EP4010581A1 - High-pressure fuel pump - Google Patents

High-pressure fuel pump

Info

Publication number
EP4010581A1
EP4010581A1 EP20745158.4A EP20745158A EP4010581A1 EP 4010581 A1 EP4010581 A1 EP 4010581A1 EP 20745158 A EP20745158 A EP 20745158A EP 4010581 A1 EP4010581 A1 EP 4010581A1
Authority
EP
European Patent Office
Prior art keywords
fuel pump
pressure fuel
membranes
section
pressure
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Withdrawn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
EP20745158.4A
Other languages
German (de)
French (fr)
Inventor
Stefan Kolb
Daniel Beckmann
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP4010581A1 publication Critical patent/EP4010581A1/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Withdrawn legal-status Critical Current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
    • 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
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • 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
    • F02M37/0041Means for damping pressure pulsations
    • 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
    • F02M59/44Details, components parts, or accessories not provided for in, or of interest apart from, the apparatus of groups F02M59/02 - F02M59/42; Pumps having transducers, e.g. to measure displacement of pump rack or piston
    • F02M59/48Assembling; Disassembling; Replacing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/04Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B1/053Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with actuating or actuated elements at the inner ends of the cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B11/00Equalisation of pulses, e.g. by use of air vessels; Counteracting cavitation
    • F04B11/0008Equalisation of pulses, e.g. by use of air vessels; Counteracting cavitation using accumulators
    • F04B11/0016Equalisation of pulses, e.g. by use of air vessels; Counteracting cavitation using accumulators with a fluid spring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B17/00Pumps characterised by combination with, or adaptation to, specific driving engines or motors
    • F04B17/03Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B53/00Component parts, details or accessories not provided for in, or of interest apart from, groups F04B1/00 - F04B23/00 or F04B39/00 - F04B47/00
    • F04B53/16Casings; Cylinders; Cylinder liners or heads; Fluid connections
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/80Fuel injection apparatus manufacture, repair or assembly
    • F02M2200/8023Fuel injection apparatus manufacture, repair or assembly the assembly involving use of quick-acting mechanisms, e.g. clips
    • 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
    • F02M2200/00Details of fuel-injection apparatus, not otherwise provided for
    • F02M2200/80Fuel injection apparatus manufacture, repair or assembly
    • F02M2200/8084Fuel injection apparatus manufacture, repair or assembly involving welding or soldering
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B23/00Pumping installations or systems
    • F04B23/04Combinations of two or more pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B9/00Piston machines or pumps characterised by the driving or driven means to or from their working members
    • F04B9/02Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical
    • F04B9/04Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical the means being cams, eccentrics or pin-and-slot mechanisms
    • F04B9/042Piston machines or pumps characterised by the driving or driven means to or from their working members the means being mechanical the means being cams, eccentrics or pin-and-slot mechanisms the means being cams

Definitions

  • the invention relates to a high-pressure fuel pump according to the preamble of claim 1.
  • DE 102015219 537 A1 describes a high-pressure fuel pump that is used in a fuel system of an internal combustion engine. With it, the fuel is compressed to a very high pressure in order to then be injected directly into the combustion chambers of the internal combustion engine by means of injectors.
  • the known high-pressure fuel pump is a piston pump, the delivery rate of which can be influenced by a quantity control valve on the inlet side. This results in pressure pulsations in a low-pressure area on the inlet side, which are reduced by a pressure pulsation damper arranged there.
  • This comprises a diaphragm box with, for example, two diaphragms which are essentially arranged approximately parallel to one another and which are welded to one another at the edges. The diaphragm box is clamped between a retaining ring and a spring in a receiving space of a pump housing.
  • the high-pressure fuel pump according to the invention comprises a low-pressure area and a pressure pulsation damper arranged in the low-pressure area.
  • the term “low pressure area” refers to an inlet-side area before the fuel is compressed.
  • the pressure pulsation damper comprises at least one diaphragm box and is in a receiving space is arranged, which is limited, for example, by a housing cover of the high-pressure fuel pump.
  • the diaphragm can preferably has two membranes, which can be arranged in mirror image to one another, for example, and between which an interior space of the pressure pulsation damper is formed, which is delimited by these membranes.
  • the interior can be filled, for example, with a compressible gaseous fluid (for example air or nitrogen), so that under certain external conditions a certain pressure prevails in the interior.
  • a holding device for holding the diaphragm can in the receiving space.
  • this comprises a connecting section which is firmly connected to the pump housing both in the axial and in the radial direction, in particular on an inner circumferential surface that delimits the receiving space, in both the axial and the radial direction.
  • the previously existing retaining ring and the previously existing spring are thus dispensed with.
  • the diaphragm box is fastened to the pump housing both in the axial and in the radial direction via the holding device and its connecting section. In the present case, one can speak of an axial and a radial direction, since the diaphragm box is usually a part that is at least partially and at least essentially rotationally symmetrical.
  • the previous components of the retaining ring and spring can be dispensed with, which saves costs and reduces the necessary axial extension (overall height).
  • the spring variance is also eliminated, and the costs are further reduced by the possible omission of further interface components. Since a spring no longer has to be supported, for example, on a housing cover delimiting the receiving space, the relevant specification is omitted, so that the cover can also be of a simpler design and thus less expensive. The same applies to the design of a housing surface on which the retaining ring previously had to be supported.
  • the connecting section be fixed on the inner lateral surface in a press fit and / or with the inner one Shell surface is welded.
  • the two membranes are welded to one another in the area of a radially outer edge by means of a weld line extending in the circumferential direction, and that the holding device has at least two clamping sections between which the two membranes are clamped in an area radially inward from the weld line are.
  • At least one of the clamping sections is designed in one piece with the connecting section. This reduces the number of parts to be handled, which simplifies assembly and ultimately saves costs again.
  • clamping sections are welded to one another. In this way, a very stable unit is created.
  • clamping sections are clipped together. This can be implemented inexpensively.
  • the connecting section is integrally formed on the diaphragm box. In this way, a particularly stable and easy-to-assemble unit is created.
  • the two membranes are welded to one another in the area of an edge of at least one of the two membranes by means of a weld line extending in the circumferential direction, with an area being present between the weld line and an interior space formed between the two membranes in which the both membranes rest against one another at least in sections with frictional engagement.
  • the discharge The welding line with regard to the movements of the membranes is not achieved here by a radially inward clamping, but by a "radially" inward frictional connection between the two membranes from the welding line. In this way, the relative movements of the two membranes are at least substantially kept away from the welding line during operation.
  • a fold be present between the weld line and the interior space formed between the two membranes.
  • a “bend” is understood to mean that the two membranes are bent, that is to say that a type of common collar-like section extending in the axial direction is formed.
  • the fold is preferably approximately 90 ° and takes place with a radius, the radius of the inner membrane in the area of the fold being smaller than the radius of the outer membrane in the area of the fold.
  • Such a fold also reduces the bending loads acting on the welding line during operation.
  • FIG. 1 shows a schematic representation of a fuel system of an internal combustion engine with a high-pressure fuel pump
  • FIG. 2 shows a partial longitudinal section through a region of the high-pressure fuel pump from FIG. 1 in a first embodiment
  • FIG. 3 shows a detail III from FIG. 2;
  • FIG. 4 shows a representation similar to FIG. 3 for a high-pressure fuel pump in a second embodiment
  • FIG. 5 shows a region of the high-pressure fuel pump from FIG. 4 in a modified embodiment
  • FIG. 6 shows a representation similar to FIG. 5 for a further modified embodiment.
  • a fuel system bears the overall reference number 10. It is used to provide fuel for an internal combustion engine, not shown further, in a very simplified schematic representation.
  • a quantity control valve 24 which can be actuated by an electromagnetic actuator 22, to a working chamber 26 of a high-pressure fuel pump 28, for example with one provided by the pre-feed pump 16 Pre-pressure of 4-8 bar, especially about 6 bar.
  • the quantity control valve 24 can be a positively openable inlet valve of the high-pressure fuel pump 28.
  • a piston 30 of the high-pressure fuel pump 28 can be moved vertically by means of a cam disk 32 in the drawing.
  • An outlet valve 36 shown as a spring-loaded check valve, and a pressure-limiting valve 38, also shown as a spring-loaded check valve, are arranged hydraulically between the working chamber 26 and an outlet 34 of the high-pressure fuel pump 28.
  • the outlet 34 is connected to a high pressure accumulator 42 (“common rail”) via a high pressure line 40.
  • the prefeed pump 16 delivers fuel from the fuel tank 12 into the low-pressure line 18.
  • the quantity control valve 24 can be closed and opened as a function of a particular fuel requirement.
  • the amount conveyed to the high-pressure accumulator 42 is conveyed Fuel amount influenced. Due to the discontinuous mode of operation of the high-pressure fuel pump 28, so-called pressure pulsations occur in several sections of the fuel system 10, in particular also upstream of the working chamber 26, that is to say in a low-pressure region 43 of the high-pressure fuel pump 28 or of the fuel system 10. In order to dampen these, a pressure pulsation damper 44 is arranged there.
  • the high-pressure fuel pump 28 comprises a pump housing 46 which is essentially cylindrical or rotationally symmetrical in shape. In the upper area of the pump housing 46 in FIG. 2, it has an end face 48 on which a hood-like housing cover 50 is placed, which is connected to the pump housing 46 in a fluid-tight manner, for example welded.
  • a fluid space 52 is formed between the end face 48 and the housing cover 50 and is connected to the low-pressure region 43 via a channel 54.
  • the above-mentioned pressure pulsation damper 44 which in the present case comprises a diaphragm box 56, is arranged in the fluid space 52.
  • the fluid space 52 can also be referred to as a receiving space.
  • the diaphragm box 56 in turn comprises in the present case two diaphragms 58a and 58b which are essentially identical to one another in a central area and are arranged in mirror image, which have an essentially circular contour in plan view and are designed to be rotationally symmetrical.
  • the two membranes 58a and 58b are welded to one another in a fluid-tight manner at their radially outer edge by a weld line 60.
  • the diaphragm box 56 is held in the fluid space 52 by a holding device 62.
  • the holding device 62 will be discussed in greater detail below.
  • An interior space 64 is formed between the two membranes 58a and 58b. This is therefore limited by the two membranes 58a and 58b.
  • This interior space 64 is filled with a gas, for example nitrogen or air, specifically at a specific pressure.
  • the holding device 62 comprises a connecting section 66, which in the present case is integrally formed on the upper membrane 58a and thus on the membrane box 56.
  • the upper diaphragm 58a is designed as follows (see also FIG. 3): a working area of the diaphragm 58a is formed by a central area 68 already mentioned above, in which there are bead-like formations (without reference numerals) that run around the circumference Allow movement of diaphragm 58a in an axial direction 70. Since the membranes 58a and 58b, as mentioned above, have an essentially circular contour and are designed to be rotationally symmetrical, said axial direction 70 can be defined. To this end, a corresponding radial direction 72 results orthogonally. The above-mentioned function of damping pressure pulsations is achieved by the aforementioned movement of the central area 68 of the diaphragm 58a and the corresponding central area (without reference symbols) of the diaphragm 58b.
  • the membrane 58a Radially outside of the central region 68, the membrane 58a has a flat first section 74 extending radially outward in the circumferential direction.
  • a bend 76 is provided on its radially outer edge, by means of which the membrane 58a is bent downward by 90 ° in the present example.
  • the bend 76 has a radius R.
  • From the bend 76 extends downward in the axial direction in the circumferential direction, a second section 78 in the manner of a cylindrical collar.
  • a third section 80 running around in the circumferential direction is integrally formed thereon, specifically at an angle of, for example, approximately 45 ° to the outside obliquely.
  • In the third section 80 there is a plurality of openings 82, evenly distributed in the circumferential direction, through which fuel can flow during operation.
  • a fourth section 84 is formed, for example in the circumferential direction, which extends straight in the axial direction 70 and downwards in FIG. 3 and is in this respect also designed in the manner
  • the diaphragm 58b has, radially outside of its central region 68, a flat first section 86 which likewise extends radially outward and runs in the circumferential direction. At its radially outer edge there is a bend 88 by means of which the membrane 58b is bent downward by 90 ° in the present example.
  • the fold 88 has a radius r.
  • a second section 90 extending in the circumferential direction in the manner of a cylindrical collar extends axially downward from the fold 88. In this way, the second section 90 of the diaphragm 58b forms a radially inner section and the second section 78 of the diaphragm 58a forms a radially outer section.
  • the second section 90 of the membrane 58b extends less far in the axial direction 70 than the second section 78 of the membrane 58a. At the protruding free edge of the second section 90 of the membrane 58b, the latter is welded to the second section 78 of the membrane 58a by the welding line 60 already mentioned above.
  • the second and radially inner section 90 of the diaphragm 58b is received in a press fit in the second and radially outer section 78 of the diaphragm 58a.
  • the fold 76 and the fold 88 as well as the first section 74 and the first section 86 are joined together in such a way that they rest against one another in a frictionally engaged manner. In this way it is achieved that the movement of the central regions 68 of the two membranes 58a and 58b is at least substantially kept away from the weld line 60.
  • the fourth section 84 of the membrane 58a is fixed on an inner lateral surface 92 of the housing cover 50 in a press fit. In an embodiment not shown, it is additionally or alternatively welded to the inner jacket surface.
  • the connecting section 66 of the holding device 62 formed in the present case in particular by the bend 76, the second section 78, the third section 80 and the fourth section 84, is connected to the housing cover 50 and to that extent to the pump housing 46 both in the axial direction 70 and also firmly connected in the radial direction 72.
  • the diaphragm can 56 is thus held immovably and cannot be lost in the housing cover 50.
  • FIG. 4 An alternative embodiment of a holding device 62 will now be explained with reference to FIG. 4: in this embodiment, the two membranes 58a and 58b are identical to one another, and the weld line 60 is on the protruding edge of the first section 74 of the membrane 58a and of the second section 86 of the Membrane 58b is present.
  • the holding device 62 has two resilient clamping sections 94 and 96 which are prestressed towards one another, between which the first section 74 of the membrane 58a and the first section 86 of the membrane 58b are clamped.
  • the two diaphragms 58a and 58b are clamped in a region radially inward from the weld line 60.
  • the lower clamping section 96 in FIG. 4 is fastened to the second section 78 in a manner not shown in detail in FIG.
  • the fastening of the lower clamping section 96 to the second section 78 can, as can be seen from FIG. 5, be achieved via a snap-in clip connection.
  • openings 98 are provided in the second section 78, into which resilient latching lugs 100 of the lower clamping section 96 can engage.
  • the lower clamping section 96 can also simply be welded to the second section 78 (weld line 102). In both cases it must be ensured that the two clamping sections 94 and 96 are axially pretensioned relative to one another, so that a sufficiently strong clamping force is exerted on the first sections 74 and 86 of the membranes 58a and 58b.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Reciprocating Pumps (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The invention relates to a high-pressure fuel pump (28) comprises a pump housing (46), a receiving space (52) in the pump housing (46), a pressure pulsation damper (44) in the form of a diaphragm cell (56) having two diaphragms (58a, 58b), which pressure pulsation damper is arranged in the receiving space (52), and a holding device (62) for holding the diaphragm cell (56) in the receiving space (52). According to the invention, the holding device (62) comprises a connection portion (66), which is connected to the pump housing (46) rigidly both in the axial direction (70) and in the radial direction (72), in particular is fastened, both in the axial direction (70) and in the radial direction (72), to an inner lateral surface (92) that delimits the receiving space (52).

Description

Beschreibung description
Titel title
Kraftstoff-Hochdruckpumpe High pressure fuel pump
Stand der Technik State of the art
Die Erfindung betrifft eine Kraftstoff-Hochdruckpumpe nach dem Oberbegriff des Anspruchs 1. The invention relates to a high-pressure fuel pump according to the preamble of claim 1.
Die DE 102015219 537 A1 beschreibt eine Kraftstoff-Hochdruckpumpe, die in einem Kraftstoffsystem einer Brennkraftmaschine eingesetzt wird. Mit ihr wird der Kraftstoff auf einen sehr hohen Druck verdichtet, um dann mittels Injektoren direkt in die Brennräume der Brennkraftmaschine eingespritzt zu werden. Die bekannte Kraftstoff-Hochdruckpumpe ist eine Kolbenpumpe, deren Fördermenge durch ein einlassseitiges Mengensteuerventil beeinflusst werden kann. Hierdurch entstehen in einem einlassseitigen Niederdruckbereich Druckpulsationen, die durch einen dort angeordneten Druckpulsationsdämpfer reduziert werden. Dieser umfasst eine Membrandose mit beispielsweise zwei im Wesentlichen in etwa parallel zueinander angeordneten Membranen, die randseitig miteinander verschweißt sind. In einem Aufnahmeraum eines Pumpengehäuses wird die Membrandose zwischen einem Haltering und einer Feder verklemmt. DE 102015219 537 A1 describes a high-pressure fuel pump that is used in a fuel system of an internal combustion engine. With it, the fuel is compressed to a very high pressure in order to then be injected directly into the combustion chambers of the internal combustion engine by means of injectors. The known high-pressure fuel pump is a piston pump, the delivery rate of which can be influenced by a quantity control valve on the inlet side. This results in pressure pulsations in a low-pressure area on the inlet side, which are reduced by a pressure pulsation damper arranged there. This comprises a diaphragm box with, for example, two diaphragms which are essentially arranged approximately parallel to one another and which are welded to one another at the edges. The diaphragm box is clamped between a retaining ring and a spring in a receiving space of a pump housing.
Offenbarung der Erfindung Disclosure of the invention
Das der vorliegenden Erfindung zu Grunde liegende Problem wird durch eine Kraftstoff-Hochdruckpumpe mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung sind in Unteransprüchen angegeben. The problem on which the present invention is based is solved by a high-pressure fuel pump having the features of claim 1. Advantageous further developments of the invention are specified in the subclaims.
Die erfindungsgemäße Kraftstoff-Hochdruckpumpe umfasst einen Niederdruckbereich und einen in dem Niederdruckbereich angeordneten Druckpulsationsdämpfer. Der Begriff „Niederdruckbereich“ ist auf einen einlassseitigen Bereich vor der Verdichtung des Kraftstoffs bezogen. Der Druckpulsationsdämpfer umfasst mindestens eine Membrandose und ist in einem Aufnahmeraum angeordnet ist, der beispielsweise von einem Gehäusedeckel der Kraftstoff-Hochdruckpumpe begrenzt wird. The high-pressure fuel pump according to the invention comprises a low-pressure area and a pressure pulsation damper arranged in the low-pressure area. The term “low pressure area” refers to an inlet-side area before the fuel is compressed. The pressure pulsation damper comprises at least one diaphragm box and is in a receiving space is arranged, which is limited, for example, by a housing cover of the high-pressure fuel pump.
Die Membrandose weist vorzugsweise zwei Membranen auf, die beispielsweise spiegelbildlich zueinander angeordnet sein können und zwischen denen ein Innenraum des Druckpulsationsdämpfers gebildet ist, der durch diese Membranen begrenzt wird. Der Innenraum kann beispielsweise mit einem kompressiblen gasförmigen Fluid (beispielsweise Luft oder Stickstoff) gefüllt sein, so dass bei bestimmten Außenbedingungen ein bestimmter Druck in dem Innenraum herrscht. The diaphragm can preferably has two membranes, which can be arranged in mirror image to one another, for example, and between which an interior space of the pressure pulsation damper is formed, which is delimited by these membranes. The interior can be filled, for example, with a compressible gaseous fluid (for example air or nitrogen), so that under certain external conditions a certain pressure prevails in the interior.
Zum Haltern der Membrandose in dem Aufnahmeraum ist eine Halteeinrichtung vorgesehen. Diese umfasst erfindungsgemäß einen Verbindungsabschnitt, der mit dem Pumpengehäuse sowohl in axialer als auch in radialer Richtung fest verbunden ist, insbesondere an einer inneren Mantelfläche, die den Aufnahmeraum begrenzt, sowohl in axialer als auch in radialer Richtung befestigt ist. Bei der erfindungsgemäßen Kraftstoff-Hochdruckpumpe wird also auf den bisher vorhandenen Haltering und die bisher vorhandene Feder verzichtet. Stattdessen ist die Membrandose über die Halteeinrichtung und deren Verbindungsabschnitt sowohl in axialer als auch in radialer Richtung am Pumpengehäuse befestigt. Dabei kann vorliegend von einer axialer und einer radialen Richtung gesprochen werden, da es sich bei der Membrandose üblicherweise um ein wenigstens abschnittsweise und wenigstens im wesentlichen rotationssymmetrisches Teil handelt. A holding device is provided for holding the diaphragm can in the receiving space. According to the invention, this comprises a connecting section which is firmly connected to the pump housing both in the axial and in the radial direction, in particular on an inner circumferential surface that delimits the receiving space, in both the axial and the radial direction. In the high-pressure fuel pump according to the invention, the previously existing retaining ring and the previously existing spring are thus dispensed with. Instead, the diaphragm box is fastened to the pump housing both in the axial and in the radial direction via the holding device and its connecting section. In the present case, one can speak of an axial and a radial direction, since the diaphragm box is usually a part that is at least partially and at least essentially rotationally symmetrical.
Aufgrund der Erfindung kann auf die bisherigen Bauteile Haltering und Feder verzichtet werden, wodurch Kosten gespart und die notwendige axiale Erstreckung (Bauhöhe) reduziert wird. Auch wird die Federvarianz eliminiert, und die Kosten werden durch den möglichen Entfall weiterer Schnittstellenkomponenten weiter reduziert. Da sich keine Feder mehr beispielsweise an einem den Aufnahmeraum begrenzenden Gehäusedeckel abstützen muss, entfällt die diesbezügliche Spezifikation, so dass auch der Deckel einfacher ausgebildet und somit preiswerter sein kann. Ähnliches gilt für die Ausgestaltung einer Gehäusefläche, an der sich bisher der Haltering abstützen musste. Due to the invention, the previous components of the retaining ring and spring can be dispensed with, which saves costs and reduces the necessary axial extension (overall height). The spring variance is also eliminated, and the costs are further reduced by the possible omission of further interface components. Since a spring no longer has to be supported, for example, on a housing cover delimiting the receiving space, the relevant specification is omitted, so that the cover can also be of a simpler design and thus less expensive. The same applies to the design of a housing surface on which the retaining ring previously had to be supported.
Bei einer Weiterbildung wird vorgeschlagen, dass der Verbindungsabschnitt an der inneren Mantelfläche im Presssitz festgelegt und/oder mit der inneren Mantelfläche verschweißt ist. Dies sind besonders einfache und zuverlässige sowie dauerfeste Verbindungsarten. Handelt es sich um die innere Mantelfläche eines Gehäusedeckels, kann die Membrandose auf einfache Weise im Gehäusedeckel vormontiert werden, wodurch nochmals Kosten gespart werden. In a further development, it is proposed that the connecting section be fixed on the inner lateral surface in a press fit and / or with the inner one Shell surface is welded. These are particularly simple, reliable and durable types of connection. In the case of the inner jacket surface of a housing cover, the diaphragm box can be preassembled in a simple manner in the housing cover, which further saves costs.
Bei einer Weiterbildung wird vorgeschlagen, dass die beiden Membranen im Bereich eines radial äußeren Randes miteinander mittels einer sich in Umfangsrichtung erstreckenden Schweißlinie verschweißt sind, und dass die Halteeinrichtung mindestens zwei Klemmabschnitte aufweist, zwischen denen die beiden Membranen in einem von der Schweißlinie radial einwärtigen Bereich verklemmt sind. Hierdurch wird die Schweißlinie entlastet und damit die Dauerfestigkeit der Membrandose verbessert. Die Entlastung basiert darauf, dass die Bewegungen der Membranen von der Schweißlinie ferngehalten oder zumindest reduziert werden, so dass die Biegebeanspruchung der Schweißverbindung reduziert wird. In a further development, it is proposed that the two membranes are welded to one another in the area of a radially outer edge by means of a weld line extending in the circumferential direction, and that the holding device has at least two clamping sections between which the two membranes are clamped in an area radially inward from the weld line are. This relieves the welding line and improves the fatigue strength of the diaphragm can. The relief is based on the fact that the movements of the membranes are kept away from the weld line or at least reduced, so that the bending stress on the welded connection is reduced.
Bei einer Weiterbildung wird vorgeschlagen, dass mindestens einer der Klemmabschnitte mit dem Verbindungsabschnitt einstückig ausgebildet ist. Dies reduziert die Anzahl der handzuhabenden Teile, wodurch die Montage vereinfacht und letztlich nochmals Kosten gespart werden. In a further development, it is proposed that at least one of the clamping sections is designed in one piece with the connecting section. This reduces the number of parts to be handled, which simplifies assembly and ultimately saves costs again.
Bei einer Weiterbildung wird vorgeschlagen, dass die Klemmabschnitte miteinander verschweißt sind. Auf diese Weise wird eine sehr dauerstabile Einheit geschaffen. In a further development, it is proposed that the clamping sections are welded to one another. In this way, a very stable unit is created.
Bei einer Weiterbildung wird vorgeschlagen, dass die Klemmabschnitte miteinander verclipst sind. Dies ist preiswert realisierbar. In a further development it is proposed that the clamping sections are clipped together. This can be implemented inexpensively.
Bei einer Weiterbildung wird vorgeschlagen, dass der Verbindungsabschnitt an die Membrandose einstückig angeformt ist. Auf diese Weise wird eine besonders stabile und einfach zu montierende Einheit geschaffen. In a further development, it is proposed that the connecting section is integrally formed on the diaphragm box. In this way, a particularly stable and easy-to-assemble unit is created.
Bei einer Weiterbildung wird vorgeschlagen, dass die beiden Membranen im Bereich eines Randes mindestens einer der beiden Membranen mittels einer sich in Umfangsrichtung erstreckenden Schweißlinie miteinander verschweißt sind, wobei zwischen der Schweißlinie und einem zwischen den beiden Membranen gebildeten Innenraum ein Bereich vorhanden ist, in dem die beiden Membranen wenigstens abschnittsweise reibschlüssig aneinander anliegen. Die Entlastung der Schweißlinie im Hinblick auf die Bewegungen der Membranen wird hier nicht durch eine radial einwärtigen Klemmung erreicht, sondern durch einen „radial“ einwärtigen von der Schweißlinie vorhandenen Reibschluss zwischen den beiden Membranen. Auf diese Weise werden die Relativbewegungen der beiden Membranen im Betrieb von der Schweißlinie wenigstens im Wesentlichen ferngehalten. In a further development, it is proposed that the two membranes are welded to one another in the area of an edge of at least one of the two membranes by means of a weld line extending in the circumferential direction, with an area being present between the weld line and an interior space formed between the two membranes in which the both membranes rest against one another at least in sections with frictional engagement. The discharge The welding line with regard to the movements of the membranes is not achieved here by a radially inward clamping, but by a "radially" inward frictional connection between the two membranes from the welding line. In this way, the relative movements of the two membranes are at least substantially kept away from the welding line during operation.
Bei einer Weiterbildung wird vorgeschlagen, dass zwischen der Schweißlinie und dem zwischen den beiden Membranen gebildeten Innenraum ein Umbug vorhanden ist. Unter einem solchen „Umbug“ wird verstanden, dass die beiden Membranen umgebogen sind, also eine Art eines gemeinsamen kragenartigen und sich in axialer Richtung erstreckenden Abschnitts gebildet wird. Der Umbug beträgt dabei vorzugsweise ungefähr 90° und erfolgt mit einem Radius, wobei der Radius der im Bereich des Umbugs inneren Membran kleiner ist als der Radius der im Bereich des Umbugs äußeren Membran. Ein solcher Umbug reduziert ebenfalls im Betrieb auf die Schweißlinie einwirkenden Biegebelastungen. In a further development, it is proposed that a fold be present between the weld line and the interior space formed between the two membranes. Such a “bend” is understood to mean that the two membranes are bent, that is to say that a type of common collar-like section extending in the axial direction is formed. The fold is preferably approximately 90 ° and takes place with a radius, the radius of the inner membrane in the area of the fold being smaller than the radius of the outer membrane in the area of the fold. Such a fold also reduces the bending loads acting on the welding line during operation.
Bei einer Weiterbildung wird vorgeschlagen, dass im Bereich des Umbugs ein radial innerer Abschnitt der einen Membran in einem radial äußeren Abschnitt der anderen Membran im Presssitz aufgenommen ist. Es wird also eine zusätzliche zylindrische Presspassung zwischen den beiden Membranen geschaffen, durch die ein starker Reibschluss zwischen den beiden Membranen erreicht wird, der Relativbewegungen der beiden Membranen zuverlässig von der Schweißlinie fernhält. In a further development, it is proposed that, in the area of the fold, a radially inner section of one membrane is received in a press fit in a radially outer section of the other membrane. An additional cylindrical interference fit is thus created between the two membranes, by means of which a strong frictional connection is achieved between the two membranes, which reliably keeps the relative movements of the two membranes away from the weld line.
Nachfolgend wird eine Ausführungsform der Erfindung unter Bezugnahme auf die Zeichnung erläutert. In der Zeichnung zeigen: An embodiment of the invention is explained below with reference to the drawing. In the drawing show:
Figur 1 eine schematische Darstellung eines Kraftstoffsystems einer Brennkraftmaschine mit einer Kraftstoff-Hochdruckpumpe; FIG. 1 shows a schematic representation of a fuel system of an internal combustion engine with a high-pressure fuel pump;
Figur 2 einen teilweisen Längsschnitt durch einen Bereich der Kraftstoff- Hochdruckpumpe von Figur 1 in einer ersten Ausführungsform; FIG. 2 shows a partial longitudinal section through a region of the high-pressure fuel pump from FIG. 1 in a first embodiment;
Figur 3 ein Detail III von Figur 2; Figur 4 eine Darstellung ähnlich zu Figur 3 für eine Kraftstoff-Hochdruckpumpe in einer zweiten Ausführungsform; FIG. 3 shows a detail III from FIG. 2; FIG. 4 shows a representation similar to FIG. 3 for a high-pressure fuel pump in a second embodiment;
Figur 5 einen Bereich der Kraftstoff-Hochdruckpumpe von Figur 4 in einer abgewandelten Ausführungsform; und FIG. 5 shows a region of the high-pressure fuel pump from FIG. 4 in a modified embodiment; and
Figur 6 eine Darstellung ähnlich zu Figur 5 für eine nochmals abgewandelte Ausführungsform. FIG. 6 shows a representation similar to FIG. 5 for a further modified embodiment.
Nachfolgend tragen funktionsäquivalente Elemente und Bereiche auch in unterschiedlichen Ausführungsformen die gleichen Bezugszeichen. In the following, functionally equivalent elements and areas also have the same reference symbols in different embodiments.
In Figur 1 trägt ein Kraftstoff System insgesamt das Bezugszeichen 10. Es dient zur Bereitstellung von Kraftstoff für eine weiter nicht dargestellte Brennkraftmaschine in einer sehr vereinfachten schematischen Darstellung. In FIG. 1, a fuel system bears the overall reference number 10. It is used to provide fuel for an internal combustion engine, not shown further, in a very simplified schematic representation.
Aus einem Kraftstofftank 12 wird Kraftstoff über eine Saugleitung 14, eine meist elektrische Vorförderpumpe 16, eine Niederdruckleitung 18 einem Einlass 20 eines von einer elektromagnetischen Betätigungseinrichtung 22 betätigbaren Mengensteuerventils 24 einem Arbeitsraum 26 einer Kraftstoff-Hochdruckpumpe 28 zugeführt, beispielsweise mit einem von der Vorförderpumpe 16 bereitgestellten Vordruck von 4-8 bar, insbesondere ungefähr 6 bar. Beispielsweise kann das Mengensteuerventil 24 ein zwangsweise öffenbares Einlassventil der Kraftstoff-Hochdruckpumpe 28 sein. From a fuel tank 12, fuel is fed via a suction line 14, a mostly electric pre-feed pump 16, a low-pressure line 18 to an inlet 20 of a quantity control valve 24, which can be actuated by an electromagnetic actuator 22, to a working chamber 26 of a high-pressure fuel pump 28, for example with one provided by the pre-feed pump 16 Pre-pressure of 4-8 bar, especially about 6 bar. For example, the quantity control valve 24 can be a positively openable inlet valve of the high-pressure fuel pump 28.
Ein Kolben 30 der Kraftstoff-Hochdruckpumpe 28 kann mittels einer Nockenscheibe 32 in der Zeichnung vertikal bewegt werden. Hydraulisch zwischen dem Arbeitsraum 26 und einem Auslass 34 der Kraftstoff- Hochdruckpumpe 28 sind ein als federbelastetes Rückschlagventil gezeichnetes Auslassventil 36 sowie ein ebenfalls als federbelastetes Rückschlagventil gezeichnetes Druckbegrenzungsventil 38 angeordnet. Der Auslass 34 ist über eine Hochdruckleitung 40 an einen Hochdruckspeicher 42 („common Rail“) angeschlossen. A piston 30 of the high-pressure fuel pump 28 can be moved vertically by means of a cam disk 32 in the drawing. An outlet valve 36, shown as a spring-loaded check valve, and a pressure-limiting valve 38, also shown as a spring-loaded check valve, are arranged hydraulically between the working chamber 26 and an outlet 34 of the high-pressure fuel pump 28. The outlet 34 is connected to a high pressure accumulator 42 (“common rail”) via a high pressure line 40.
Im Betrieb des Kraftstoff Systems 10 fördert die Vorförderpumpe 16 Kraftstoff vom Kraftstofftank 12 in die Niederdruckleitung 18. Das Mengensteuerventil 24 kann in Abhängigkeit von einem jeweiligen Bedarf an Kraftstoff geschlossen und geöffnet werden. Hierdurch wird die zu dem Hochdruckspeicher 42 geförderte Kraftstoffmenge beeinflusst. Bedingt durch die diskontinuierliche Arbeitsweise der Kraftstoff-Hochdruckpumpe 28 treten an mehreren Abschnitten des Kraftstoffsystems 10 sogenannte Druckpulsationen auf, insbesondere auch stromaufwärts von dem Arbeitsraum 26, also in einem Niederdruckbereich 43 der Kraftstoff-Hochdruckpumpe 28 bzw. des Kraftstoffsystems 10. Um diese zu dämpfen, ist dort ein Druckpulsationsdämpfer 44 angeordnet. When the fuel system 10 is in operation, the prefeed pump 16 delivers fuel from the fuel tank 12 into the low-pressure line 18. The quantity control valve 24 can be closed and opened as a function of a particular fuel requirement. As a result, the amount conveyed to the high-pressure accumulator 42 is conveyed Fuel amount influenced. Due to the discontinuous mode of operation of the high-pressure fuel pump 28, so-called pressure pulsations occur in several sections of the fuel system 10, in particular also upstream of the working chamber 26, that is to say in a low-pressure region 43 of the high-pressure fuel pump 28 or of the fuel system 10. In order to dampen these, a pressure pulsation damper 44 is arranged there.
Wie aus Figur 2 ersichtlich ist, umfasst die Kraftstoff-Hochdruckpumpe 28 ein Pumpengehäuse 46, welches im wesentlichen zylindrische bzw. rotationssymmetrische Form hat. Im in Figur 2 oberen Bereich des Pumpengehäuses 46 hat dieses eine Stirnseite 48, auf die ein haubenartiger Gehäusedeckel 50 aufgesetzt ist, der mit dem Pumpengehäuse 46 fluiddicht verbunden, beispielsweise verschweißt ist. Zwischen der Stirnseite 48 und dem Gehäusedeckel 50 wird ein Fluidraum 52 gebildet, der über einen Kanal 54 mit dem Niederdruckbereich 43 verbunden ist. In dem Fluidraum 52 ist der bereits oben erwähnte Druckpulsationsdämpfer 44 angeordnet, der vorliegend eine Membrandose 56 umfasst. Insoweit kann der Fluidraum 52 auch als Aufnahmeraum bezeichnet werden. As can be seen from FIG. 2, the high-pressure fuel pump 28 comprises a pump housing 46 which is essentially cylindrical or rotationally symmetrical in shape. In the upper area of the pump housing 46 in FIG. 2, it has an end face 48 on which a hood-like housing cover 50 is placed, which is connected to the pump housing 46 in a fluid-tight manner, for example welded. A fluid space 52 is formed between the end face 48 and the housing cover 50 and is connected to the low-pressure region 43 via a channel 54. The above-mentioned pressure pulsation damper 44, which in the present case comprises a diaphragm box 56, is arranged in the fluid space 52. In this respect, the fluid space 52 can also be referred to as a receiving space.
Die Membrandose 56 wiederum umfasst vorliegend zwei zueinander in einem mittigen Bereich im Wesentlichen identische und spiegelbildlich angeordnete Membranen 58a und 58b, die in der Draufsicht eine im wesentlichen kreisförmige Kontur aufweisen und rotationssymmetrisch ausgebildet sind. Die beiden Membranen 58a und 58b sind, wie aus Figur 3 hervorgeht, an ihrem radial äußeren Rand miteinander fluiddicht durch eine Schweißlinie 60 verschweißt. Die Membrandose 56 ist in dem Fluidraum 52 durch eine Halteeinrichtung 62 gehalten. Auf die Halteeinrichtung 62 wird weiter unten noch stärker in Detail eingegangen werden. Zwischen den beiden Membranen 58a und 58b ist ein Innenraum 64 gebildet. Dieser wird also durch die beiden Membranen 58a und 58b begrenzt. Dieser Innenraum 64 ist mit einem Gas, beispielsweise Stickstoff oder Luft, befüllt, und zwar mit einem spezifischen Druck. The diaphragm box 56 in turn comprises in the present case two diaphragms 58a and 58b which are essentially identical to one another in a central area and are arranged in mirror image, which have an essentially circular contour in plan view and are designed to be rotationally symmetrical. As can be seen from FIG. 3, the two membranes 58a and 58b are welded to one another in a fluid-tight manner at their radially outer edge by a weld line 60. The diaphragm box 56 is held in the fluid space 52 by a holding device 62. The holding device 62 will be discussed in greater detail below. An interior space 64 is formed between the two membranes 58a and 58b. This is therefore limited by the two membranes 58a and 58b. This interior space 64 is filled with a gas, for example nitrogen or air, specifically at a specific pressure.
Die Halteeinrichtung 62 umfasst einen Verbindungsabschnitt 66, der vorliegend einstückig an die obere Membran 58a und somit an die Membrandose 56 angeformt ist. Hierzu ist die obere Membran 58a wie folgt ausgebildet (siehe auch Figur 3): ein Arbeitsbereich der Membran 58a wird durch einen bereits oben erwähnten mittigen Bereich 68 gebildet, in dem in Umfangsrichtung umlaufende sickenartige Ausformungen (ohne Bezugszeichen) vorhanden sind, die eine Bewegung der Membran 58a in einer axialen Richtung 70 ermöglichen. Da die Membranen 58a und 58b, wie oben erwähnt, im wesentlichen kreisförmige Kontur aufweisen und rotationssymmetrisch ausgebildet sind, kann die besagte axiale Richtung 70 definiert werden. Hierzu orthogonal ergibt sich eine entsprechende radiale Richtung 72. Durch die erwähnte Bewegung des mittigen Bereichs 68 der Membran 58a und des entsprechenden mittigen Bereichs (ohne Bezugszeichen) der Membran 58b wird die oben erwähnte Funktion der Dämpfung von Druckpulsationen erreicht. The holding device 62 comprises a connecting section 66, which in the present case is integrally formed on the upper membrane 58a and thus on the membrane box 56. For this purpose, the upper diaphragm 58a is designed as follows (see also FIG. 3): a working area of the diaphragm 58a is formed by a central area 68 already mentioned above, in which there are bead-like formations (without reference numerals) that run around the circumference Allow movement of diaphragm 58a in an axial direction 70. Since the membranes 58a and 58b, as mentioned above, have an essentially circular contour and are designed to be rotationally symmetrical, said axial direction 70 can be defined. To this end, a corresponding radial direction 72 results orthogonally. The above-mentioned function of damping pressure pulsations is achieved by the aforementioned movement of the central area 68 of the diaphragm 58a and the corresponding central area (without reference symbols) of the diaphragm 58b.
Radial außerhalb von dem mittigen Bereich 68 weist die Membran 58a einen sich nach radial außen erstreckenden in Umfangsrichtung umlaufenden flachen ersten Abschnitt 74 auf. An dessen radial äußerem Rand ist ein Umbug 76 vorhanden, durch den die Membran 58a um vorliegend beispielhaft 90° nach unten umgebogen wird. Der Umbug 76 hat einen Radius R. Von dem Umbug 76 erstreckt sich in axialer Richtung nach unten ein in Umfangsrichtung umlaufender zweiter Abschnitt 78 in der Art eines zylindrischen Kragens. An diesen ist ein in Umfangsrichtung umlaufender dritter Abschnitt 80 angeformt, und zwar in einem Winkel von vorliegend beispielhaft ungefähr 45° nach schräg außen. In dem dritten Abschnitt 80 ist in Umfangsrichtung gleichmäßig verteilt eine Mehrzahl von Öffnungen 82 vorhanden, durch die im Betrieb Kraftstoff strömen kann. An den dritten Abschnitt 80 ist wiederum ein vorliegend beispielhaft in Umfangsrichtung umlaufender vierter Abschnitt 84 angeformt, der sich in axialer Richtung 70 gerade und in Figur 3 nach unten erstreckt und insoweit ebenfalls in der Art eines zylindrischen Kragens ausgebildet ist. Radially outside of the central region 68, the membrane 58a has a flat first section 74 extending radially outward in the circumferential direction. A bend 76 is provided on its radially outer edge, by means of which the membrane 58a is bent downward by 90 ° in the present example. The bend 76 has a radius R. From the bend 76 extends downward in the axial direction in the circumferential direction, a second section 78 in the manner of a cylindrical collar. A third section 80 running around in the circumferential direction is integrally formed thereon, specifically at an angle of, for example, approximately 45 ° to the outside obliquely. In the third section 80 there is a plurality of openings 82, evenly distributed in the circumferential direction, through which fuel can flow during operation. On the third section 80 a fourth section 84 is formed, for example in the circumferential direction, which extends straight in the axial direction 70 and downwards in FIG. 3 and is in this respect also designed in the manner of a cylindrical collar.
Die Membran 58b weist radial außerhalb von deren mittigem Bereich 68 einen sich ebenfalls nach radial außen erstreckenden und in Umfangsrichtung umlaufenden flachen ersten Abschnitt 86 auf. An dessen radial äußerem Rand ist ein Umbug 88 vorhanden, durch den die Membran 58b um vorliegend beispielhaft 90° nach unten umgebogen wird. Der Umbug 88 hat einen Radius r. Von dem Umbug 88 erstreckt sich in axialer Richtung nach unten ein in Umfangsrichtung umlaufender zweiter Abschnitt 90 in der Art eines zylindrischen Kragens. Auf diese Weise bildet der zweite Abschnitt 90 der Membran 58b einen radial inneren Abschnitt und der zweite Abschnitt 78 der Membran 58a einen radial äußeren Abschnitt. Der zweite Abschnitt 90 der Membran 58b erstreckt sich in der axialen Richtung 70 jedoch weniger weit als der zweite Abschnitt 78 der Membran 58a. Am abragenden freien Rand des zweiten Abschnitts 90 der Membran 58b ist diese durch die bereits oben erwähnte Schweißlinie 60 mit dem zweiten Abschnitt 78 der Membran 58a verschweißt. Dabei ist der zweite und radial innere Abschnitt 90 der Membran 58b in dem zweiten und radial äußeren Abschnitt 78 der Membran 58a im Presssitz aufgenommen. Außerdem sind der Umbug 76 und der Umbug 88 sowie der erste Abschnitt 74 und der erste Abschnitt 86 so zusammengefügt, dass diese reibschlüssig aneinander anliegen. Auf diese Weise wird erreicht, dass die Bewegung der mittigen Bereiche 68 der beiden Membranen 58a und 58b von der Schweißlinie 60 wenigstens im Wesentlichen ferngehalten wird. The diaphragm 58b has, radially outside of its central region 68, a flat first section 86 which likewise extends radially outward and runs in the circumferential direction. At its radially outer edge there is a bend 88 by means of which the membrane 58b is bent downward by 90 ° in the present example. The fold 88 has a radius r. A second section 90 extending in the circumferential direction in the manner of a cylindrical collar extends axially downward from the fold 88. In this way, the second section 90 of the diaphragm 58b forms a radially inner section and the second section 78 of the diaphragm 58a forms a radially outer section. However, the second section 90 of the membrane 58b extends less far in the axial direction 70 than the second section 78 of the membrane 58a. At the protruding free edge of the second section 90 of the membrane 58b, the latter is welded to the second section 78 of the membrane 58a by the welding line 60 already mentioned above. The second and radially inner section 90 of the diaphragm 58b is received in a press fit in the second and radially outer section 78 of the diaphragm 58a. In addition, the fold 76 and the fold 88 as well as the first section 74 and the first section 86 are joined together in such a way that they rest against one another in a frictionally engaged manner. In this way it is achieved that the movement of the central regions 68 of the two membranes 58a and 58b is at least substantially kept away from the weld line 60.
Der vierte Abschnitt 84 der Membran 58a ist an einer inneren Mantelfläche 92 des Gehäusedeckels 50 im Presssitz festgelegt. Bei einer nicht gezeigten Ausführungsform ist er zusätzlich oder alternativ mit der inneren Mantelfläche verschweißt. Auf diese Weise ist der vorliegend insbesondere durch den Umbug 76, den zweiten Abschnitt 78, den dritten Abschnitt 80 und den vierten Abschnitt 84 gebildete Verbindungsabschnitt 66 der Halteeinrichtung 62 mit dem Gehäusedeckel 50 und insoweit mit dem Pumpengehäuse 46 sowohl in der axialen Richtung 70 als auch in der radialen Richtung 72 fest verbunden. Somit ist die Membrandose 56 in dem Gehäusedeckel 50 unverrückbar und unverlierbar gehalten. The fourth section 84 of the membrane 58a is fixed on an inner lateral surface 92 of the housing cover 50 in a press fit. In an embodiment not shown, it is additionally or alternatively welded to the inner jacket surface. In this way, the connecting section 66 of the holding device 62, formed in the present case in particular by the bend 76, the second section 78, the third section 80 and the fourth section 84, is connected to the housing cover 50 and to that extent to the pump housing 46 both in the axial direction 70 and also firmly connected in the radial direction 72. The diaphragm can 56 is thus held immovably and cannot be lost in the housing cover 50.
Eine alternative Ausführungsform einer Halteeinrichtung 62 wird nun unter Bezugnahme auf Figur 4 erläutert: bei dieser Ausführungsform sind die beiden Membranen 58a und 58b zueinander identisch ausgeführt, und die Schweißlinie 60 ist am abragenden Rand des ersten Abschnitts 74 der Membran 58a und des zweiten Abschnitts 86 der Membran 58b vorhanden. Die Halteeinrichtung 62 weist zwei federnde und zueinander hin vorgespannte Klemmabschnitte 94 und 96 auf, zwischen denen der erste Abschnitt 74 der Membran 58a und der erste Abschnitt 86 der Membran 58b verklemmt sind. Die beiden Membranen 58a und 58b sind insoweit in einem von der Schweißlinie 60 radial einwärtigen Bereich verklemmt. Der in Figur 4 obere Klemmabschnitt 94 ist an den in Figur 4 oberen Rand des zweiten Abschnitts 78 der Halteeinrichtung 62 angeformt und insoweit einstückig mit dem vorliegend vor allem durch den zweiten Abschnitt 78, den dritten Abschnitt 80 und den vierten Abschnitt 84 gebildeten Verbindungsabschnitt 66 einstückig ausgebildet. Der in Figur 4 untere Klemmabschnitt 96 ist am zweiten Abschnitt 78 auf in Figur 4 nicht näher dargestellte Art und Weise befestigt. Die Befestigung des unteren Klemmabschnitt 96 am zweiten Abschnitt 78 kann, wie aus Figur 5 ersichtlich ist, über eine einrastende Clips-Verbindung erreicht werden. Hierzu sind im zweiten Abschnitt 78 Öffnungen 98 vorhanden, in welche federnde Rastnasen 100 des unteren Klemmabschnitts 96 einrasten können.An alternative embodiment of a holding device 62 will now be explained with reference to FIG. 4: in this embodiment, the two membranes 58a and 58b are identical to one another, and the weld line 60 is on the protruding edge of the first section 74 of the membrane 58a and of the second section 86 of the Membrane 58b is present. The holding device 62 has two resilient clamping sections 94 and 96 which are prestressed towards one another, between which the first section 74 of the membrane 58a and the first section 86 of the membrane 58b are clamped. The two diaphragms 58a and 58b are clamped in a region radially inward from the weld line 60. The upper clamping section 94 in FIG. 4 is formed on the upper edge of the second section 78 of the holding device 62 in FIG. 4 and is thus one-piece with the connecting section 66 formed primarily by the second section 78, the third section 80 and the fourth section 84 educated. The lower clamping section 96 in FIG. 4 is fastened to the second section 78 in a manner not shown in detail in FIG. The fastening of the lower clamping section 96 to the second section 78 can, as can be seen from FIG. 5, be achieved via a snap-in clip connection. For this purpose, openings 98 are provided in the second section 78, into which resilient latching lugs 100 of the lower clamping section 96 can engage.
Alternativ kann der untere Klemmabschnitt 96, wie aus Figur 6 ersichtlich ist, auch einfach am zweiten Abschnitt 78 verschweißt werden (Schweißlinie 102). In beiden Fällen ist darauf zu achten, dass die beiden Klemmabschnitte 94 und 96 relativ zueinander axial vorgespannt sind, so dass eine ausreichend starke Klemmkraft auf die ersten Abschnitte 74 und 86 der Membranen 58a und 58b ausgeübt wird. Alternatively, as can be seen from FIG. 6, the lower clamping section 96 can also simply be welded to the second section 78 (weld line 102). In both cases it must be ensured that the two clamping sections 94 and 96 are axially pretensioned relative to one another, so that a sufficiently strong clamping force is exerted on the first sections 74 and 86 of the membranes 58a and 58b.

Claims

Ansprüche Expectations
1. Kraftstoff-Hochdruckpumpe (28) mit einem Pumpengehäuse (46), einem in dem Pumpengehäuse (46) vorhandenen Aufnahmeraum (52), einem in dem Aufnahmeraum (52) angeordneten Druckpulsationsdämpfer (44) in Form einer Membrandose (56) mit zwei Membranen (58a, 58b), und einer Halteeinrichtung (62) zum Haltern der Membrandose (56) in dem Aufnahmeraum (52), dadurch gekennzeichnet, dass die Halteeinrichtung (62) einen Verbindungsabschnitt (66) umfasst, der mit dem Pumpengehäuse (46) sowohl in axialer Richtung (70) als auch in radialer Richtung (72) fest verbunden ist, insbesondere an einer inneren Mantelfläche (92), die den Aufnahmeraum (52) begrenzt, sowohl in axialer Richtung (70) als auch in radialer Richtung (72) befestigt ist. 1. High-pressure fuel pump (28) with a pump housing (46), a receiving space (52) present in the pump housing (46), a pressure pulsation damper (44) arranged in the receiving space (52) in the form of a diaphragm box (56) with two diaphragms (58a, 58b), and a holding device (62) for holding the diaphragm box (56) in the receiving space (52), characterized in that the holding device (62) comprises a connecting section (66) which both with the pump housing (46) is firmly connected in the axial direction (70) and in the radial direction (72), in particular on an inner jacket surface (92) which delimits the receiving space (52), both in the axial direction (70) and in the radial direction (72) is attached.
2. Kraftstoff-Hochdruckpumpe (28) nach Anspruch 1, dadurch gekennzeichnet, dass der Verbindungsabschnitt (66) an der inneren Mantelfläche (92) im Presssitz festgelegt und/oder mit der inneren Mantelfläche (92) verschweißt ist. 2. High-pressure fuel pump (28) according to claim 1, characterized in that the connecting section (66) is fixed on the inner lateral surface (92) in a press fit and / or is welded to the inner lateral surface (92).
3. Kraftstoff-Hochdruckpumpe (28) nach wenigstens einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die beiden Membranen (58a, 58b) im Bereich eines radial äußeren Randes miteinander mittels einer sich in Umfangsrichtung erstreckenden Schweißlinie (60) verschweißt sind, und dass die Halteeinrichtung (62) mindestens zwei Klemmabschnitte (9496) aufweist, zwischen denen die beiden Membranen (58a, 58b) in einem von der Schweißlinie (60) radial einwärtigen Bereich verklemmt sind. 3. High-pressure fuel pump (28) according to at least one of the preceding claims, characterized in that the two membranes (58a, 58b) are welded to one another in the region of a radially outer edge by means of a weld line (60) extending in the circumferential direction, and that the Holding device (62) has at least two clamping sections (9496), between which the two membranes (58a, 58b) are clamped in an area radially inward from the weld line (60).
4. Kraftstoff-Hochdruckpumpe (28) nach Anspruch 3, dadurch gekennzeichnet, dass mindestens einer der Klemmabschnitte (94, 96) mit dem Verbindungsabschnitt (66) einstückig ausgebildet ist. 4. High-pressure fuel pump (28) according to claim 3, characterized in that at least one of the clamping sections (94, 96) is formed in one piece with the connecting section (66).
5. Kraftstoff-Hochdruckpumpe (28) nach wenigstens einem der Ansprüche 3 oder 4, dadurch gekennzeichnet, dass die Klemmabschnitte (94, 96) miteinander verschweißt sind (102). 5. High pressure fuel pump (28) according to at least one of claims 3 or 4, characterized in that the clamping sections (94, 96) are welded to one another (102).
6. Kraftstoff-Hochdruckpumpe (28) nach wenigstens einem der Ansprüche 3-5, dadurch gekennzeichnet, dass die Klemmabschnitte (94, 96) miteinander verclipst sind (98, 100). 6. High-pressure fuel pump (28) according to at least one of claims 3-5, characterized in that the clamping sections (94, 96) are clipped together (98, 100).
7. Kraftstoff-Hochdruckpumpe (28) nach wenigstens einem der Ansprüche 1-2, dadurch gekennzeichnet, dass der Verbindungsabschnitt (66) an die Membrandose (56) einstückig angeformt ist. 7. High-pressure fuel pump (28) according to at least one of claims 1-2, characterized in that the connecting portion (66) is integrally formed on the diaphragm box (56).
8. Kraftstoff-Hochdruckpumpe (28) nach wenigstens einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die beiden Membranen (58a, 58b) im Bereich eines Randes mindestens einer der beiden Membranen (58a, 58b) mittels einer sich in Umfangsrichtung erstreckenden Schweißlinie (60) miteinander verschweißt sind, wobei zwischen der Schweißlinie (60) und einem zwischen den beiden Membranen (58a, 58b) gebildeten Innenraum (64) ein Bereich vorhanden ist, in dem die beiden Membranen (58a, 58b) wenigstens abschnittsweise reibschlüssig aneinander anliegen. 8. High-pressure fuel pump (28) according to at least one of the preceding claims, characterized in that the two membranes (58a, 58b) in the region of an edge of at least one of the two membranes (58a, 58b) by means of a weld line (60) extending in the circumferential direction ) are welded to one another, with an area between the weld line (60) and an interior space (64) formed between the two membranes (58a, 58b) in which the two membranes (58a, 58b) abut against one another at least in sections with frictional engagement.
9. Kraftstoff-Hochdruckpumpe (28) nach Anspruch 8, dadurch gekennzeichnet, dass zwischen der Schweißlinie und dem zwischen den beiden Membranen (58a, 58b) gebildeten Innenraum ein Umbug (76, 88) vorhanden ist. 9. High-pressure fuel pump (28) according to claim 8, characterized in that a fold (76, 88) is present between the weld line and the interior space formed between the two membranes (58a, 58b).
10. Kraftstoff-Hochdruckpumpe (28) nach Anspruch 9, dadurch gekennzeichnet, dass im Bereich des Umbugs (76, 88) ein radial innerer Abschnitt (90) der einen Membran (58b) in einem radial äußeren Abschnitt (78) der anderen Membran (58a) im Presssitz aufgenommen ist. 10. High-pressure fuel pump (28) according to claim 9, characterized in that in the region of the fold (76, 88) a radially inner section (90) of one membrane (58b) in a radially outer section (78) of the other membrane ( 58a) is received in a press fit.
EP20745158.4A 2019-08-09 2020-07-22 High-pressure fuel pump Withdrawn EP4010581A1 (en)

Applications Claiming Priority (2)

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DE102019212005.9A DE102019212005A1 (en) 2019-08-09 2019-08-09 High pressure fuel pump
PCT/EP2020/070631 WO2021028169A1 (en) 2019-08-09 2020-07-22 High-pressure fuel pump

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JP (1) JP2022543692A (en)
KR (1) KR20220043928A (en)
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JP7433552B1 (en) 2022-07-14 2024-02-19 三菱電機株式会社 Order support device, order support method, factory system, order method, and order support system

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US5772288A (en) * 1996-06-11 1998-06-30 Accuride Corporation Vehicle wheel
US5758564A (en) * 1996-06-13 1998-06-02 Tse Brakes, Inc. Brake actuator and method of manufacture
EP1411236B1 (en) * 2002-10-19 2012-10-10 Robert Bosch Gmbh Device for damping of pressure pulsations in a fluid system, especially in a fuel system of an internal combustion engine
US20080175735A1 (en) * 2007-01-10 2008-07-24 Stanadyne Corporation Inlet pressure attenuator for single plunger fuel pump
DE102008047303A1 (en) * 2008-02-18 2009-08-20 Continental Teves Ag & Co. Ohg Pulsationsdämpfungskapsel
JP5002523B2 (en) * 2008-04-25 2012-08-15 日立オートモティブシステムズ株式会社 Fuel pressure pulsation reduction mechanism and high-pressure fuel supply pump for internal combustion engine equipped with the same
JP2012184757A (en) * 2011-03-08 2012-09-27 Denso Corp Damper device and high-pressure pump having the same
WO2015081338A1 (en) * 2013-12-01 2015-06-04 Aspen Compressor, Llc Compact low noise rotary compressor
KR20160121010A (en) * 2015-04-09 2016-10-19 주식회사 현대케피코 Damper assembly of high-pressure fuelpump
WO2017022605A1 (en) * 2015-07-31 2017-02-09 イーグル工業株式会社 Diaphragm damper device coiled wave spring and damper system
DE102015219537A1 (en) 2015-10-08 2017-04-27 Robert Bosch Gmbh Diaphragm can for damping pressure pulsations in a low-pressure region of a piston pump
DE102016203217B4 (en) * 2016-02-29 2020-12-10 Vitesco Technologies GmbH Damper capsule, pressure pulsation damper and high-pressure fuel pump

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WO2021028169A1 (en) 2021-02-18
US20220333568A1 (en) 2022-10-20

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