EP2239451B1 - A fuel injector for internal combustion engines - Google Patents

A fuel injector for internal combustion engines Download PDF

Info

Publication number
EP2239451B1
EP2239451B1 EP09156590A EP09156590A EP2239451B1 EP 2239451 B1 EP2239451 B1 EP 2239451B1 EP 09156590 A EP09156590 A EP 09156590A EP 09156590 A EP09156590 A EP 09156590A EP 2239451 B1 EP2239451 B1 EP 2239451B1
Authority
EP
European Patent Office
Prior art keywords
cut
atomizer
section
longitudinal bore
spindle
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.)
Active
Application number
EP09156590A
Other languages
German (de)
French (fr)
Other versions
EP2239451A1 (en
Inventor
Pierpaolo Miotti
Marco Destro
Marco Coppo
Luca Formia
Marco Garlasche'
Massimo Lombardo
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.)
Wartsila Switzerland Ltd
Original Assignee
Wartsila Switzerland Ltd
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 Wartsila Switzerland Ltd filed Critical Wartsila Switzerland Ltd
Priority to EP09156590A priority Critical patent/EP2239451B1/en
Priority to DK09156590.3T priority patent/DK2239451T3/en
Priority to AT09156590T priority patent/ATE523686T1/en
Priority to JP2010017827A priority patent/JP5822249B2/en
Priority to CN201010156144.8A priority patent/CN101852157B/en
Priority to KR1020100028612A priority patent/KR101686671B1/en
Publication of EP2239451A1 publication Critical patent/EP2239451A1/en
Application granted granted Critical
Publication of EP2239451B1 publication Critical patent/EP2239451B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1806Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for characterised by the arrangement of discharge orifices, e.g. orientation or size
    • F02M61/182Discharge orifices being situated in different transversal planes with respect to valve member direction of movement
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/042The valves being provided with fuel passages
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/06Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series the valves being furnished at seated ends with pintle or plug shaped extensions
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/04Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
    • F02M61/10Other injectors with elongated valve bodies, i.e. of needle-valve type
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1866Valve seats or member ends having multiple cones
    • 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
    • F02M61/00Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
    • F02M61/16Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
    • F02M61/18Injection nozzles, e.g. having valve seats; Details of valve member seated ends, not otherwise provided for
    • F02M61/1893Details of valve member ends not covered by groups F02M61/1866 - F02M61/188

Definitions

  • the present invention relates to a fuel injector for internal combustion engines.
  • the invention relates in particular to a fuel injector for large two-stroke internal combustion engines, such as diesel engines for naval propulsion.
  • the present invention relates to a fuel injector according to the preamble of claim 1, comprising a housing, a valve guide fixed at the lower end of the housing, an atomizer fixed at a lower end of the valve guide and provided with a plurality of nozzle bores, a spindle having a valve portion cooperating with a valve seat of the valve guide, and a cut-off element extending into a longitudinal bore of the atomizer to reduce the volume in fluid connection with the nozzle bores when the spindle is in a closed position.
  • EP-A-052937 discloses a fuel injector comprising an axially displaceable spindle having a valve portion which cooperates with a corresponding valve seat of the valve guide and a cut-off element extending below the valve portion of the valve spindle into a central bore of the atomizer.
  • the outer wall of the cut-off element is effective to open and close inlet openings of the nozzle bores.
  • the nozzle bores are arranged in a single row, i.e. the inlet openings of the nozzle bores are all placed at approximately the same distance from the lower end of the atomizer.
  • a problem of this solution is that the total number of nozzle bores arranged within a maximum angle cannot be increased without compromising the strength of the side wall of the atomizer.
  • W02008/071187 discloses a fuel injector according to the preamble of claim 1, wherein the inlet openings of the nozzle bores of the atomizer are arranged in a first row and in a second row axially spaced apart and separated from each other by a cylindrical sealing portion.
  • a cut-off element extending into a longitudinal bore of the atomizer has a first cylindrical section arranged to open and close the lower row of inlet openings and a second cylindrical section cooperating with a secondary valve seat for closing off the upper row of inlet openings when the valve spindle is closed.
  • the lower row of inlet openings is supplied by fuel flowing through a central duct of the cut-off element and the upper row of inlet openings is supplied by fuel flowing in an annular passage defined between the inner wall of the atomizer bore and the outer surface of the cut-off element.
  • the object of the present invention is to provide an improved injector which gives greater freedom in the arrangement of the nozzle bores in the atomizer, which ensures that all the nozzle bores are supplied simultaneously and which requires a very short travel of the spindle even if the nozzle bores are arranged in an irregular pattern.
  • the inlet openings of the nozzle bores are all in flow connection with an injection chamber between upper and lower cut-off sections and in the open position of the spindle the upper cut-off section remains closed and the lower cut-off section is opened to establish a flow connection between a central duct of the cut-off element and the injection chamber.
  • the arrangement according to the invention provides more freedom in the positioning of the nozzle bores, which can be located at any atomizer height and according to a pattern designed to optimize the spray quality.
  • the nozzle bores should not necessarily be located in one or two single rows as in the prior art.
  • the atomizer of the present invention can be designed with a greater number of nozzle bores, thus improving the spray quality and the fuel combustion, without compromising the strength of the side wall of the atomizer.
  • the nozzle bores of the present invention can be axially spaced apart from each other with a relevant height difference even with a very short lift of the spindle.
  • the lift of the spindle can be shorter than the axial distance between the nozzle bores.
  • the reference number 10 indicates a fuel injector for diesel engines according to the present invention.
  • the injector 10 is intended to be mounted into an elongated cavity 12 formed in the head 14 of the engine.
  • the injector 10 comprises an elongated housing 16 having at its top an enlarged head 18 protruding outside of the cavity 12 and fixed to the engine head 14 by screws 20 (only one of which is visible in figure 1 ).
  • a fuel supply duct 22 is formed in the housing 16 and is connected at its upper end to an opening 24 connected to a fuel supply line (not shown).
  • a thrust element 26 is axially movable along a longitudinal axis 28 inside a through cavity 30 formed in the housing 16.
  • a compression spring 32 acts on a top head 34 of the thrust -element 26. The upper end of the compression spring 32 acts against an adjustment member 36 screwed into an axial hole formed in the head 18 of the injector 10.
  • a valve guide 38 is fixed at a lower end of the housing 16.
  • a tubular fixing member 40 engages a threaded portion 42 of the housing 16 to secure the valve guide 38 at the front bottom end of the housing 16.
  • the guide valve 38 has a longitudinal guide bore 44.
  • a chamber 46 is formed at the lower end of the guide bore 44. The chamber 46 is in flow connection with a fuel supply duct 48 the upper end of which is connected to the lower end of the fuel supply duct 22 of the housing 16.
  • a conical valve seat 50 is provided at the bottom end of the chamber 46 of the valve guide 38.
  • a short duct 52 extends downwardly of the valve seat 50 and opens on a front face 54 of the valve guide 38.
  • An atomizer 56 is fixed at a lower end of the valve guide 38.
  • the atomizer 56 has a cylindrical body of corrosion-resistant material with a closed bottom end 58. As shown in figure 1 , the lower end of the atomizer 56 extends in a combustion chamber C of the engine.
  • An upper front face 60 of the atomizer 56 frontally abuts the front face 54 of the valve guide 38.
  • a circular upper flange 62 of the atomizer 56 engages a bottom cylindrical surface 64 of the guide valve 38.
  • a vertical pin 66 engages mutually facing openings of the valve guide 38 and of the atomizer 56 to set the atomizer 56 in a fixed angular position with respect to the valve guide 38.
  • the atomizer 56 is axially fixed to the valve guide 38 by means of a cup-shaped retaining element 68.
  • the retaining element 68 and the atomizer 56 have mutually abutting conical surfaces 70 and 72.
  • the cylindrical body of the atomizer 56 projects downwardly through a bottom opening 74 of the retaining element 68.
  • the retaining element 68 has an upper flange 76 which snap-engages an elastic ring 78 carried at the lower end of the tubular fixing member 40.
  • the atomizer 56 has a longitudinal bore 80 closed at its bottom end.
  • the upper end of the longitudinal bore 80 is in flow connection with the chamber 46 through the short duct 52 and the valve seat 50.
  • a plurality of nozzle bores 82 is formed in the lateral wall of the atomizer 56.
  • the nozzle bores 82 have respective inner openings 84 facing into the longitudinal bore 80 and outlet openings 86 open on the outer surface of the atomizer 56.
  • the inlet openings 84 of at least some of the nozzle bores 82 are axially spaced from each other.
  • the nozzle bores 82 are positioned according to a substantially irregular pattern.
  • the nozzle bores 82 can be arranged according to any desired pattern.
  • the position of the nozzle bores 82 can be defined as desired by the designer in order to optimize' the spray quality.
  • the number of the nozzle bores 82, the axial position of the inlet and outlet openings 84, 86 and the inclination of the axes of the nozzle bores 82 with respect to the longitudinal axis 28 can be varied as desired for providing an optimal spraying pattern.
  • the fact that the nozzle bores 82 can be placed at any desired axial position is particularly useful in that the total number of nozzle bores arranged within a maximum angle (of e.g. 120°) can be increased without compromising the strength of the side wall of the atomizer 56.
  • the nozzle bores 82 are not necessarily located in parallel rows as in prior art solutions.
  • the outlet openings 86 of the nozzle bores 82 can be located at different atomizer heights H1, H2, H3, H4, H5.
  • a spindle 88 is axially displaceable into the valve guide 38.
  • the spindle 88 has a cylindrical portion 90 which slidably engages the longitudinal guide bore 44 of the valve guide 38.
  • the spindle 88 has a conical valve portion 92 which cooperates with, the conical valve seat 50 of the valve guide 38.
  • the spindle 88 is axially movable between a closed position shown in figure 2 and an open position shown in figure 3 . Referring to figure 1 , the upper end of the spindle 88 abuts against the lower end of the thrust element 26.
  • the compression spring 32 biases the spindle 88 in its closed position wherein the valve portion 92 of the spindle 88 abuts against the valve seat 50 to shut-off the flow connection between the chamber 46 and the longitudinal bore 80 of the atomizer 56.
  • the spindle 88 comprises a cut-off element 94 which extends coaxially below the valve portion 92 and into the longitudinal duct 80 of the atomizer 56.
  • the cut-off element 94 is fixed to or integrally formed with the remaining part of the spindle 88.
  • the outer surface of the cut-off element 94 has a first cylindrical sealing portion 96 and a second cylindrical sealing portion 98 axially spaced apart from each other.
  • the first sealing portion 96 engages with tight fit a first cylindrical sealing surface 100 of the longitudinal bore 80 to define an upper cut-off section 102.
  • the second sealing portion 98 engages with tight fit a second cylindrical sealing surface 104 of the longitudinal bore 80 to define a lower cut-off section 106.
  • the first cylindrical sealing surface 100 has a diameter greater than that of the second cylindrical sealing surface 104.
  • the cut-off element 94 has a portion 108 with reduced diameter axially extending between the first sealing portion 96 and the second sealing portion 98.
  • annular injection chamber 110 is defined in a region of the longitudinal bore 80 comprised between the upper cut-off section 102 and the lower cut-off section 106.
  • the inlet openings 84 of the nozzle bores 82 are all in flow connection with the injection chamber 110.
  • the cut-off element 94 has a central duct 112 which is in flow connection through transverse holes 116 with an upper region 114 of the longitudinal bore 80 located above the upper cut-off section 102.
  • the central duct 112 is also in flow connection through a bottom opening 120 with a lower region 118 of the longitudinal bore 80 located below the lower cut-off off section 106.
  • the injection chamber 110 is sealed from the upper region 114 by the upper cut-off section 102 and is also sealed from the lower region 118 by the lower cut-off section 106.
  • the upper region 114 is also sealed from the chamber 46 by the mutually abutting surfaces of the valve seat 50 and valve portion 92.
  • the upward movement of the cut-off element 94 opens the lower cut-off section 106 and puts the injection chamber 110 in flow connection with the lower region 118. Pressurised fluid reaches the injection chamber 110 through the upper region 114, the transverse holes 116, the central duct 112 and the bottom opening 120. All the nozzle bores 82 are simultaneously supplied with pressurised fuel as soon as the lower cut-off section 106 is opened.
  • a second embodiment of the present invention is shown in figures 6 and 7 .
  • the elements corresponding to the ones previously disclosed are indicated by the same reference numbers.
  • the cut-off off element 94 has a constant or substantially constant outer diameter between the first sealing portion 96 and the second sealing portion 98.
  • the longitudinal bore 80 of the atomizer 56 has an annular chamber 122 of increased diameter between the first sealing surface 100 and the second sealing surface 104.
  • the chamber 122 can have any shape, not necessarily cylindrical.
  • a recess 124 in the annular chamber 122 there is formed a recess 124 in correspondence with the inlet openings 84 of the nozzle bores 82.
  • the annular chamber 122 and the recess 124 form the injection chamber 110.
  • the operation of this second embodiment is substantially identical to that of the embodiment previously described-with reference to figures 2 and 3 .
  • a remarkable advantage of the present invention is that a reduced axial travel of the spindle is sufficient for supplying simultaneously all the nozzle bores 82.
  • the opening travel of the spindle 88 is independent of the position and dimensions of the nozzle bores 82.
  • the nozzle bores 82 can be arranged according to any desired pattern, which can be chosen to optimize the spray quality.
  • the number of the nozzle bores 82 can also be increased without compromising the strength of the wall of the atomizer.

Landscapes

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

Abstract

A fuel injector for internal combustion engines, comprising: - a housing (16), - a valve guide (38) fixed at a lower end of said housing (16), the valve guide (38) having a longitudinal guide bore (44) and a chamber (46) provided with a valve seat (50), said chamber (46) being connected to a fuel supply duct (22,48); - an atomizer (56) fixed at a lower end of said valve guide (38), the atomizer (56) having a longitudinal bore (80) in flow connection with said chamber (46), the atomizer having a plurality of nozzle bores (82) having inlet openings (84) facing into said longitudinal bore (80); - a spindle (88) having a valve portion (92) cooperating with said valve seat (50), and a cut-off element (94) extending into said longitudinal bore (80) of the atomizer (56), wherein an upper cut-off section (102) and a lower cut-off section (106) axially spaced apart from each other are defined between the outer surface of the cut-off element (94) and the inner surface of the longitudinal bore (80), cut-off sections (102,106) being both closed in the closed position of the spindle (88), the cut-off element (94) having a central duct (112) in flow connection with the longitudinal bore (80) of the atomizer (56) both above the upper cut-off section (102) and below the lower cut-off section (106).

Description

    Background of the invention
  • The present invention relates to a fuel injector for internal combustion engines. The invention relates in particular to a fuel injector for large two-stroke internal combustion engines, such as diesel engines for naval propulsion.
  • More specifically, the present invention relates to a fuel injector according to the preamble of claim 1, comprising a housing, a valve guide fixed at the lower end of the housing, an atomizer fixed at a lower end of the valve guide and provided with a plurality of nozzle bores, a spindle having a valve portion cooperating with a valve seat of the valve guide, and a cut-off element extending into a longitudinal bore of the atomizer to reduce the volume in fluid connection with the nozzle bores when the spindle is in a closed position.
  • Background of the invention
  • EP-A-052937 discloses a fuel injector comprising an axially displaceable spindle having a valve portion which cooperates with a corresponding valve seat of the valve guide and a cut-off element extending below the valve portion of the valve spindle into a central bore of the atomizer. The outer wall of the cut-off element is effective to open and close inlet openings of the nozzle bores.
  • In the solution disclosed in EP-A-052937 the nozzle bores are arranged in a single row, i.e. the inlet openings of the nozzle bores are all placed at approximately the same distance from the lower end of the atomizer. A problem of this solution is that the total number of nozzle bores arranged within a maximum angle cannot be increased without compromising the strength of the side wall of the atomizer.
  • W02008/071187 discloses a fuel injector according to the preamble of claim 1, wherein the inlet openings of the nozzle bores of the atomizer are arranged in a first row and in a second row axially spaced apart and separated from each other by a cylindrical sealing portion. A cut-off element extending into a longitudinal bore of the atomizer has a first cylindrical section arranged to open and close the lower row of inlet openings and a second cylindrical section cooperating with a secondary valve seat for closing off the upper row of inlet openings when the valve spindle is closed.
  • When the valve spindle is open, the lower row of inlet openings is supplied by fuel flowing through a central duct of the cut-off element and the upper row of inlet openings is supplied by fuel flowing in an annular passage defined between the inner wall of the atomizer bore and the outer surface of the cut-off element.
  • Summary of the invention
  • The object of the present invention is to provide an improved injector which gives greater freedom in the arrangement of the nozzle bores in the atomizer, which ensures that all the nozzle bores are supplied simultaneously and which requires a very short travel of the spindle even if the nozzle bores are arranged in an irregular pattern.
  • In accordance with the present invention, this object is achieved by a fuel injector having the features of claim 1.
  • In the solution according to the present invention, in the closed position of the spindle the inlet openings of the nozzle bores are all in flow connection with an injection chamber between upper and lower cut-off sections and in the open position of the spindle the upper cut-off section remains closed and the lower cut-off section is opened to establish a flow connection between a central duct of the cut-off element and the injection chamber.
  • In the solution according to the present invention all the nozzle bores are simultaneously supplied when the lower cut-off section is opened.
  • The arrangement according to the invention provides more freedom in the positioning of the nozzle bores, which can be located at any atomizer height and according to a pattern designed to optimize the spray quality. In accordance with the present invention, the nozzle bores should not necessarily be located in one or two single rows as in the prior art.
  • The atomizer of the present invention can be designed with a greater number of nozzle bores, thus improving the spray quality and the fuel combustion, without compromising the strength of the side wall of the atomizer.
  • The nozzle bores of the present invention can be axially spaced apart from each other with a relevant height difference even with a very short lift of the spindle. In particular, the lift of the spindle can be shorter than the axial distance between the nozzle bores.
  • Brief description of the drawings
  • Further characteristics and advantages of the present invention will become clear in the course of the detailed description which follows, given purely by way of non-limiting example, with reference to the annexed drawings, wherein:
    • figure 1 is an axial cross-section of an injector according to the present invention,
    • figures 2 and 3 are enlarged views of the part indicated by the arrow II in figure 1 respectively in a closed and open position,
    • figure 4 is an enlarged perspective view of the part indicated by the arrow II in figure 1,
    • figure 5 is a front view of the part indicated by the arrow V in figure 4,
    • figure 6 is a cross-section corresponding to figure 2 and showing a second embodiment of the present invention,
    • figure 7 is a cross-section taken along line VII-VII of figure 6.
    Description of the preferred embodiments
  • Referring to figure 1, the reference number 10 indicates a fuel injector for diesel engines according to the present invention. The injector 10 is intended to be mounted into an elongated cavity 12 formed in the head 14 of the engine. The injector 10 comprises an elongated housing 16 having at its top an enlarged head 18 protruding outside of the cavity 12 and fixed to the engine head 14 by screws 20 (only one of which is visible in figure 1).
  • In the following description and in the claims the terms "upper", "lower", "top", "bottom" and the like refer to the normal position of use of the injector 10. It is however envisaged that the injector 10 could be mounted in a more or less inclined position with respect to a vertical axis.
  • A fuel supply duct 22 is formed in the housing 16 and is connected at its upper end to an opening 24 connected to a fuel supply line (not shown). A thrust element 26 is axially movable along a longitudinal axis 28 inside a through cavity 30 formed in the housing 16. A compression spring 32 acts on a top head 34 of the thrust -element 26. The upper end of the compression spring 32 acts against an adjustment member 36 screwed into an axial hole formed in the head 18 of the injector 10.
  • A valve guide 38 is fixed at a lower end of the housing 16. A tubular fixing member 40 engages a threaded portion 42 of the housing 16 to secure the valve guide 38 at the front bottom end of the housing 16. The guide valve 38 has a longitudinal guide bore 44. A chamber 46 is formed at the lower end of the guide bore 44. The chamber 46 is in flow connection with a fuel supply duct 48 the upper end of which is connected to the lower end of the fuel supply duct 22 of the housing 16.
  • With reference to figures 2 and 3, a conical valve seat 50 is provided at the bottom end of the chamber 46 of the valve guide 38. A short duct 52 extends downwardly of the valve seat 50 and opens on a front face 54 of the valve guide 38.
  • An atomizer 56 is fixed at a lower end of the valve guide 38. The atomizer 56 has a cylindrical body of corrosion-resistant material with a closed bottom end 58. As shown in figure 1, the lower end of the atomizer 56 extends in a combustion chamber C of the engine. An upper front face 60 of the atomizer 56 frontally abuts the front face 54 of the valve guide 38. A circular upper flange 62 of the atomizer 56 engages a bottom cylindrical surface 64 of the guide valve 38. A vertical pin 66 engages mutually facing openings of the valve guide 38 and of the atomizer 56 to set the atomizer 56 in a fixed angular position with respect to the valve guide 38.
  • The atomizer 56 is axially fixed to the valve guide 38 by means of a cup-shaped retaining element 68. The retaining element 68 and the atomizer 56 have mutually abutting conical surfaces 70 and 72. The cylindrical body of the atomizer 56 projects downwardly through a bottom opening 74 of the retaining element 68. As shown in figure 1, the retaining element 68 has an upper flange 76 which snap-engages an elastic ring 78 carried at the lower end of the tubular fixing member 40.
  • With reference to figures 2 and 3, the atomizer 56 has a longitudinal bore 80 closed at its bottom end. The upper end of the longitudinal bore 80 is in flow connection with the chamber 46 through the short duct 52 and the valve seat 50. A plurality of nozzle bores 82 is formed in the lateral wall of the atomizer 56. The nozzle bores 82 have respective inner openings 84 facing into the longitudinal bore 80 and outlet openings 86 open on the outer surface of the atomizer 56. The inlet openings 84 of at least some of the nozzle bores 82 are axially spaced from each other. In the example shown in figures 4 and 5, the nozzle bores 82 are positioned according to a substantially irregular pattern.
  • An important feature of the present invention is that the nozzle bores 82 can be arranged according to any desired pattern. The position of the nozzle bores 82 can be defined as desired by the designer in order to optimize' the spray quality. In particular, the number of the nozzle bores 82, the axial position of the inlet and outlet openings 84, 86 and the inclination of the axes of the nozzle bores 82 with respect to the longitudinal axis 28 can be varied as desired for providing an optimal spraying pattern. The fact that the nozzle bores 82 can be placed at any desired axial position is particularly useful in that the total number of nozzle bores arranged within a maximum angle (of e.g. 120°) can be increased without compromising the strength of the side wall of the atomizer 56. The nozzle bores 82 are not necessarily located in parallel rows as in prior art solutions. For instance, as shown in figure 5, the outlet openings 86 of the nozzle bores 82 can be located at different atomizer heights H1, H2, H3, H4, H5.
  • With reference to figure 1, a spindle 88 is axially displaceable into the valve guide 38. The spindle 88 has a cylindrical portion 90 which slidably engages the longitudinal guide bore 44 of the valve guide 38. As best shown in figures 2 and 3, the spindle 88 has a conical valve portion 92 which cooperates with, the conical valve seat 50 of the valve guide 38. The spindle 88 is axially movable between a closed position shown in figure 2 and an open position shown in figure 3. Referring to figure 1, the upper end of the spindle 88 abuts against the lower end of the thrust element 26. The compression spring 32, through the thrust element 26, biases the spindle 88 in its closed position wherein the valve portion 92 of the spindle 88 abuts against the valve seat 50 to shut-off the flow connection between the chamber 46 and the longitudinal bore 80 of the atomizer 56.
  • Referring to figures 2 and 3, the spindle 88 comprises a cut-off element 94 which extends coaxially below the valve portion 92 and into the longitudinal duct 80 of the atomizer 56. The cut-off element 94 is fixed to or integrally formed with the remaining part of the spindle 88. The outer surface of the cut-off element 94 has a first cylindrical sealing portion 96 and a second cylindrical sealing portion 98 axially spaced apart from each other. The first sealing portion 96 engages with tight fit a first cylindrical sealing surface 100 of the longitudinal bore 80 to define an upper cut-off section 102. The second sealing portion 98 engages with tight fit a second cylindrical sealing surface 104 of the longitudinal bore 80 to define a lower cut-off section 106. The first cylindrical sealing surface 100 has a diameter greater than that of the second cylindrical sealing surface 104.
  • In the closed position of the spindle 88 shown in figure 2 the upper cut-off section 102 and the lower cut-off section 106 are both closed. In the open position of the spindle 88 shown in figure 3 the upper cut-off section 102 remains closed and the lower cut-off section 106 is open. Preferably, the cut-off element 94 has a portion 108 with reduced diameter axially extending between the first sealing portion 96 and the second sealing portion 98.
  • In the closed position shown in figure 2 an annular injection chamber 110 is defined in a region of the longitudinal bore 80 comprised between the upper cut-off section 102 and the lower cut-off section 106. The inlet openings 84 of the nozzle bores 82 are all in flow connection with the injection chamber 110.
  • The cut-off element 94 has a central duct 112 which is in flow connection through transverse holes 116 with an upper region 114 of the longitudinal bore 80 located above the upper cut-off section 102. The central duct 112 is also in flow connection through a bottom opening 120 with a lower region 118 of the longitudinal bore 80 located below the lower cut-off off section 106.
  • When the spindle 88 is in the closed position shown in figure 2, the injection chamber 110 is sealed from the upper region 114 by the upper cut-off section 102 and is also sealed from the lower region 118 by the lower cut-off section 106. The upper region 114 is also sealed from the chamber 46 by the mutually abutting surfaces of the valve seat 50 and valve portion 92. When pressurised fuel is supplied to the chamber 46 through the supply ducts 22 and 48, an upwardly directed hydraulic force is generated on the spindle 88. When such force overcomes the force of the compression spring 32, the spindle 88 moves to the open position of figure 3. In this position, the upper region 114 of the longitudinal bore 80 is in flow connection with the chamber 46 through the open valve seat 50. The upward movement of the cut-off element 94 opens the lower cut-off section 106 and puts the injection chamber 110 in flow connection with the lower region 118. Pressurised fluid reaches the injection chamber 110 through the upper region 114, the transverse holes 116, the central duct 112 and the bottom opening 120. All the nozzle bores 82 are simultaneously supplied with pressurised fuel as soon as the lower cut-off section 106 is opened.
  • A second embodiment of the present invention is shown in figures 6 and 7. The elements corresponding to the ones previously disclosed are indicated by the same reference numbers. In this second embodiment of the present invention, the cut-off off element 94 has a constant or substantially constant outer diameter between the first sealing portion 96 and the second sealing portion 98. The longitudinal bore 80 of the atomizer 56 has an annular chamber 122 of increased diameter between the first sealing surface 100 and the second sealing surface 104. The chamber 122 can have any shape, not necessarily cylindrical. Preferably, in the annular chamber 122 there is formed a recess 124 in correspondence with the inlet openings 84 of the nozzle bores 82. The annular chamber 122 and the recess 124 form the injection chamber 110. The operation of this second embodiment is substantially identical to that of the embodiment previously described-with reference to figures 2 and 3.
  • A remarkable advantage of the present invention is that a reduced axial travel of the spindle is sufficient for supplying simultaneously all the nozzle bores 82. The opening travel of the spindle 88 is independent of the position and dimensions of the nozzle bores 82. In addition, since the inlet openings 84 of all the nozzle bores 82 are all in flow communication with the same injection chamber 110, the nozzle bores 82 can be arranged according to any desired pattern, which can be chosen to optimize the spray quality. The number of the nozzle bores 82 can also be increased without compromising the strength of the wall of the atomizer.

Claims (5)

  1. A fuel injector for internal combustion engines, comprising:
    - a housing (16),
    - a valve guide (38) fixed at a lower end of said housing (16), the valve guide (38) having a longitudinal guide bore (44) and a chamber (46) provided with a valve seat (50), said chamber (46) being connected to a fuel supply duct (22, 48);
    - an atomizer (56) fixed at a lower end of said valve guide (38), the atomizer (56) having a longitudinal bore (80) in flow connection with said chamber (46), the atomizer having a plurality of nozzle bores (82) having inlet openings (84) facing into said longitudinal bore (80); and
    - a spindle (88) having a valve portion (92) cooperating with said valve seat (50) and a cut-off element (94) extending into said longitudinal bore (80) of the atomizer (56), wherein an upper cut-off section (102) and a lower cut-off-section (106) axially spaced apart from each other are defined between the outer surface of the cut-off element (94) and the inner surface of the longitudinal bore (80), cut-off sections (102, 106) being both closed- in the closed position of the spindle (88), the cut-off element (94) having a central duct (112) in flow connection with the longitudinal bore (80) of the atomizer (56) both above the upper cut-off section (102) and below the lower cut-off section (106);
    characterized in that in the closed position of the spindle (88) the inlet openings (84) of said nozzle bores (82) are all in flow connection with an injection chamber (110) between said upper and lower cut-off sections (102, 106), and that in the open position of the spindle (88) the upper cut-off section (102) remains closed and the lower cut-off section (106) is opened to establish a flow connection between the central duct (112) of the cut-off element (94) and said injection chamber (110).
  2. A fuel injector according to claim 1, characterized in that the cut-off element (94) has a first and a second cylindrical sealing portion (96, 98) forming respectively with first and second cylindrical sealing surfaces (100, 104) of said longitudinal bore (80) said upper and lower cut-off sections (102, 106).
  3. A fuel injector according to claim 1 or claim 2, characterised in that a lower region (118) of said longitudinal bore (80) below said lower cut-off section (106) is in flow connection with said central duct (112) of the cut-off element (94).
  4. A fuel injector according to claim 2, characterized in that said first cylindrical sealing surface (100) has a diameter greater than that of said second cylindrical sealing surface (104).
  5. A fuel injector according to claim 2, characterized in that the cut-off element (94) has a constant or substantially constant outer diameter between said first and second cylindrical sealing portions (96, 98) and that the longitudinal bore (80) of the atomizer (56) has a chamber (122) with increased diameter between said first and second cylindrical sealing surfaces (100, 104).
EP09156590A 2009-03-30 2009-03-30 A fuel injector for internal combustion engines Active EP2239451B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
EP09156590A EP2239451B1 (en) 2009-03-30 2009-03-30 A fuel injector for internal combustion engines
DK09156590.3T DK2239451T3 (en) 2009-03-30 2009-03-30 Fuel injection device for internal combustion engines
AT09156590T ATE523686T1 (en) 2009-03-30 2009-03-30 FUEL INJECTION VALVE FOR COMBUSTION ENGINES
JP2010017827A JP5822249B2 (en) 2009-03-30 2010-01-29 Fuel injector for internal combustion engine
CN201010156144.8A CN101852157B (en) 2009-03-30 2010-03-30 A fuel injector for internal combustion engines
KR1020100028612A KR101686671B1 (en) 2009-03-30 2010-03-30 A fuel injector for internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP09156590A EP2239451B1 (en) 2009-03-30 2009-03-30 A fuel injector for internal combustion engines

Publications (2)

Publication Number Publication Date
EP2239451A1 EP2239451A1 (en) 2010-10-13
EP2239451B1 true EP2239451B1 (en) 2011-09-07

Family

ID=40941514

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09156590A Active EP2239451B1 (en) 2009-03-30 2009-03-30 A fuel injector for internal combustion engines

Country Status (6)

Country Link
EP (1) EP2239451B1 (en)
JP (1) JP5822249B2 (en)
KR (1) KR101686671B1 (en)
CN (1) CN101852157B (en)
AT (1) ATE523686T1 (en)
DK (1) DK2239451T3 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013001098B3 (en) * 2013-01-23 2014-07-03 L'orange Gmbh Fuel injector for use in common-rail system in motor car, has nozzle needle comprising end section that is sealingly retained in through-hole of nozzle tip, where axial bore is extended as blind hole towards near nozzle into end section
RU2677436C1 (en) * 2016-12-13 2019-01-16 МАН Дизель энд Турбо, филиал МАН Дизель энд Турбо СЕ, Тускланд. Nozzle of the fuel valve for injection of fuel in the cylinder of the big two-tact internal combustion engine with turbocharging with compressed ignition

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010040401A1 (en) * 2010-09-08 2012-03-08 Robert Bosch Gmbh fuel injector
DK2503138T3 (en) * 2011-03-24 2013-06-03 Omt Ohg Torino S P A Electrically controlled fuel injection device for large diesel engines
JP5798898B2 (en) * 2011-11-24 2015-10-21 三菱重工業株式会社 Fuel injection device
US10337448B2 (en) * 2015-12-22 2019-07-02 Ford Global Technologies, Llc Methods and systems for a fuel injector assembly
JP7079182B2 (en) * 2018-10-26 2022-06-01 株式会社クボタ Electronic fuel injection diesel engine
DK181318B1 (en) 2022-02-18 2023-08-10 Man Energy Solutions Filial Af Man Energy Solutions Se Tyskland A fuel valve for a large turbocharged two-stroke uniflow crosshead internal combustion engine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2711902A1 (en) * 1977-03-18 1978-09-21 Bosch Gmbh Robert FUEL INJECTOR
DE2948451A1 (en) * 1979-12-01 1981-06-04 Robert Bosch Gmbh, 7000 Stuttgart Fuel injector for IC engine - has push rod upstream of valve determining cross=section of injection openings
DK495880A (en) 1980-11-20 1982-05-21 B & W Diesel As FUEL ENGINE FOR COMBUSTION ENGINES
JPH0158770U (en) * 1987-10-07 1989-04-12
JPH0538353U (en) * 1991-10-30 1993-05-25 いすゞ自動車株式会社 Hole type nozzle
JPH05321789A (en) * 1992-05-15 1993-12-07 Kubota Corp Multihole nozzle type fuel injection on valve for diesel engine
JPH08144896A (en) * 1994-11-25 1996-06-04 Zexel Corp Variable nozzle hole type fuel injection nozzle
DE19815918A1 (en) * 1998-04-09 1999-10-21 Man B & W Diesel As Fuel injector
JPH11351103A (en) * 1998-06-13 1999-12-21 Toyota Central Res & Dev Lab Inc Fuel injection valve
EP1380750B1 (en) * 1999-06-25 2005-11-23 Delphi Technologies, Inc. Fuel injector
JP4182315B2 (en) * 2000-02-04 2008-11-19 株式会社デンソー Fuel injection nozzle
WO2001059293A1 (en) * 2000-02-07 2001-08-16 Robert Bosch Gmbh Injection nozzle
JP5249943B2 (en) * 2006-12-15 2013-07-31 マン・ディーゼル・アンド・ターボ,フィリアル・アフ・マン・ディーゼル・アンド・ターボ・エスイー,ティスクランド Fuel injector for internal combustion engines
WO2008071187A1 (en) 2006-12-15 2008-06-19 Man Diesel A/S A fuel injector for an internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102013001098B3 (en) * 2013-01-23 2014-07-03 L'orange Gmbh Fuel injector for use in common-rail system in motor car, has nozzle needle comprising end section that is sealingly retained in through-hole of nozzle tip, where axial bore is extended as blind hole towards near nozzle into end section
RU2677436C1 (en) * 2016-12-13 2019-01-16 МАН Дизель энд Турбо, филиал МАН Дизель энд Турбо СЕ, Тускланд. Nozzle of the fuel valve for injection of fuel in the cylinder of the big two-tact internal combustion engine with turbocharging with compressed ignition

Also Published As

Publication number Publication date
JP2010236536A (en) 2010-10-21
EP2239451A1 (en) 2010-10-13
KR101686671B1 (en) 2016-12-14
CN101852157A (en) 2010-10-06
CN101852157B (en) 2015-06-24
JP5822249B2 (en) 2015-11-24
ATE523686T1 (en) 2011-09-15
KR20100109501A (en) 2010-10-08
DK2239451T3 (en) 2011-10-10

Similar Documents

Publication Publication Date Title
EP2239451B1 (en) A fuel injector for internal combustion engines
EP2999877B1 (en) Fuel injector
US20220082073A1 (en) Fuel injector having valve seat orifice plate with valve seat and drain and re-pressurization orifices
US6027047A (en) Magnetic valve-controlled injector for a storage fuel injection system of a multi-cylinder internal combustion engine
CN101925734B (en) Fuel injector
US20040011894A1 (en) Fuel injecton valve
EP2011993B1 (en) Dual spray injection nozzle
CN1759240A (en) The Fuelinjection nozzle that is used for internal-combustion engine
KR101822195B1 (en) A fuel injector for internal combustion engines
EP2541037B1 (en) A fuel valve for large turbocharged two stroke diesel engines
US6824085B2 (en) Fuel injector
CA2272426C (en) Injector nozzle with improved engine combustion efficiency
EP2405127B1 (en) A fuel injector for internal combustion engines
EP2218900B1 (en) Valve assembly for an injection valve and injection valve
EP1467087B1 (en) Spray pattern element and fuel injection valve with a spray pattern element
US20020050532A1 (en) Injector with a control face on the outlet side
WO1984001980A1 (en) Fuel injection valve
US20220298999A1 (en) Fuel injector
KR102615468B1 (en) Control valve device of fuel injector
JPH08247002A (en) Fuel injection nozzle
JP3901358B2 (en) Fuel injection nozzle
CN111720248A (en) Fuel injector
KR19990046719A (en) Swirl structure for high pressure fuel injector
GB2207463A (en) I.C. engine petrol injector
JP2009002212A (en) Fuel injection nozzle

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20091014

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA RS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK TR

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: SULZER MANAGEMENT AG PATENTABTEILUNG/0067

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DK

Ref legal event code: T3

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602009002507

Country of ref document: DE

Effective date: 20111103

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111207

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111208

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 523686

Country of ref document: AT

Kind code of ref document: T

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120107

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20120109

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20120611

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602009002507

Country of ref document: DE

Effective date: 20120611

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120331

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20121130

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120330

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120402

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111218

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20111207

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20130330

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130330

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: INTELLECTUAL PROPERTY SERVICES GMBH, CH

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCAR

Free format text: NEW ADDRESS: LANGFELDSTRASSE 88, 8500 FRAUENFELD (CH)

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20110907

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120330

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20090330

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DK

Payment date: 20160310

Year of fee payment: 8

REG Reference to a national code

Ref country code: CH

Ref legal event code: PFA

Owner name: WINTERTHUR GAS AND DIESEL AG, CH

Free format text: FORMER OWNER: WAERTSILAE SWITZERLAND LTD., CH

REG Reference to a national code

Ref country code: DK

Ref legal event code: EBP

Effective date: 20170331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170331

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20230314

Year of fee payment: 15

Ref country code: DE

Payment date: 20230328

Year of fee payment: 15

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20230402

Year of fee payment: 15