EP3215733A1 - Fuel delivery system - Google Patents

Fuel delivery system

Info

Publication number
EP3215733A1
EP3215733A1 EP15771586.3A EP15771586A EP3215733A1 EP 3215733 A1 EP3215733 A1 EP 3215733A1 EP 15771586 A EP15771586 A EP 15771586A EP 3215733 A1 EP3215733 A1 EP 3215733A1
Authority
EP
European Patent Office
Prior art keywords
fuel
piston
pressure
flow path
venturi
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.)
Withdrawn
Application number
EP15771586.3A
Other languages
German (de)
English (en)
French (fr)
Inventor
Andrew Brown
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.)
Delphi International Operations Luxembourg SARL
Original Assignee
Delphi International Operations Luxembourg SARL
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 Delphi International Operations Luxembourg SARL filed Critical Delphi International Operations Luxembourg SARL
Publication of EP3215733A1 publication Critical patent/EP3215733A1/en
Withdrawn legal-status Critical Current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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/02Fuel-injection apparatus having several injectors fed by a common pumping element, or having several pumping elements feeding a common injector; Fuel-injection apparatus having provisions for cutting-out pumps, pumping elements, or injectors; Fuel-injection apparatus having provisions for variably interconnecting pumping elements and injectors alternatively
    • F02M63/0225Fuel-injection apparatus having a common rail feeding several injectors ; Means for varying pressure in common rails; Pumps feeding common rails
    • F02M63/023Means for varying pressure in common rails
    • F02M63/0235Means for varying pressure in common rails by bleeding fuel pressure
    • F02M63/024Means for varying pressure in common rails by bleeding fuel pressure between the low pressure pump and the high pressure pump
    • 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
    • F02M37/00Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/0011Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
    • F02M37/0023Valves in the fuel supply and return system
    • F02M37/0029Pressure regulator in the low pressure fuel system
    • 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
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/002Arrangement of leakage or drain conduits in or from injectors
    • 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
    • F02M59/00Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
    • F02M59/20Varying fuel delivery in quantity or timing
    • F02M59/34Varying fuel delivery in quantity or timing by throttling of passages to pumping elements or of overflow passages, e.g. throttling by means of a pressure-controlled sliding valve having liquid stop or abutment
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/0031Valves characterized by the type of valves, e.g. special valve member details, valve seat details, valve housing details
    • F02M63/0056Throttling valves, e.g. having variable opening positions throttling the flow
    • 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
    • F02M63/00Other fuel-injection apparatus having pertinent characteristics not provided for in groups F02M39/00 - F02M57/00 or F02M67/00; Details, component parts, or accessories of fuel-injection apparatus, not provided for in, or of interest apart from, the apparatus of groups F02M39/00 - F02M61/00 or F02M67/00; Combination of fuel pump with other devices, e.g. lubricating oil pump
    • F02M63/0012Valves
    • F02M63/007Details not provided for in, or of interest apart from, the apparatus of the groups F02M63/0014 - F02M63/0059
    • F02M63/0073Pressure balanced valves

Definitions

  • the present invention relates to fuel delivery systems, and specifically to pressure regulating means for duel delivery systems for common rail fuel injection systems, such as diesel fuel injection systems.
  • a known fuel delivery system for a common rail application such as a single plunger common rail diesel pump application, comprises a low pressure regulator which controls a return flow of fuel from a cambox to a fuel tank, and a separate venturi, which creates a depression, i.e. a reduction in pressure, for an injector leak return flow path.
  • a fuel flow through the venturi alters depending on an opening/closing function of the regulator.
  • the separate low pressure regulator and venturi of prior art pumps requires multiple internal drillings, and a relatively large pump envelope to accommodate the two separate components.
  • the present invention provides, in a first aspect, pressure regulating means according to claim 1.
  • the pressure regulating means comprises a piston located for reciprocating movement within an outer body of integral component; wherein fuel from the second inlet fuel flow enters a recess of the pressure regulating means via an entry port; wherein the piston is biased by a spring into a closed position in which an exit flow of fuel from the recess to the back-leak fuel flow path is prevented via at least one regulated flow port is prevented, and wherein an exit fuel of fuel from the recess to the back-leak fuel flow path via at least one back-leak return port is enabled; and wherein at a predetermined inlet fuel pressure, the piston is urged against the biasing of the spring into a fully open position, in which exit fuel flows from the recess to the back-leak flow path via the each or regulated flow port and via the or each back-leak return port are enabled;
  • the recess is defined within the piston and the spring is provided in a spring chamber, wherein the recess and the spring chamber are separated by a wall of the piston, the pressure regulating means
  • the venturi may comprise a gap in an internal annular projection provided in the piston.
  • the present invention comprises a fuel delivery system for an internal combustion engine comprising pressure regulating means in accordance with the above.
  • Figure 1 is a schematic representation of an fuel delivery system in accordance with a first embodiment of the present invention
  • Figure 2 is a cross-sectional view of a combined low pressure regulator/venturi component in accordance with the first embodiment of the present invention
  • Figure 3 is a schematic representation of a fuel delivery system in accordance with a second embodiment of the present invention
  • Figure 4 is a cross-sectional view of a combined low pressure regulator/venturi component in accordance with the second embodiment of the present invention.
  • a venturi is incorporated into a low pressure regulator piston, to form a single pressure regulating component.
  • pressure regulating means comprising a combined low pressure regulator/venturi unit 100 in accordance with a first embodiment of the present invention, is illustrated schematically as part of a fuel delivery system 2.
  • Fuel such as diesel is supplied, at low pressure, from a fuel supply comprising a fuel tank 10, to a cambox 12. From the cambox 12, fuel is provided along a first inlet fuel flow path 6, via a filter 14, an inlet metering valve 16 and an inlet valve 18, to a pumping chamber 20. The fuel is subsequently pressurised to a high pressure in the pumping chamber 20, and the high pressure fuel is supplied along a high pressure fuel path 32, via an outlet valve 22 and common rail accumulator volume 24, to one or more injectors 26.
  • a second inlet flow path 8 is also provided from the cambox 12; the second flow path 8 provides fuel, at an inlet pressure, to the regulator/venturi unit 100.
  • the regulator/venturi unit 100 regulates the pressure of this return flow of fuel, thereby controlling the average fuel pressure within the cambox. After exiting the combined regulator/venturi unit 100, a flow of fuel at a back- leak pressure returns to the fuel tank 10 along a back-leak return flow path 30.
  • the regulator/venturi unit 100 also receives a back- leak flow of fuel from the injectors 26, via an injector back-leak flow path 32.
  • the venturi acts upon this injector back-leak flow, and it is subsequently also returned to the fuel tank 10 via the back-leak return flow path 30.
  • regulator/venturi unit 100 The operation of the regulator/venturi unit 100 is described in greater detail below.
  • the combined regulator/venturi unit 100 of a first embodiment of the present invention comprises an outer body 102, in which an internal member comprising a piston 104 is arranged for reciprocating movement therein.
  • An interior of the piston 104 defines a recess 106.
  • the regulator/venturi unit 100 comprises a first, entry end 108, and distal from the first end 108, a second end 110, towards which a spring chamber 120 is provided.
  • the spring chamber 120 is separated from the recess 106 of the piston 104 by a radial wall 112 of the piston.
  • Biasing means comprising a coil spring 122 is provided in the spring chamber 120; the spring 122 abuts a first spring seat 124 provided by an internal face 162 of a radial wall 160 of the outer body 102 defining the second end 110 of the unit 100, and a second spring seat 126 provided by an end face 116 of the piston 104.
  • the piston 104 comprises an internal orifice 130, formed by gap in an annular internal projection 118.
  • the regulator/venturi unit 100 comprises an entry port 134 at the entry end 108, for receiving fuel from the second inlet flow path 108 from the cambox 12.
  • a plurality of ports are provided through the outer body of the unit 100: regulated flow ports 140, 142 are provided towards the first end 108 of the unit 100, a back- leak return port 144 is provided towards the second end 110 of the unit 100, and a venturi port 132 is at a position axially between the regulated flow ports 140, 142 and the back- leak return port 144.
  • back- leak return port 144 is provided in an axial side wall 166 of the outer body of the regulator/venturi unit 100. Additionally, a damping orifice 146 is provided through the outer body
  • the piston 104 is moveable between a fully open position and a fully closed position. In the fully open position, as shown in Figure 2, the piston 104 is at a lowermost position (in the orientation of Figures 1 and 2), and in the closed position, the piston 104 is at an uppermost position.
  • the piston 104 is biased into the fully closed position by the spring, i.e. the spring 122 biases the piston away from the internal end face 162 of the outer body 102 of the unit 100.
  • the regulated flow ports 140, 142 are sealed by an external surface of a top section 168 of an axial wall 164 of the piston 104, thereby closing the flow path out of the recess 106 via the regulated flow ports 140, 142.
  • a fuel flow path is enabled through the venturi port 132, via a corresponding venturi port 170 provided in the axial side wall 166 of the piston 104, into a venturi section 172 of the recess 106.
  • This flow creates a depression which is enabled by cut-outs 152, 154 provided in the external wall 164 of the piston 104 above and below the venturi port 170, which prevent the external wall 164 from sealing the venturi port 132 of the outer body 102.
  • the venturi ports 132, 170 still act to reduce the pressure of the injector back flow received into the recess 106 to the predetermined level.
  • a flow path is enabled out of the recess 106 through the back-leak return port 144, via a corresponding back-leak return port 172 provided in the axial wall of the piston 104, by virtue of further cut-outs 156, 158 provided in the external wall 164 of the piston 104 above and below the back- leak return port 172, which prevent the external wall 164 from sealing the back-leak return port 144.
  • Fuel entering the recess 106 from the injector back- leak flow path 32 via the venturi ports 132, 170 is at a higher pressure than the inlet pressure.
  • the venturi ports 132, 170 create a depression in the injector return flow, thereby reducing the pressure of the injector return flow of fuel, to a predetermined level.
  • Fuel entering the recess 106 via the entry port 134, will be at the inlet pressure, as determined by pressure of fuel exiting the cambox 12. Accordingly, a force provided to the piston 104 by the fuel entering the recess 106 will be dependent upon the magnitude of the inlet pressure.
  • the force applied to the piston 104 will exceed the biasing force of the spring 122.
  • the piston 104 is then urged, along a longitudinal axis A of the regulator/venturi unit 100, towards the internal end face 162 of the outer body 102, i.e. the piston 104 is urged from the fully closed position to the fully open position in which fuel can flow out of the regulated flow ports 140, 142.
  • the piston 104 is pushed downwardly.
  • the spring chamber 120 and the damping orifice 146 act as a damping mechanism to damp movement of the piston 104 towards the internal end face 162 of the outer body 102.
  • the regulated flow ports 140, 142 are no longer obstructed/sealed by the external wall 164 of the piston 104, and therefore an additional flow path is enabled from the cambox 12 to the back-leak return flow path 30, through the regulated flow ports 140, 142, i.e. in the open position, fuel exits to the back-leak return flow path 30, via the regulated flow ports 140, 142 in addition to the back-leak return port 144.
  • a partial flow of fuel can exit via the regulated flow ports 140, 142, i.e. a reduced volume of fuel can exit via the regulated flow ports 140, 142 than if the piston 104 was in the fully open position.
  • the regulator/venturi unit 10 acts to regulate fuel pressure within the cambox 12. If the fuel pressure within the cambox 12 is too great, i.e. exceeds a predetermined value, the piston 104 is caused to move to the open position and allow more fuel to flow through to the back-leak return path 30, thereby reducing the fuel pressure within the cambox 12 to the predetermined pressure. Accordingly, the selected predetermined average fuel pressure is maintained in the cambox 12.
  • the opening pressure for the regulator/venturi component 100 i.e.
  • the pressure at which the piston 104 is caused to move towards the fully open position is determined by the size of the piston internal orifice 130, the rate and pre-load of the spring 122, the positions of the regulated flow ports 140, 142, and the size of the damping orifice 146. These parameters are therefore selected according to the required predetermined average fuel pressure of the cambox 12.
  • the size of the internal orifice 130 is selected to allow the correct volume of fuel through the venturi section 172 to obtain the necessary reduction to a regulated pressure setting.
  • a combined low pressure regulator/venturi unit 200 in accordance with an alternative, second embodiment of the present invention is illustrated schematically as part of a fuel delivery system 202 in Figure 3.
  • the alternative regulator/venturi unit 200 is illustrated in isolation in Figure 4, in a fully open position.
  • the second embodiment comprises a combined regulator/venturi unit 200 comprising a piston 204 which is arranged for reciprocating movement within the outer body 202 of the regulator/venturi unit 200.
  • the piston 204 does not include a radial wall to separate the recess 206 from the spring chamber. Accordingly, the recess 206 comprises the internal area defined within piston 106, and also the spring chamber area.
  • the back-leak return port 244 is located in the radial wall 260 of the outer body 202 of the regulator/venturi unit 200 which defines the second end 210 of the unit 200, remote from the first, entry end 208.
  • opening of the piston i.e. movement of the piston 204 towards the internal end face 262 of the outer body 202, is not damped.
  • the regulated flow ports 240, 242 are sealed by an external surface of a top section 168 of an external wall 264 of the piston 204 however fuel can flow through the back-leak return port 244, and when the piston 204 is in the open position, fuel can flow from the recess 206 through both the back-leak return port 244 as well as through the regulated flow ports 240, 242.
  • the second embodiment therefore allows fuel flow to pass through the regulator/venturi unit 200 with less restriction on the downstream side (i.e. towards the second end 210 of the unit 200) of the venturi ports 232, 270.
  • the pressure of fuel flowing through the venturi is more consistent than in prior art embodiments, as it is incorporated in the regulator. Accordingly, a more consistent depression in fuel pressure is generated by the venturi than in prior art embodiments.
  • the present invention reduces the number of internal drillings required compared to prior art embodiments. Furthermore, combining the venturi and regulator into one component also allows for a reduced overall pump packaging size compared to prior art embodiments.
  • REFERENCES fuel delivery system 2

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
EP15771586.3A 2014-11-04 2015-09-29 Fuel delivery system Withdrawn EP3215733A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1419607.5A GB201419607D0 (en) 2014-11-04 2014-11-04 Fuel delivery system
PCT/EP2015/072353 WO2016071046A1 (en) 2014-11-04 2015-09-29 Fuel delivery system

Publications (1)

Publication Number Publication Date
EP3215733A1 true EP3215733A1 (en) 2017-09-13

Family

ID=52118661

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15771586.3A Withdrawn EP3215733A1 (en) 2014-11-04 2015-09-29 Fuel delivery system

Country Status (5)

Country Link
EP (1) EP3215733A1 (ko)
KR (1) KR20170080623A (ko)
CN (1) CN107002619A (ko)
GB (1) GB201419607D0 (ko)
WO (1) WO2016071046A1 (ko)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2552174A (en) * 2016-07-12 2018-01-17 Delphi Int Operations Luxembourg Sarl Hydraulic fuel circuit of a fuel injection equipment
WO2019238229A1 (en) * 2018-06-13 2019-12-19 Volvo Truck Corporation Flow regulation device, fuel managing system comprising such a device and automotive vehicle comprising such a system
US11092126B2 (en) * 2019-09-03 2021-08-17 Pratt & Whitney Canada Corp. Common-rail fuel system with ejector pump and method of use thereof
WO2022020693A1 (en) * 2020-07-24 2022-01-27 Cummins Inc. Modular and scalable common rail fuel system architecture
DE102021002134B3 (de) * 2021-04-22 2022-09-29 Daimler Truck AG Kraftstoffsystem für eine Verbrennungskraftmaschine, insbesondere eines Kraftfahrzeugs, sowie Kraftfahrzeug mit einem solchen Kraftstoffsystem
DE102021002127B3 (de) * 2021-04-22 2022-09-29 Daimler Truck AG Kraftstoffsystem für eine Verbrennungskraftmaschine, insbesondere eines Kraftfahrzeugs, sowie Kraftfahrzeug mit einem solchen Kraftstoffsystem
CN114017223B (zh) * 2021-11-03 2023-03-24 南岳电控(衡阳)工业技术股份有限公司 一种排油结构及供油系统

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10332484A1 (de) * 2003-07-17 2005-02-10 Robert Bosch Gmbh Kraftstoffeinspritzsystem für Verbrennungskraftmaschinen
DE102007053275B4 (de) * 2007-11-08 2019-09-05 Robert Bosch Gmbh Kraftstoffsystem einer Brennkraftmaschine
JP4968037B2 (ja) * 2007-12-13 2012-07-04 株式会社デンソー 背圧制御弁およびそれを用いた低圧燃料システム
US8800594B2 (en) * 2012-02-02 2014-08-12 Honeywell International Inc. Gas turbine engine fuel return valve and system

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
None *
See also references of WO2016071046A1 *

Also Published As

Publication number Publication date
GB201419607D0 (en) 2014-12-17
WO2016071046A1 (en) 2016-05-12
CN107002619A (zh) 2017-08-01
KR20170080623A (ko) 2017-07-10

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