particularly to those pumps of the type employed for injecting, liquid fuel under heavy pressure into air highly, compressed in the combustion chamber and space above the piston within the cylinder bore of internal combustion engines, such as the Diesel type engine, and the objects of improvement are, first, to provide a fuel pump that will be positive in its delivery of said fuel under extremely high pressures; second, to provide a fuel pump structure for multiple en-' 'gine units wherein a plurality of pump units are provided, each individually adjustable to the fuel requirement of the particular engine unit it is pumping fuel to; third, to provide a fuel pump of rigid construction, not .liable to disorder and cheap to manufacture.
- Figure 1 is a front elevation of my fuel pump of multiple unit structure in which one of the pump units is partly in section.
- FIG 2 is a sectional view of my pump take on line V. V. of Figure 1, with the fuel control sleeve adjusted to partial pumping operation.
- Figure 3 is a similar sectional view to Figure 2' except the fuel control sleeve is adjusted to maximum fuel pumping operation.
- FIG 4 is an enlarged view of the control connector by the union nut- Within the bore Ill I is stationary sleeve ll shouldered therein by liquid fuel is delivered to the pump.
- Reciprocable within the bore l3 of the bushing I I is pumping plunger I! having axially extending fuel escape port I3 beginning at'the upper end of the pumping plunger to the transverse sleeve ports I! through which the excess fuel escapes to the chamber 20 and through the passage 43 to the chamber 22 and through hole 23 to the spring chamber 24, and back to the fuel container through hole 25 and tube 26 or to any other container as maybe desired.
- Within the base portion l of the pump housing is the.
- plunger operating mechanism consisting of the drive shaft 21 provided'with'operating' cam 28 having a convex lift portion 29, and concave flanks 30 and lift dwell extremity 3
- plunger lift roller 32 pivotally connected to forked lifter arm 33 by pivotal pin 34', and which arm has upwardly extending bosses.
- union connector 5 to which is connected a metal tube extending to the particular engine unit to which the fuel pumped is delivered.
- fuel delivery valve 6 engaging seat I in valve cage 8, the valve 6 being pressed against its seat by helical spring 9.
- the union connector 5 is screw-threaded at its exterior to receive a connector nut on the fuel delivery tube and has its upper end of conical shape to fit into the belied-out end .of the fueldelivery tube and to provide a flange whereby the belled-out end may be drawn against the conicalend of the union vide clearance for the roller 32 and upwardly ex-.
- transverse slot 50 The purpose of the transverse slot 50 is to provide clearance for allowing the removal or insertion of thesleeve sliding gear 52 and shaft 53.
- thefuel pump is also started with the result that as the shaft 21 thereof, to-
- the fuel control sleeve is so adjusted that all of the fuel entering bore l8 through inlet ports 3 I4 is forced past the discharge valve 6 by the 1 pumping plunger, while as shown in Figs/2 and 4, the fuel control sleeve is so adjusted that the ports l9 are partly uncovered, or open and when 5 the fuel control sleeve is in the position shown in Fig. 4, a portion ofthe fuel escapes from the bore l3 and a lesser amount of the fuel is forced 1 past the discharge valve 6 to the engine.
- the amount of fuel required by the engine to.
- the sliding 1 for adjustment of the fuel control sleeve is accomplished by the gear 52 in engagement with the gear rack teeth 5
- I provide an adjustment for timing the stroke of the pumping plunger in relation to the movement of the engine's pistons position, whereby the time of fuel injection to the engine may be varied, and thereby bring about combustion in the several cylinders of a multiple cylinder engine at the exact desired instant which has been found contributes to a reduction of vibration and reduced fuel consumption.
- eccentric 36 supporting one end of lifter arm 33, as by turning the eccentric from 1 rotational movement and the roller together with the arm 33, guide 39 and pumping plunger forced upward on the discharge stroke, either earlier or later as may be desired, by the cam 28.
- the cam in order to overcome noise caused by knocking of the cam against the roller 32, is provided with convex lift portion 29 whereby play between the roller and the semi-circular portion of the cam is taken up before the cam proper contacts the roller, which lift is very rapid after it is started which is due to the concave formed flanks of the cam, which has at its extreme height, dwellportion at 3
Description
F. DAVIS FUEL PUMP FOR ENGINES 5 Sheets-Sheet 1 a W5 INVENTOR 4M 21. pm
Filed March 14, 1938 flqyd A TTORNE Y Aug. 5, 1941.
: W t-F,
Aug. 5, 1941. F. DAVIS 2,251,783
' FUEL PUMP FOR ENGINES Filed March 14, 1938 5 Sheets-Shet z INVENTOR 6M W. Dada A TTORNEY Patented Aug. 5, 1941 FUEL PUMP FOR ENGINES Floyd Davis, Norton Township, Muskegon County Mich.
Application March 14, 1938, Serial No. 195,859
3 Claims.
My present invention relates to a fuel pump for engines, and particularly to those pumps of the type employed for injecting, liquid fuel under heavy pressure into air highly, compressed in the combustion chamber and space above the piston within the cylinder bore of internal combustion engines, such as the Diesel type engine, and the objects of improvement are, first, to provide a fuel pump that will be positive in its delivery of said fuel under extremely high pressures; second, to provide a fuel pump structure for multiple en-' 'gine units wherein a plurality of pump units are provided, each individually adjustable to the fuel requirement of the particular engine unit it is pumping fuel to; third, to provide a fuel pump of rigid construction, not .liable to disorder and cheap to manufacture.
The above named objects and other objects that will appear from a perusal of the following description are attained by the pump structure shown in the accompanying drawings, in which:
Figure 1 is a front elevation of my fuel pump of multiple unit structure in which one of the pump units is partly in section.
Figure 2 is a sectional view of my pump take on line V. V. of Figure 1, with the fuel control sleeve adjusted to partial pumping operation.
Figure 3 is a similar sectional view to Figure 2' except the fuel control sleeve is adjusted to maximum fuel pumping operation.
Figure 4 is an enlarged view of the control connector by the union nut- Within the bore Ill I is stationary sleeve ll shouldered therein by liquid fuel is delivered to the pump. Reciprocable within the bore l3 of the bushing I I is pumping plunger I! having axially extending fuel escape port I3 beginning at'the upper end of the pumping plunger to the transverse sleeve ports I! through which the excess fuel escapes to the chamber 20 and through the passage 43 to the chamber 22 and through hole 23 to the spring chamber 24, and back to the fuel container through hole 25 and tube 26 or to any other container as maybe desired. Within the base portion l of the pump housing is the. pumping plunger operating mechanism consisting of the drive shaft 21 provided'with'operating' cam 28 having a convex lift portion 29, and concave flanks 30 and lift dwell extremity 3| of arc form having its radii emanating from the axis of the shaft 21. En.- gaging the cam 23 is plunger lift roller 32 pivotally connected to forked lifter arm 33 by pivotal pin 34', and which arm has upwardly extending bosses.
' 35 at each side of the roller 32. The forked lever 33 at its opposite end from the said roller 32 encircles eccentric 36 carried by turnable shaft 31 mounted in suitable bearings 38 at each side of the base I. The bosses 35 at each side of the roller 32 are arcked upward and engage the pumping plunger thrust plug 39 reciprocable in the thrust plug guide member 3 of the housing and consisting of a head 40 having slot 4| to pro- Throughout the several views of the drawings,
similar referencenumerals refer to similar parts,
the housing and 3 an intermediate portion of the said housing. At the top of the portion 2 is union connector 5 to which is connected a metal tube extending to the particular engine unit to which the fuel pumped is delivered. Within the union connector 5 is fuel delivery valve 6 engaging seat I in valve cage 8, the valve 6 being pressed against its seat by helical spring 9. The union connector 5 is screw-threaded at its exterior to receive a connector nut on the fuel delivery tube and has its upper end of conical shape to fit into the belied-out end .of the fueldelivery tube and to provide a flange whereby the belled-out end may be drawn against the conicalend of the union vide clearance for the roller 32 and upwardly ex-. tending shank portion 42 having axially extending screw-threaded hole 43 into which is screwed the lower end of the pumping plunger having screw-threaded thereon lock nuts 44 whereby the pump plunger may be adjusted longitudinally for controlling the fuel pumped individually to the engine unit desired; resting on the lock nuts 44 is spring abutment collar 45 engaged by helical spring 46 which spring is engaged "at its upslid for controlling the amount of fuel pumped.
j The purpose of the transverse slot 50 is to provide clearance for allowing the removal or insertion of thesleeve sliding gear 52 and shaft 53. In the operation of my improved fuel pump,
of fuel supply which may be in any suitable container and also between union connector 5 and the fuel injection valve of the particular enginecylinder it is desired to inject fuel into, and
having provided suitable means for driving the pump in synchronism with the longitudinal excursion of the engine's piston, which preferably consists of a chain of gears between the engines 1 main shaft and the shaft of the fuel pump, and having provided the said connections, I start the engine by any one of the well known methods tuclinally to cover or uncover the fuel inlet ports H more or less, I provide an adjustment there- I for between the pumping plunger and the guide tubular connection having been made between 1 the fuel inlet port l5, the hole and the source employed for starting Diesel engines. As the engine is started, thefuel pump isalso started with the result that as the shaft 21 thereof, to-
, gether with the cam 28, which in its rotation,
lifts the friction reduction roller 32 and plunger guide 39 and through its connection with the pumping plunger l'l causes the pumping plunger to slide upwardly through the fuel control sleeve 48, closing the fuel inlet port 14, thus trapping I any fuel above the pumping plunger in the bore portion l3 of the bushing ll, which trapped fuel as the pumping plunger continues to move upward is forced past the fuel delivery valve 6 through the union connector 5 and conductor tube which 'is connected therewith, and to the engine. "The quantity of fuel pumped to the engine is controlled by the fuel control sleeve 48 which controlsthe radial ports l9 having communication with the bore l3 above the pumping plunger through fuel escape port l8. In Fig. 3, the fuel control sleeve is so adjusted that all of the fuel entering bore l8 through inlet ports 3 I4 is forced past the discharge valve 6 by the 1 pumping plunger, while as shown in Figs/2 and 4, the fuel control sleeve is so adjusted that the ports l9 are partly uncovered, or open and when 5 the fuel control sleeve is in the position shown in Fig. 4, a portion ofthe fuel escapes from the bore l3 and a lesser amount of the fuel is forced 1 past the discharge valve 6 to the engine. Thus, the amount of fuel required by the engine to. perform the desired work is controlled, as when the fuel control sleeve is adjusted to a position that will not allow the radial ports to be uncovered during the pumping plungers reciprocable excursions, the full amount o'f'fuel will be delivered to the engine, and when the fuel control sleeve is adjusted to a position where the I radial ports are uncovered by the sleeve, or partly uncovered, during the pumpingv plunger's fuel forcing excursions, a lesser amount of fuel will be forced to the engine and the surplus fuel will flow into the chamber 20 and from thence through the slot 49 to the chamber 22 I and where it is piped to the fuel supply. The sliding 1 for adjustment of the fuel control sleeve is accomplished by the gear 52 in engagement with the gear rack teeth 5|, at the side of the fuel 1 control sleeve which has in circumferential rela- 1 tion to the said teeth, slot or groove 43 through 1 which the surplus fuel escapes from the cham- -ber 20 between the sleeves I l and 43. to the chamthrough holes 23 to spring chamber 24 from member 39 by threading the end of the pumping plunger into the guide member and lock the plunger in the guide member by nuts 44, against relative displacement, and in addition to the adjustment of the pumping plunger to properly cover and uncover the fuel inlet ports it, I provide an adjustment for timing the stroke of the pumping plunger in relation to the movement of the engine's pistons position, whereby the time of fuel injection to the engine may be varied, and thereby bring about combustion in the several cylinders of a multiple cylinder engine at the exact desired instant which has been found contributes to a reduction of vibration and reduced fuel consumption. This adjustment of timing the instant of fuel injection is accomplished by eccentric 36 supporting one end of lifter arm 33, as by turning the eccentric from 1 rotational movement and the roller together with the arm 33, guide 39 and pumping plunger forced upward on the discharge stroke, either earlier or later as may be desired, by the cam 28. The cam in order to overcome noise caused by knocking of the cam against the roller 32, is provided with convex lift portion 29 whereby play between the roller and the semi-circular portion of the cam is taken up before the cam proper contacts the roller, which lift is very rapid after it is started which is due to the concave formed flanks of the cam, which has at its extreme height, dwellportion at 3| whereby the fuel pumped by the pumping plunger is given time to somewhat settle to escape from the pump and through the delivery tube back to the fuel container.
Having described my improved fuel pump for engines, the rights I desire to secure are set forth in the following'claims.
I'claim: I 1, In a fuel pump for engines, a reciprocal pumping plunger having extending axially there-- in from is upper end an excess fuel port, and an excess fuel port extending transversely through the pumping plunger :and open to the axially extending port a slidable fuel control sleeve surrounding the upper 'end portion of the pumping plunger and slidable in the pump housing and having its upper end registering with the transversely extending excess fuel port, a stationary fuel control sleeve having extending from therein the upperend of the pumping plunger, the said stationary sleeve having apart in register with the end of the pumping plunger and with the pumps fuel supply port, and a chamber between the upper end of the slidablesleeve and the lower end of the fixed sleeve for varying the 7 capacity of the pump or amount of fuel pumped.
her ,22, from where it drains'through the. hole b 2: to chamber thereof through hole a and tube 28 back to the fuel ejontiiinei'l' In order that the pumping plunger may be adjusted longi- 2. Inan internal combustion engine fuel pump having a housing with a cylindrical bore and a reciprocal plunger in the bore, the said plunger having a free upper end with an excess fuel escapeport extending axially of the plunger from the free end thereof and having communication with an excess fuel escape port extending transversely through the pumping plunger, a stationary sleeve extending into the cylindrical bore of the housing, and having a port in registry with the free end of the pumping plunger that extends slidably in the said sleeve, the port being in registry with the free end of the pumping plunger having time registry with the fuel supply port of the pump, and a fuel control sleeve slidable in the cylindrical bore of the housing and surrounding the pumping plunger, intermediate the ends thereof, for controlling the escape of excess fuel from the excess fuel port that extends transversely through the pumping plunger, the said sleeve being slidable in the cylindrical bore of the housing, and having a slot at its periphery extending from end to end of the sleeve, for permitting escape or excess fuel from the chamber between the said stationary and slidable sleeves.
3. A structure containing the elements in combination defined in claim 2 and including, a cam shaft having thereon a cam comprising liit portion having two concave flanks and convex portions between the said concave flanks and the cam shaft, and means interposed between the cam and the pumping plunger for gnoving the plunger in response to rotation of the said cam.
FLOYD DAVIS.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US195859A US2251783A (en) | 1938-03-14 | 1938-03-14 | Fuel pump for engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US195859A US2251783A (en) | 1938-03-14 | 1938-03-14 | Fuel pump for engines |
Publications (1)
Publication Number | Publication Date |
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US2251783A true US2251783A (en) | 1941-08-05 |
Family
ID=22723113
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US195859A Expired - Lifetime US2251783A (en) | 1938-03-14 | 1938-03-14 | Fuel pump for engines |
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Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2436797A (en) * | 1943-12-27 | 1948-03-02 | Deschamps Fuel Injection Corp | Fuel injection pump |
US2439879A (en) * | 1944-12-02 | 1948-04-20 | Allen Ivis James | Multicylinder fuel injection pump |
US2455571A (en) * | 1944-11-11 | 1948-12-07 | Timken Roller Bearing Co | Fuel injection pump |
US2517483A (en) * | 1945-05-24 | 1950-08-01 | Mono Cam Ltd | Fuel injection pump |
US2519893A (en) * | 1943-09-23 | 1950-08-22 | Deschamps Fuel Injection Corp | Fuel injection pump |
US2555005A (en) * | 1948-01-31 | 1951-05-29 | Gen Electric | Reciprocating compressor with unloading and capacity modulating control |
US2588481A (en) * | 1942-07-22 | 1952-03-11 | Niles Bement Pond Co | Fuel injector pump mechanism |
US2661729A (en) * | 1948-06-02 | 1953-12-08 | Cummins Engine Co Inc | Fuel feeding apparatus |
US3247800A (en) * | 1959-07-02 | 1966-04-26 | John F Campbell | Pump |
US4069799A (en) * | 1974-06-20 | 1978-01-24 | Warszawskie Zaklady Mechaniczne "Deltawzm" | Injection pump |
WO1993023667A1 (en) * | 1992-05-18 | 1993-11-25 | Paul Marius A | Fuel injector system |
-
1938
- 1938-03-14 US US195859A patent/US2251783A/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2588481A (en) * | 1942-07-22 | 1952-03-11 | Niles Bement Pond Co | Fuel injector pump mechanism |
US2519893A (en) * | 1943-09-23 | 1950-08-22 | Deschamps Fuel Injection Corp | Fuel injection pump |
US2436797A (en) * | 1943-12-27 | 1948-03-02 | Deschamps Fuel Injection Corp | Fuel injection pump |
US2455571A (en) * | 1944-11-11 | 1948-12-07 | Timken Roller Bearing Co | Fuel injection pump |
US2439879A (en) * | 1944-12-02 | 1948-04-20 | Allen Ivis James | Multicylinder fuel injection pump |
US2517483A (en) * | 1945-05-24 | 1950-08-01 | Mono Cam Ltd | Fuel injection pump |
US2555005A (en) * | 1948-01-31 | 1951-05-29 | Gen Electric | Reciprocating compressor with unloading and capacity modulating control |
US2661729A (en) * | 1948-06-02 | 1953-12-08 | Cummins Engine Co Inc | Fuel feeding apparatus |
US3247800A (en) * | 1959-07-02 | 1966-04-26 | John F Campbell | Pump |
US4069799A (en) * | 1974-06-20 | 1978-01-24 | Warszawskie Zaklady Mechaniczne "Deltawzm" | Injection pump |
US5299919A (en) * | 1991-11-01 | 1994-04-05 | Paul Marius A | Fuel injector system |
WO1993023667A1 (en) * | 1992-05-18 | 1993-11-25 | Paul Marius A | Fuel injector system |
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