EP2188518B1 - Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne - Google Patents

Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne Download PDF

Info

Publication number
EP2188518B1
EP2188518B1 EP08786078.9A EP08786078A EP2188518B1 EP 2188518 B1 EP2188518 B1 EP 2188518B1 EP 08786078 A EP08786078 A EP 08786078A EP 2188518 B1 EP2188518 B1 EP 2188518B1
Authority
EP
European Patent Office
Prior art keywords
combustion chamber
chamber window
ignition device
laser ignition
housing
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.)
Not-in-force
Application number
EP08786078.9A
Other languages
German (de)
English (en)
Other versions
EP2188518A1 (fr
Inventor
Martin Weinrotter
Pascal Woerner
Juergen Raimann
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 EP2188518A1 publication Critical patent/EP2188518A1/fr
Application granted granted Critical
Publication of EP2188518B1 publication Critical patent/EP2188518B1/fr
Not-in-force 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
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P23/00Other ignition
    • F02P23/04Other physical ignition means, e.g. using laser rays

Definitions

  • This laser ignition comprises an ignition laser, which projects into the combustion chamber of an internal combustion engine.
  • the ignition laser is optically pumped by a light source from a pump light source.
  • combustion chamber window is present, which is transmissive to the laser beams generated in the ignition laser.
  • This combustion chamber window must be sealingly received in a housing of the ignition laser. High demands are placed on the seal between the combustion chamber window and the housing because surface temperatures of over 600 ° C. can occur on the combustion chamber window during operation of the internal combustion engine. In addition, intermittent pressure loads of more than 250 bar are added. If a firing laser is used to ignite a gas turbine, although lower pressures prevail in the combustion chamber of the gas turbine, but the surface of the combustion chamber window can reach temperatures of up to 1,000 ° C, in any case, uncontrolled Glühzünditch must be prevented.
  • the invention is based on the object to provide an ignition laser in which the combustion chamber window and the housing are sealed so that over the entire life of the engine and the pressure prevailing in the combustion chamber of an internal combustion engine and temperatures safe and reliable sealing of the combustion chamber window and housing is guaranteed.
  • an ignition laser for an internal combustion engine comprising a laser-active solid, a combustion chamber window and a housing achieved in that the housing and the combustion chamber windows are at least indirectly connected to one another cohesively.
  • the material-tight connection of housing and combustion chamber window according to the invention ensures the required tightness even at the highest pressures and temperatures. It is important to ensure that the part of the housing, which is materially connected to the combustion chamber window, a similar thermal expansion coefficient as the combustion chamber window has. As a result, the thermal stresses are reduced and as a result, the life and reliability of the cohesive connection between the housing and the combustion chamber window increases.
  • the membrane and / or the intermediate ring it is recommended to use materials whose thermal expansion coefficient substantially corresponds to that of the combustion chamber window.
  • the material Pernifer 2198 MS from Thyssen VDM is particularly suitable for this purpose.
  • the inner sleeve, the membrane and / or the intermediate ring from a ductile material, preferably nickel or copper.
  • a ductile material preferably nickel or copper.
  • a heat-resistant material preferably made of steel of type 1.4913, has proven.
  • the cohesive connection between the housing, membrane, intermediate ring and combustion chamber window can be achieved by brazing, soldering, welding, gluing, in particular by means of ceramic and / or metallic adhesive, or vitrification.
  • solder In order to achieve a good connection between solder and combustion chamber window during soldering, it is important that the surface of the combustion chamber window is wetted. This can be done by metallizing, for example via the so-called W / Mn method, the Mo / Mn method, the vapor deposition by CVD (Chemical Vapor Deposition) or PVD (Physical Vapor Deposition), ion plating and / or active soldering. In active soldering, the solder contains at least one surface-active element, such as titanium.
  • a glass solder is possible; advantageous with a silver-glass composition.
  • Such glass solders are offered and sold, for example, by Schott and Ferro.
  • the silver acts inter alia as a ductile material, so that materials can be joined together, the coefficient of thermal expansion is different.
  • solders which have a comparatively low soldering temperature in order to reduce the thermal stresses that arise during cooling.
  • the solder must withstand the temperatures occurring during operation.
  • the joint between the housing and the combustion chamber window is preferably arranged on the side of the combustion chamber window facing away from the combustion chamber of the internal combustion engine. It is alternatively also possible to provide a joint on both sides of the combustion chamber window. This results in a redundancy of the seal and thus increased security against the loss of function of the seal.
  • combustion chamber window and the housing are not to be materially sealed but to be sealed by pressing, it has proven to be advantageous to provide a coating of a ductile material, preferably of copper, in the region of the sealing surface. If this coating consists, for example, of copper, this becomes ductile due to the high surface pressure and operating temperatures between the combustion chamber window and housing in the region of the sealing surface and thus fills the roughness of the combustion chamber window and housing in the region of the sealing surface. This ensures a durable and reliable seal.
  • a ductile material preferably of copper
  • the thickness of this coating can be between 5 .mu.m and 100 .mu.m and preferably applied by electroplating.
  • the outer sleeve has a shoulder at its end facing the combustion chamber, this shoulder partially covering the combustion chamber window.
  • the outer sleeve and the inner sleeve can be bonded together in a prestressed state.
  • the biasing force of the screw can be influenced within wide limits.
  • the methods of (Dehn) -screw calculation can be used.
  • the outer sleeve may have a region in which a controlled elongation occurs, while the inner sleeve is compressed in the region between the sealing surface and bolt thread by the biasing force. This results in a "softer" screw, which in particular has a positive effect on the sealing force even at changing temperatures.
  • FIG. 1a An internal combustion engine carries in FIG. 1a Overall, the reference numeral 10. It can be used to drive a motor vehicle, not shown.
  • the internal combustion engine 10 usually comprises a plurality of cylinders, of which in FIG. 1 only one is designated by the reference numeral 12.
  • a combustion chamber 14 of the cylinder 12 is limited by a piston 16.
  • Fuel enters the combustion chamber 14 directly through an injector 18, which is connected to a designated also as a rail fuel pressure accumulator 20.
  • the fuel-air mixture can also be formed outside the combustion chamber 14, for example in the intake manifold.
  • the present in the combustion chamber 14 fuel-air mixture 22 is ignited by means of a laser pulse 24 which is radiated from an ignition laser 26 comprehensive ignition device 27 into the combustion chamber 14.
  • the laser device 24 is fed via a light guide device 28 with a pumping light, which is provided by a pumping light source 30.
  • the pumping light source 30 is controlled by a control unit 32, which also controls the injector 18.
  • the pumping light source 30 feeds a plurality of optical fiber devices 28 for different ignition lasers 26, which are each assigned to a cylinder 12 of the internal combustion engine 10.
  • the pumping light source 30 has a plurality of individual laser light sources 340, which are connected to a pulse power supply 36.
  • a "stationary" distribution of pump light to the various laser devices 26 is realized, so that no optical distributors or the like between the pump light source 30 and the ignition lasers 26 are required.
  • the ignition laser 26 has, for example, a laser-active solid 44 with a passive Q-switching circuit 46, which forms an optical resonator together with a coupling mirror 42 and a Auskoppelapt 48.
  • the ignition laser 26 Upon application of a pumping light generated by the pumping light source 30, the ignition laser 26 generates a laser pulse 24 in a manner known per se, which is directed by a focusing optics 52 onto one in the combustion chamber 14 (FIG. FIG. 1a ) located ignition point ZP is focused.
  • the components present in the housing 38 of the ignition laser 26 are separated from the combustion chamber 14 by a combustion chamber window 58.
  • FIG. 2 is the detail X the FIG. 1b shown greatly enlarged in partial longitudinal section. From this greatly enlarged illustration, it becomes clear that the combustion chamber window 58 is adhesively bonded to an end face (without reference numeral) of the housing 38.
  • the joint is in FIG. 2 provided with the reference numeral 60.
  • the cohesive connection between the combustion chamber windows 58 and Housing 38 can be made by soldering, in particular brazing, soldering, gluing, vitrification or welding.
  • the housing 38 preferably has a thermal expansion coefficient corresponding to the coefficient of thermal expansion of the combustion chamber window 58. As a result, thermal stresses are avoided and as a result, the joint 60 relieved. At the same time, however, make sure that the housing 38 is made of a heat-resistant material. And as a result, also has a sufficient fatigue strength at the prevailing operating temperatures in the combustion chamber. Particularly advantageous in this embodiment is their low space requirement.
  • FIG. 3 is a further embodiment of a compound according to the invention between the combustion chamber window 58 and housing 38 also shown in partial longitudinal section.
  • the housing 38 is formed in two parts. It comprises an inner sleeve 62 and an outer sleeve 64.
  • the outer sleeve 64 has at a combustion chamber 14 (see FIG. 1a ) facing a paragraph 66 on.
  • the paragraph 66 has essentially two functions. First, it shields a portion of the combustion chamber window 58 from the combustion chamber and the pressures and temperatures prevailing there, so that the thermal load of the combustion chamber window 58 is reduced.
  • the combustion chamber window 58 to press against the inner sleeve 62 and thereby increase the tightness of the joint 60.
  • a female thread is provided on the outer sleeve 64, which cooperates with a corresponding bolt thread of the inner sleeve 62.
  • This thread consisting of female thread and bolt thread is indicated in its entirety by the reference numeral 68.
  • the inner sleeve can be pressed with a predetermined contact pressure on the outer sleeve and the connection can be made by welding or another cohesive method.
  • the designer By separating the housing 38 into an inner sleeve 62 and an outer sleeve 64, the designer has more degrees of freedom for functionally optimized design of the two components mentioned and the joint 60 are available.
  • the material of the outer sleeve 64 can be optimized in terms of heat resistance and fatigue strength, while the material of the inner sleeve 62 is selected so that its thermal expansion coefficient as much as possible Thermal expansion coefficient corresponds to the combustion chamber window 58. As a result, the thermal stresses are reduced and the joint 60 relieved.
  • a sealing surface 70 is formed between the shoulder 66 and the combustion chamber window, which thus represents a redundant seal, which to a certain extent precedes the joint 60 and thereby either already completely separates the combustion chamber 14 and the interior of the ignition laser 26 causes or at least reduces the temperature and pressure stress of the joint 60 and as a result, the joint 60 relieved.
  • the shoulder 66 or the combustion chamber window 58 with the area of the sealing surface 70 with a coating of a ductile material, such as copper.
  • a coating of a ductile material such as copper.
  • the combustion chamber window 58 is materially connected to the shoulder 66 of the outer sleeve 64 and the combustion chamber window 58 is pressed sealingly against the end face of the inner sleeve.
  • the thermal load in the area of the contact surface between the shoulder 66 and the combustion chamber window 58 is higher than between the combustion chamber window 58 and the inner sleeve 62.
  • a membrane 72 is provided, which is integrally connected at one end in the region of the joint 60 with the combustion chamber window 58. At its other end, it is integrally connected to the outer sleeve 64.
  • This second joint is in FIG. 4 provided with the reference numeral 74. With its side facing away from the combustion chamber window, the membrane 72 rests on the inner sleeve 62 and is additionally pressed by the pressure prevailing in the combustion chamber 14 or by the tension of the inner sleeve 62 with the outer sleeve 64 against the inner sleeve 62.
  • a gas-tight connection between the diaphragm 72 and the inner sleeve 62 is not necessary in the region of the joint 60, since the membrane is connected at its other end to the second joint 64 in a gastight manner with the outer sleeve 64.
  • the diaphragm 72 is connected in the region of the second joint 74 with the inner sleeve 62. Also, the use of the membrane 72 causes relative movements between the combustion chamber window 58 and housing 38 can be compensated without major mechanical stresses and with respect to the materials and a degree of freedom in the selection of materials of inner sleeve 62, outer sleeve 64 and membrane 72 is obtained.
  • an intermediate ring 76 is inserted between the inner sleeve 62 and the combustion chamber window 58, as shown in FIG. 6 is shown.
  • This intermediate ring 76 may be made of a different material than the inner sleeve 62 and is integrally connected in the region of the first joint 60 with the combustion chamber window 58 and in the region of the second joint 64 integrally with the inner sleeve 62. It goes without saying that in the first joint 60 and the second joint 64 not necessarily the same joining methods must be used. Rather, it is the case that at the joints 60 and 74 the respectively optimal method should be used.
  • the intermediate ring 76 may consist of several different materials, which are firmly and tightly joined together. As a result, a gradual or continuous adaptation of the (material) properties of combustion chamber window 58 and inner sleeve 62 is achieved.
  • a sealing surface 70 and a first joint 60 are provided on the combustion chamber window 58.
  • a material connection between the shoulder 66 and the combustion chamber window 58 instead of the sealing surface 70. This embodiment is not shown.
  • FIGS. 2 to 6 All embodiments according to the FIGS. 2 to 6 is common that the power flow from the combustion chamber window 58 to the housing 38 and the inner sleeve 62 always passes through the joint.
  • FIG. 7 an embodiment is shown in which the first joint 60 is not used for power transmission.
  • the membrane 72 sealingly attached to the combustion chamber window 58 in the region of the first joint 60 and on the other hand to the inner sleeve 62 in the region of the second joint 74 integrally connected thereto.
  • a recess 78 is provided on the end face of the inner surface 62, which ensures that the membrane 72 is not used in the region of the first joint 60 for power transmission between the combustion chamber window 58 and inner sleeve 62.
  • the membrane may also be sealingly connected to the outer sleeve 64 as shown in FIG. 7b is shown. Also, the joint may be disposed on the outer diameter of the combustion chamber window 58 (see FIG. 7c ).
  • FIG. 8 shown it is, as in FIG. 8 shown, also possible to clamp the combustion chamber window 58 between the shoulder 66 and the inner sleeve 62 by means of the thread 68 and thereby produce two sealing surfaces, namely the first sealing surface 70 and a second sealing surface 78.
  • This embodiment is in FIG. 8 shown. Again, may be provided on the sealing surfaces 78 and 70, a thin coating of a ductile material, such as copper.
  • inner sleeve 62, outer sleeve 64 and combustion chamber window 58 can also be braced against one another before the joining operation and connected in this braced condition. As a result, an insoluble prestressed connection can be made.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lasers (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Claims (14)

  1. Dispositif d'allumage laser pour un moteur à combustion interne (10) comprenant un corps solide à activité laser (44), une fenêtre de chambre de combustion (58) et un boîtier (38), caractérisé en ce que le boîtier (38) et la fenêtre de chambre de combustion (58) sont assemblés l'un à l'autre, au moins indirectement (60, 74) par une liaison matérielle.
  2. Dispositif d'allumage laser selon la revendication 1, caractérisé en ce que le boîtier (38) et la fenêtre de chambre de combustion (58) sont assemblés l'un à l'autre indirectement par une liaison matérielle au moyen d'une membrane (72) ou d'un anneau intermédiaire (76).
  3. Dispositif d'allumage laser selon l'une quelconque des revendications précédentes, caractérisé en ce que le boîtier (38) comprend une douille intérieure (62) et une douille extérieure (64).
  4. Dispositif d'allumage laser selon la revendication 2 ou 3, caractérisé en ce que la membrane (72) est assemblée par une liaison matérielle à la douille extérieure (64) et à la fenêtre de chambre de combustion (58).
  5. Dispositif d'allumage laser selon la revendication 2 ou 3, caractérisé en ce que la membrane (72) est assemblée par une liaison matérielle à la douille intérieure (62) et à la fenêtre de chambre de combustion (58).
  6. Dispositif d'allumage laser selon l'une quelconque des revendications 2 à 5, caractérisé en ce que la douille intérieure (62), la membrane (72) et/ou l'anneau intermédiaire (76) sont composés d'un matériau, de préférence du Pernifer 2198 MS du fabricant Thyssen VDM, dont le coefficient de dilatation thermique [1/K] correspond essentiellement au coefficient de dilatation thermique ([1/K] de la fenêtre de chambre de combustion (58).
  7. Dispositif d'allumage laser selon l'une quelconque des revendications 2 à 6, caractérisé en ce que la douille intérieure (62), la membrane (72) et/ou l'anneau intermédiaire (76) se composent d'un matériau ductile, de préférence du nickel (Ni) ou du cuivre (Cu).
  8. Dispositif d'allumage laser selon l'une quelconque des revendications 2 à 7, caractérisé en ce que la douille extérieure (64) se compose d'un matériau résistant à chaud, de préférence d'acier portant la dénomination de producteur 1.4913.
  9. Dispositif d'allumage laser selon l'une quelconque des revendications précédentes, caractérisé en ce que le boîtier (38), la membrane (72), l'anneau intermédiaire (76) et la fenêtre de chambre de combustion (58) sont assemblés les uns aux autres par brasage dur, brasage tendre, soudage, collage ou vitrification.
  10. Dispositif d'allumage laser selon l'une quelconque des revendications précédentes, caractérisé en ce qu'un point de jonction (60) entre le boîtier (38) et la fenêtre de chambre de combustion (58) se trouve sur le côté de la fenêtre de chambre de combustion (58) situé à l'opposé d'une chambre de combustion (14) du moteur à combustion interne (10).
  11. Dispositif d'allumage laser selon l'une quelconque des revendications précédentes, caractérisé en ce que le boîtier (38) et/ou la fenêtre de chambre de combustion (58) est revêtu(e), dans la région d'une face d'étanchéité (70), avec un matériau d'étanchéité, de préférence un matériau d'étanchéité ductile et résistant à la température, de préférence encore du cuivre (Cu).
  12. Dispositif d'allumage laser selon la revendication 11, caractérisé en ce que le revêtement avec un matériau d'étanchéité présente une épaisseur d'environ 5 µm à 100 µm.
  13. Dispositif d'allumage laser selon l'une quelconque des revendications 2 à 12, caractérisé en ce que la douille extérieure (64) présente à son extrémité tournée vers la chambre de combustion (14) un épaulement (66), et en ce que l'épaulement (66) recouvre partiellement la fenêtre de chambre de combustion (58).
  14. Dispositif d'allumage laser selon l'une quelconque des revendications 3 à 13, caractérisé en ce que la douille extérieure (64) présente à son extrémité située à l'opposé de la chambre de combustion (14) un filet femelle, en ce que la douille intérieure présente un filet mâle () coopérant avec le filet femelle de la douille extérieure (64), et en ce que la fenêtre de chambre de combustion (58) peut être serrée entre l'épaulement (66) de la douille extérieure (64) et la douille intérieure (62).
EP08786078.9A 2007-08-31 2008-07-11 Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne Not-in-force EP2188518B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007041528A DE102007041528A1 (de) 2007-08-31 2007-08-31 Zündeinrichtung für eine Laserzündung einer Brennkraftmaschine
PCT/EP2008/059080 WO2009027145A1 (fr) 2007-08-31 2008-07-11 Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne

Publications (2)

Publication Number Publication Date
EP2188518A1 EP2188518A1 (fr) 2010-05-26
EP2188518B1 true EP2188518B1 (fr) 2016-09-07

Family

ID=39944431

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08786078.9A Not-in-force EP2188518B1 (fr) 2007-08-31 2008-07-11 Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne

Country Status (5)

Country Link
US (1) US8312854B2 (fr)
EP (1) EP2188518B1 (fr)
JP (1) JP5328790B2 (fr)
DE (1) DE102007041528A1 (fr)
WO (1) WO2009027145A1 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011087192A1 (de) 2011-11-28 2013-05-29 Robert Bosch Gmbh Gehäuse für eine Laserzündkerze
US9742156B2 (en) 2007-08-31 2017-08-22 Robert Bosch Gmbh Laser spark plug having an improved seal between the combustion chamber window and the casing
DE102009026794A1 (de) * 2009-06-05 2010-12-09 Robert Bosch Gmbh Laserzündeinrichtung
DE102007046312A1 (de) * 2007-09-27 2009-04-02 Robert Bosch Gmbh Lasereinrichtung für die Zündeinrichtung einer Brennkraftmaschine
AT505766B1 (de) * 2007-12-19 2009-04-15 Ge Jenbacher Gmbh & Co Ohg Vorrichtung zum einkoppeln von laserlicht in einen brennraum einer brennkraftmaschine
AT506343B1 (de) * 2008-02-07 2010-12-15 Ge Jenbacher Gmbh & Co Ohg Laserzündeinrichtung
DE102008001239A1 (de) * 2008-04-17 2009-10-22 Robert Bosch Gmbh Lasereinrichtung und Betriebsverfahren hierfür
DE102008040429A1 (de) * 2008-07-15 2010-01-28 Ge Jenbacher Gmbh & Co. Ohg Strömungsschutzvorrichtung an einer Laserzündkerze zur Verbesserung des Entflammungsverhaltens
DE102008041130A1 (de) 2008-08-08 2010-02-11 Robert Bosch Gmbh Zündeinrichtung für eine Laserzündung einer Brennkraftmaschine
US8833323B2 (en) 2009-02-02 2014-09-16 Robert Bosch Gmbh Ignition laser
DE102009000958A1 (de) * 2009-02-18 2010-08-19 Robert Bosch Gmbh Laserzündkerze
DE102010029385A1 (de) * 2010-05-27 2011-12-01 Robert Bosch Gmbh Laserinduzierte Fremdzündung für eine Brennkraftmaschine
DE102010043058A1 (de) * 2010-10-28 2012-05-03 Robert Bosch Gmbh Laserzündkerze und Betriebsverfahren hierfür
DE102011079017A1 (de) * 2011-07-12 2013-01-17 Robert Bosch Gmbh Verfahren und Vorrichtung zum Betreiben einer Laserzündkerze
JP5873689B2 (ja) 2011-11-07 2016-03-01 株式会社日本自動車部品総合研究所 レーザ点火装置
DE102011087191A1 (de) 2011-11-28 2013-05-29 Robert Bosch Gmbh Gehäuse für eine Laserzündkerze und Herstellungsverfahren hierfür
DE102011087193A1 (de) 2011-11-28 2013-05-29 Robert Bosch Gmbh Gehäuse für eine Laserzündkerze
JP6224527B2 (ja) * 2014-06-02 2017-11-01 京セラ株式会社 レーザープラグ用絶縁基体およびレーザープラグ
CN106796031B (zh) 2014-08-18 2022-07-08 伍德沃德有限公司 火炬式点火器
US9574541B2 (en) 2015-05-27 2017-02-21 Princeton Optronics Inc. Compact laser ignition device for combustion engine
EP3376021B1 (fr) * 2017-03-16 2022-05-04 Ricoh Company, Ltd. Dispositif laser et moteur à combustion interne
JP7183649B2 (ja) * 2018-09-14 2022-12-06 株式会社デンソー レーザ点火プラグ
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5588074U (fr) * 1978-12-14 1980-06-18
JPS59826B2 (ja) 1978-12-26 1984-01-09 株式会社リコー 静電印刷用導電性トナ−
JPS59101585A (ja) * 1982-11-30 1984-06-12 Nippon Denso Co Ltd 内燃機関の点火装置
JP3368687B2 (ja) * 1994-09-29 2003-01-20 日産自動車株式会社 内燃機関の空燃比検出装置
AT412167B (de) * 2002-10-31 2004-10-25 Ge Jenbacher Gmbh & Co Ohg Verbrennungsmotor
FR2868146B1 (fr) * 2004-03-26 2009-01-23 Vallourec Mannesmann Oil Gas F Joint filete tubulaire resistant aux contraintes de flexion
JP2005042582A (ja) * 2003-07-25 2005-02-17 Mitsubishi Heavy Ind Ltd 集光シールガラス付き集光装置を備えたレーザ着火式エンジン
JP2005042591A (ja) * 2003-07-25 2005-02-17 Mitsubishi Heavy Ind Ltd 複数パルスレーザ照射レーザ着火式エンジン及びその運転方法
WO2005021959A1 (fr) * 2003-08-27 2005-03-10 Ge Jenbacher Gmbh & Co Ohg Moteur a combustion interne muni d'un systeme d'allumage laser
DE102004001554A1 (de) 2004-01-10 2005-08-04 Robert Bosch Gmbh Vorrichtung zum Zünden einer Brennkraftmaschine
AT501203A1 (de) * 2004-12-20 2006-07-15 Ge Jenbacher Gmbh & Co Ohg Linse für einen lasergezündeten verbrennungsmotor
WO2006125685A1 (fr) * 2005-05-27 2006-11-30 Robert Bosch Gmbh Dispositif d'allumage pour moteur a combustion interne
AT503275A1 (de) * 2006-02-20 2007-09-15 Ge Jenbacher Gmbh & Co Ohg Aufnahmevorrichtung zur befestigung eines brennraumfensters
DE102006024679A1 (de) * 2006-05-26 2007-11-29 Robert Bosch Gmbh Zündeinrichtung für eine Brennkraftmaschine
JP2007322548A (ja) * 2006-05-30 2007-12-13 Auto Network Gijutsu Kenkyusho:Kk レンズ固定構造
AT504012B1 (de) * 2006-08-09 2009-04-15 Ge Jenbacher Gmbh & Co Ohg Laserzundvorrichtung
AT506343B1 (de) * 2008-02-07 2010-12-15 Ge Jenbacher Gmbh & Co Ohg Laserzündeinrichtung

Also Published As

Publication number Publication date
US8312854B2 (en) 2012-11-20
EP2188518A1 (fr) 2010-05-26
US20100263615A1 (en) 2010-10-21
DE102007041528A1 (de) 2009-03-05
JP5328790B2 (ja) 2013-10-30
WO2009027145A1 (fr) 2009-03-05
JP2010537119A (ja) 2010-12-02

Similar Documents

Publication Publication Date Title
EP2188518B1 (fr) Dispositif d'allumage pour un allumage laser d'un moteur à combustion interne
EP2135008B1 (fr) Bougie de préchauffage
EP2392055A1 (fr) Laser d'allumage
WO2010015500A1 (fr) Dispositif d’allumage pour un allumage laser de moteur à combustion interne
EP1482168B1 (fr) Serre-flan pour injecteur de carburant
EP2358991A1 (fr) Allumage commandé, induit par laser, pour moteur à combustion interne
WO2009043608A1 (fr) Dispositif laser pour dispositif d'allumage de moteur thermique
EP2414662B1 (fr) Dispositif hydraulique de transmission ou amplification de course
EP2830803A1 (fr) Rotor de turbine à gaz d'échappement et procédé de fabrication du rotor de turbine
DE102012212264B4 (de) Verfahren zum Herstellen eines Festkörperaktuators
AT506343A1 (de) Laserzündeinrichtung
EP1745210B1 (fr) Ensemble buse et soupape d'injection
EP2025441A1 (fr) Procédé de brasage d'un premier élément métallique avec un second élément métallique utilisant en combination un assemblage mécanique; élément métallique ainsi fabriqué
EP3581907B1 (fr) Capteur de pression membrane avec un tube de support de ressort de mesure et capteur de pression situé au dessus du tube de support de ressort de mesure
EP3049666B1 (fr) Piezo-injecteur pour injection directe
EP1576279B1 (fr) Soupape d'injection de carburant
DE102015220012B4 (de) Verfahren zur Herstellung eines zweiteiligen Düsenkörpers und zweiteiliger Düsenkörper
EP2891789A1 (fr) Injecteur de carburant et procédé de fabrication d'un injecteur de carburant
DE102008032676B4 (de) Feder-/Aktuatorelement, Feder-/Aktuatoranordnung sowie Verfahren zu deren Herstellung und Steuerelement für ein Ventil
EP1803930B1 (fr) Module avec soudure convenant à haute pression
EP1849991A2 (fr) Corps métallique
EP1452729B1 (fr) Injecteur de carburant
WO2013079238A1 (fr) Bougie d'allumage laser dotée d'un dispositif d'étanchéité améliorée entre la fenêtre de chambre de combustion et l'enveloppe
DE102011087192A1 (de) Gehäuse für eine Laserzündkerze
EP3112662A1 (fr) Injecteur de carburant

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: 20100331

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 MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

DAX Request for extension of the european patent (deleted)
GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160530

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

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 MT NL NO PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 827115

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161015

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502008014616

Country of ref document: DE

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20160907

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

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: 20160907

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: 20161207

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: 20160907

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: 20160907

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: 20160907

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: 20160907

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: 20161208

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: 20160907

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: 20160907

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

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: 20160907

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: 20160907

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: 20160907

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: 20160907

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: 20170109

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: 20170107

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: 20160907

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: 20161207

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502008014616

Country of ref document: DE

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

Ref country code: IT

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: 20160907

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

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20160907

26N No opposition filed

Effective date: 20170608

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: 20160907

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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: CH

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

Effective date: 20170731

Ref country code: IE

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

Effective date: 20170711

Ref country code: LI

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

Effective date: 20170731

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20170731

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: 20170711

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

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 NON-PAYMENT OF DUE FEES

Effective date: 20170731

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 827115

Country of ref document: AT

Kind code of ref document: T

Effective date: 20170711

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: 20160907

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

Ref country code: AT

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

Effective date: 20170711

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

Ref country code: DE

Payment date: 20180928

Year of fee payment: 11

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; INVALID AB INITIO

Effective date: 20080711

Ref country code: MC

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: 20160907

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

Ref country code: CY

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

Effective date: 20160907

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

Ref country code: FR

Payment date: 20190724

Year of fee payment: 12

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

Ref country code: GB

Payment date: 20190725

Year of fee payment: 12

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 502008014616

Country of ref document: DE

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: 20160907

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

Ref country code: DE

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

Effective date: 20200201

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

Effective date: 20200711

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: 20200711

Ref country code: FR

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

Effective date: 20200731