EP4010581A1 - Pompe à carburant à haute pression - Google Patents

Pompe à carburant à haute pression

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Withdrawn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)
English (en)
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/fr
Withdrawn legal-status Critical Current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.

Landscapes

  • 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

L'invention concerne une pompe à carburant à haute pression (28) qui comprend un corps de pompe (46), un espace de réception (52) dans le corps de pompe (46), un amortisseur (44) sous la forme d'une cellule à diaphragme (56) ayant deux diaphragmes (58a, 58b), lequel amortisseur est disposé dans l'espace de réception (52), et un dispositif de maintien (62) pour maintenir la cellule à diaphragme (56) dans l'espace de réception (52). Selon l'invention, le dispositif de maintien (62) comprend une partie de raccordement (66), qui est reliée au corps de pompe (46) rigidement à la fois dans la direction axiale (70) et dans la direction radiale (72), en particulier est fixée, à la fois dans la direction axiale (70) et dans la direction radiale (72), à une surface latérale interne (92) qui délimite l'espace de réception (52).
EP20745158.4A 2019-08-09 2020-07-22 Pompe à carburant à haute pression Withdrawn EP4010581A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102019212005.9A DE102019212005A1 (de) 2019-08-09 2019-08-09 Kraftstoff-Hochdruckpumpe
PCT/EP2020/070631 WO2021028169A1 (fr) 2019-08-09 2020-07-22 Pompe à carburant à haute pression

Publications (1)

Publication Number Publication Date
EP4010581A1 true EP4010581A1 (fr) 2022-06-15

Family

ID=71784037

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20745158.4A Withdrawn EP4010581A1 (fr) 2019-08-09 2020-07-22 Pompe à carburant à haute pression

Country Status (7)

Country Link
US (1) US20220333568A1 (fr)
EP (1) EP4010581A1 (fr)
JP (1) JP2022543692A (fr)
KR (1) KR20220043928A (fr)
CN (1) CN114555932A (fr)
DE (1) DE102019212005A1 (fr)
WO (1) WO2021028169A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7433552B1 (ja) 2022-07-14 2024-02-19 三菱電機株式会社 受注支援装置、受注支援方法、工場システム、受注方法、および受注支援システム

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (fr) * 2002-10-19 2012-10-10 Robert Bosch Gmbh Dispositif pour l'atténuation des pulsations de pression dans un système de fluide, en particulier dans un système de carburant d'un moteur à combustion interne
US20080175735A1 (en) * 2007-01-10 2008-07-24 Stanadyne Corporation Inlet pressure attenuator for single plunger fuel pump
DE102008047303A1 (de) * 2008-02-18 2009-08-20 Continental Teves Ag & Co. Ohg Pulsationsdämpfungskapsel
JP5002523B2 (ja) * 2008-04-25 2012-08-15 日立オートモティブシステムズ株式会社 燃料の圧力脈動低減機構、及びそれを備えた内燃機関の高圧燃料供給ポンプ
JP2012184757A (ja) * 2011-03-08 2012-09-27 Denso Corp ダンパ装置およびこれを備えた高圧ポンプ
WO2015081338A1 (fr) * 2013-12-01 2015-06-04 Aspen Compressor, Llc Compresseur rotatif compact à faible bruit
KR20160121010A (ko) * 2015-04-09 2016-10-19 주식회사 현대케피코 연료의 맥동을 저감시키는 고압 연료펌프의 댐퍼구조체
WO2017022605A1 (fr) * 2015-07-31 2017-02-09 イーグル工業株式会社 Ressort ondulé hélicoïdal de dispositif amortisseur à membrane et système amortisseur
DE102015219537A1 (de) 2015-10-08 2017-04-27 Robert Bosch Gmbh Membrandose zum Dämpfen von Druckpulsationen in einem Niederdruckbereich einer Kolbenpumpe
DE102016203217B4 (de) * 2016-02-29 2020-12-10 Vitesco Technologies GmbH Dämpferkapsel, Druckpulsationsdämpfer und Kraftstoffhochdruckpumpe

Also Published As

Publication number Publication date
DE102019212005A1 (de) 2021-02-11
KR20220043928A (ko) 2022-04-05
JP2022543692A (ja) 2022-10-13
CN114555932A (zh) 2022-05-27
WO2021028169A1 (fr) 2021-02-18
US20220333568A1 (en) 2022-10-20

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