EP1346147A1 - Soupape d'injection de carburant - Google Patents

Soupape d'injection de carburant

Info

Publication number
EP1346147A1
EP1346147A1 EP01995612A EP01995612A EP1346147A1 EP 1346147 A1 EP1346147 A1 EP 1346147A1 EP 01995612 A EP01995612 A EP 01995612A EP 01995612 A EP01995612 A EP 01995612A EP 1346147 A1 EP1346147 A1 EP 1346147A1
Authority
EP
European Patent Office
Prior art keywords
fuel
swirl
fuel injection
valve
bypass
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Withdrawn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
EP01995612A
Other languages
German (de)
English (en)
Inventor
Fevzi Yildirim
Guenther Hohl
Michael Huebel
Norbert Keim
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 EP1346147A1 publication Critical patent/EP1346147A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/162—Means to impart a whirling motion to fuel upstream or near discharging orifices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M51/00—Fuel-injection apparatus characterised by being operated electrically
    • F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
    • F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
    • F02M51/0625—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures
    • F02M51/0664—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding
    • F02M51/0671—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means characterised by arrangement of mobile armatures having a cylindrically or partly cylindrically shaped armature, e.g. entering the winding; having a plate-shaped or undulated armature entering the winding the armature having an elongated valve body attached thereto
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18—Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for

Definitions

  • the invention relates to a fuel injector according to the preamble of the main claim.
  • Internal combustion engine which has a ' guide and seat area at the downstream end of the fuel injector, which is formed by three disc-shaped elements.
  • a swirl element is embedded between a guide element and a valve seat element.
  • the guide element serves to guide an axially movable valve needle projecting through it, while a valve closing section of the valve needle interacts with a valve seat surface of the valve seat element.
  • the "swirl element has an inner opening region with a plurality of swirl channels, which are not related to the outer periphery of the swirl element in combination. The total opening area extends completely across the axial thickness of the swirl element.
  • a disadvantage of the fuel injector known from the abovementioned publication is in particular that Fixed swirl angle that cannot be adapted to different operating conditions such as partial and full load operation of an internal combustion engine. As a result, the cone opening angle ⁇ of the injected mixture cloud cannot be adapted to the various operating states, which leads to inhomogeneities in combustion, increased fuel consumption and increased exhaust gas emissions.
  • the fuel injector according to the invention with the characterizing features of the main claim has the advantage that the swirl is adjustable depending on the operating state of the fuel injector, whereby a spray pattern adapted to the operating state of the fuel injector can be generated. This enables the mixture formation and the combustion process to be optimized.
  • the measures according to the invention are also used in a fuel injector continuous stroke can be used advantageously, since the desired modeling of the mixture cloud can also be carried out in a simple manner by means of a suitable geometry of the swirl channels.
  • the formation of a driver and the separation of the U-disc from the valve needle are advantageous, since the opening process of the fuel injector is not influenced by the lifting of the by-pass disc and the valve needle first goes through an undisturbed partial stroke until the driver strikes the by-pass disc.
  • Fig. 1 shows a partial axial section through a first
  • FIG. 2B is an enlarged detail in area II in Fig. 1, wherein the fuel injector is shown in the open state
  • FIG. 3A in the same representation as in Fig. 2A, a second embodiment of a Fuel injection valve according to the invention, wherein the fuel injection valve is shown in the closed state, and
  • FIG. 3B in the same representation as in Fig. 2B, a second embodiment of a fuel injector according to the invention, the fuel injector being shown in the open state.
  • a first exemplary embodiment of a fuel injection valve 1 designed according to the invention shown in FIG. 1 serves in particular for the direct injection of fuel into the combustion chamber of a spark-ignited, mixture-compressing internal combustion engine.
  • the fuel injector 1 comprises a solenoid 8 as actuator 27, which is encapsulated in a coil housing 9, a tubular inner pole 11 and a sleeve-shaped outer pole 14, which is welded to a nozzle body 2.
  • An armature 12 is operatively connected to a valve needle 3, which is formed in the spray direction towards a valve closing body 4.
  • the valve closing body 4 forms a sealing seat with a valve seat surface 6, which is formed on a valve seat body 5.
  • the fuel injection valve 1 opens inwards. At least one spray opening 7 is formed in the valve seat body 5.
  • a swirl device 15 is provided on the inflow side of the sealing seat, which comprises a guide disk 16, a bypass disk 17 and swirl channels 18.
  • the swirl device 15 is explained in more detail in the description of FIGS. 2A and 2B.
  • the armature 12 In the idle state of the fuel injection valve 1, the armature 12 is acted upon by the return spring 10 against a lifting direction in such a way that the valve closing body 4 is held in sealing contact with the valve seat surface 6.
  • the magnet coil 8 When the magnet coil 8 is excited, it builds up a magnetic field which moves the armature 12 against the spring force of the return spring 10 in the stroke direction.
  • the armature 12 also takes the valve needle 3 with it in the stroke direction.
  • the valve closing body 4 which is formed in one piece with the valve needle 3 in the exemplary embodiment, lifts off the valve seat surface 6, as a result of which the bypass disk 17, which is non-positively connected to the valve needle 3 by means of a weld seam 21, also moves in the stroke direction and thus a bypass channel 19 is opened. Fuel is passed through flow openings 20 in the guide disk 16 and through the bypass anal 19 and the swirl channels 18 past the sealing seat and into the at least one spray opening 7. A detailed representation of the process can be seen in FIGS. 2A and 2B.
  • the armature 12 drops from the inner pole 11 after the magnetic field has been sufficiently reduced by the force of the return spring 10, as a result of which the valve needle 3, which is operatively connected to the armature 12, moves against the stroke direction, the bypass disk 17 closes the bypass anal 19 , The valve closing body 4 is placed on the valve seat surface 6 and the fuel injector 1 is closed.
  • FIG. 2A shows an excerpted, schematic axial sectional view of the fuel injector 1 designed according to the invention in the closed state in area II in FIG. 1. Only those components are shown in the enlarged view that are essential in relation to the invention.
  • the design of the other components can be identical to a known fuel injection valve 1. Elements already described are included in all figures Matching reference numerals, so that a repetitive description is unnecessary.
  • a mixture-compressing, spark-ignited internal combustion engine places different demands on the shape, stoichiometry and penetration capacity of the mixture cloud injected into the combustion chamber than in full-load operation in part-load operation.
  • the mixture cloud should have a relatively small opening angle ⁇ , a large penetration capacity, a narrow core area with a richer mixture due to the small opening angle ot and a very lean shell, while in full-load range a large opening angle ⁇ and thus an almost homogeneous filling of the cylinder ignitable mixture is required.
  • the modeling of the mixture cloud parameters can be made possible by influencing the swirl by the measures according to the invention described here. If the fuel emerges from the spray opening with a small swirl, a mixture cloud with a small opening angle is injected, while a strong swirl generates a large beam expansion and thus a mixture cloud with a large opening angle.
  • the invention is particularly advantageously applicable in connection with a fuel injector 1 with a multi-stage stroke or piezoelectric actuators 27.
  • the swirl device 15 indicated in FIG. 1 with a bypass channel 19 provides for the fuel flow through the swirl device 15 to be designed as a function of the stroke of the valve needle 3 of the fuel injection valve 1. 2A, the bypass channel 19 is closed, and the fuel can only flow through the swirl channels 18 in the closed state of the fuel injection valve 1.
  • FIG. 2B shows, in the same representation as FIG. 2A, the fuel injection valve 1 according to the invention in the open state.
  • the actuator 27, which is designed as a solenoid coil 8 in the present exemplary embodiment is actuated, the valve needle 3 is raised in a stroke direction counter to the flow direction of the fuel, as a result of which the bypass disk 17 connected to the valve needle 3 via a weld seam 21 is also moved in the stroke direction.
  • the fuel flows through flow openings 20 in the guide disk 16 to the bypass 19.
  • 3A and 3B illustrate a second exemplary embodiment of the fuel injection valve 1 according to the invention in the same view as FIGS. 2A and 2B.
  • the bypass disk 17 in the present second exemplary embodiment is not with the valve needle 3 through a weld seam 21 or through Pressed connected, but is plugged onto the valve needle 3 axially movable.
  • the valve needle 3 has a driver 24 which is positively connected to the valve needle 3 by means of a weld seam 25 or by pressing etc.
  • This embodiment is particularly advantageously applicable to fuel injectors 1 with a two-stage stroke.
  • valve needle 3 passes through a partial stroke, which is accompanied, for example, only by a slight increase in the bypass disc 17 via the driver 24 or even without an increase in the bypass disc 17, which is why the fuel has a large tangential swirl component after the sealing seat having.
  • the invention is not limited to the exemplary embodiments shown and is particularly in the case of fuel injectors 1 with a multi-stage stroke, in the case of fuel injectors 1 with piezoelectric or magnetostrictive actuators 27 and realizable in any design variants of fuel injection valves 1.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

L'invention concerne une soupape d'injection de carburant (1), notamment de systèmes d'injection de carburant de moteurs à combustion interne. Cette soupape comprend un actionneur (27) et un pointeau (3) qui est actionné par l'actionneur (27) et qui commande un corps obturateur (4), lequel forme avec une surface siège de soupape (6) un siège étanche. Cette soupape comprend également un dispositif de turbulences (15) qui présente au moins un canal de turbulences (18) qui est parcouru de carburant soumis une composante tangentielle par rapport à l'axe longitudinal (26) de la soupape d'injection de carburant (1). La position axiale d'un disque de contournement (17) qui est en liaison active avec le pointeau (3), définit la section transversale d'au moins un canal de contournement (19) qui contourne le canal ou les canaux ce turbulences (18) en étant dépourvu(s) de composante tangentielle.
EP01995612A 2000-12-19 2001-12-15 Soupape d'injection de carburant Withdrawn EP1346147A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE10063260A DE10063260B4 (de) 2000-12-19 2000-12-19 Brennstoffeinspritzventil mit einstellbarem Drall
DE10063260 2000-12-19
PCT/DE2001/004747 WO2002050426A1 (fr) 2000-12-19 2001-12-15 Soupape d'injection de carburant

Publications (1)

Publication Number Publication Date
EP1346147A1 true EP1346147A1 (fr) 2003-09-24

Family

ID=7667765

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01995612A Withdrawn EP1346147A1 (fr) 2000-12-19 2001-12-15 Soupape d'injection de carburant

Country Status (5)

Country Link
US (1) US6857585B2 (fr)
EP (1) EP1346147A1 (fr)
JP (1) JP2004516408A (fr)
DE (1) DE10063260B4 (fr)
WO (1) WO2002050426A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7155458B1 (en) * 2002-04-05 2006-12-26 Network Appliance, Inc. Mechanism for distributed atomic creation of client-private files
US7093776B2 (en) * 2004-06-29 2006-08-22 Delphi Technologies, Inc Fuel injector nozzle atomizer having individual passages for inward directed accelerated cross-flow
DE102004031790A1 (de) * 2004-07-01 2006-01-26 Robert Bosch Gmbh Common-Rail-Injektor
DE102005023793B4 (de) * 2005-05-19 2012-01-12 Ulrich Schmid Vorrichtung zur Drallerzeugung in einem Kraftstoffeinspritzventil
EP1811166B1 (fr) * 2006-01-24 2008-11-05 Continental Automotive GmbH Ensemble à vanne pour une soupape d'injection et soupape d'injection
CN101375034B (zh) * 2006-01-27 2012-01-18 通用汽车环球科技运作公司 用于火花点火直喷式发动机的方法和设备
KR101458955B1 (ko) * 2008-01-04 2014-11-10 삼성전자주식회사 넓은 패스 전압 윈도우를 얻는 플래쉬 메모리 장치의프로그램 검증 방법
US20100314470A1 (en) * 2009-06-11 2010-12-16 Stanadyne Corporation Injector having swirl structure downstream of valve seat

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4321900A (en) * 1979-10-12 1982-03-30 Toyota Jidosha Kogyo Kabushiki Kaisha Fuel injection type internal combustion engine
US5299919A (en) * 1991-11-01 1994-04-05 Paul Marius A Fuel injector system
US5392994A (en) * 1993-11-01 1995-02-28 General Motors Corporation Fuel injection nozzle
US6125818A (en) * 1997-03-19 2000-10-03 Hiatchi, Ltd. Fuel injector and internal combustion engine having the same
DE19736682A1 (de) * 1997-08-22 1999-02-25 Bosch Gmbh Robert Brennstoffeinspritzventil
DE19736684A1 (de) 1997-08-22 1999-02-25 Bosch Gmbh Robert Brennstoffeinspritzventil
DE19915210A1 (de) 1999-04-03 2000-10-05 Bosch Gmbh Robert Brennstoffeinspritzventil

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO0250426A1 *

Also Published As

Publication number Publication date
WO2002050426A1 (fr) 2002-06-27
JP2004516408A (ja) 2004-06-03
US6857585B2 (en) 2005-02-22
DE10063260A1 (de) 2002-07-11
US20030155439A1 (en) 2003-08-21
DE10063260B4 (de) 2007-11-29

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Inventor name: YILDIRIM, FEVZI

Inventor name: HUEBEL, MICHAEL

Inventor name: HOHL, GUENTHER

Inventor name: KEIM, NORBERT

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