EP2561214A2 - Procédé pour faire fonctionner une bougie d'allumage laser pour un moteur à combustion interne - Google Patents

Procédé pour faire fonctionner une bougie d'allumage laser pour un moteur à combustion interne

Info

Publication number
EP2561214A2
EP2561214A2 EP11711496A EP11711496A EP2561214A2 EP 2561214 A2 EP2561214 A2 EP 2561214A2 EP 11711496 A EP11711496 A EP 11711496A EP 11711496 A EP11711496 A EP 11711496A EP 2561214 A2 EP2561214 A2 EP 2561214A2
Authority
EP
European Patent Office
Prior art keywords
internal combustion
combustion engine
spark plug
laser
ignition
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP11711496A
Other languages
German (de)
English (en)
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 EP2561214A2 publication Critical patent/EP2561214A2/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P23/00—Other ignition
    • F02P23/04—Other physical ignition means, e.g. using laser rays
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B19/00—Engines characterised by precombustion chambers
    • F02B19/12—Engines characterised by precombustion chambers with positive ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P13/00—Sparking plugs structurally combined with other parts of internal-combustion engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P15/00—Electric spark ignition having characteristics not provided for in, or of interest apart from, groups F02P1/00 - F02P13/00 and combined with layout of ignition circuits
    • F02P15/08—Electric spark ignition having characteristics not provided for in, or of interest apart from, groups F02P1/00 - F02P13/00 and combined with layout of ignition circuits having multiple-spark ignition, i.e. ignition occurring simultaneously at different places in one engine cylinder or in two or more separate engine cylinders
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Definitions

  • the invention relates to a method according to the preamble of claim 1, and a computer program and a control and / or regulating device according to the independent claims.
  • ignition systems for internal combustion engines are known in which by means of a
  • Laser spark plug ignited in a combustion chamber existing fuel-air mixture It is important to achieve the fastest possible burn-through of the fuel-air mixture in the combustion chamber in order to achieve low fuel consumption and improved knock characteristics.
  • High-voltage ignition work it is known to additionally provide an antechamber for a faster ignition of the fuel-air mixture.
  • the problem underlying the invention is achieved by a method according to claim 1 and by a laser spark plug, a control and / or
  • the invention is based on the consideration that the use of a
  • Laser spark plug in particular with simultaneous use of an antechamber for the laser spark plug, the ignition of an internal combustion engine can improve. To ensure optimal burnout of the fuel-air mixture in one
  • Overflow holes is pressed into it. If a first ignition by the laser spark plug takes place in this state, then a flame core generated thereby is displaced in the flow direction of the mixture flowing into the pre-chamber. The enlarging flame core or the associated flame core center can therefore be moved away from the ignition location at least temporarily. Depending on the particular
  • flow conditions can again be an ignitable mixture at the ignition location of the laser spark plug.
  • the ignition location of the laser spark plug is the point at which the light energy emitted by the laser spark plug (laser ignition pulse) is bundled with a high energy density.
  • the flow conditions in the prechamber can advantageously be used to ignite more than one flame kernel, thereby igniting the mixture in the prechamber and therefore also in the main combustion chamber in a particularly rapid manner.
  • An advantage of the method according to the invention is that by means of a laser spark plug, a particularly rapid burn-through in the prechamber and in the combustion chamber of the internal combustion engine can be achieved, whereby a fuel consumption and a knock sensitivity of the
  • Internal combustion engine can be improved.
  • the operating method according to the invention with the several Laserzündimpulsen perform only in some modes of the internal combustion engine.
  • the number of laser ignition pulses and / or a time interval between at least two of the laser ignition pulses be changed between different operating cycles of the internal combustion engine. This advantageously creates a possibility of having a considerable influence on the ignition process and thus improving the operation of the laser spark plug and of the internal combustion engine without the need for additional construction work.
  • Laser ignition pulses or the resulting - due to the flow conditions in the antechamber - resulting local distance between the flame cores produced can be selected depending on the size of the prechamber. Basically, it can be beneficial if the generated
  • Flame nuclei contact one wall of the antechamber - or the flame cores each other - as late as possible to keep the burning time in the antechamber and in the main combustion chamber as short as possible. It follows that the distance of the laser ignition pulses and the flame cores thus produced should be chosen to be correspondingly large.
  • Laser ignition pulses can be carried out, for example, by changing a pump current for operating the laser spark plug or a power of a pump pulse. It can be about a Q-switch of a solid state laser of
  • Laser ignition pulses are selected in dependence on at least one of the following variables: a mixture composition of a fuel at the ignition location; a boost pressure at an inlet of a cylinder of the internal combustion engine; a gas pressure in the cylinder of the internal combustion engine; a rotational speed of the internal combustion engine; a load situation of the internal combustion engine; one
  • Internal combustion engine in particular an exhaust gas temperature and / or the air ratio lambda; a temperature of a combustion chamber; a flow rate of the mixture composition in the prechamber; a geometry of
  • a respective ignition energy of a single laser ignition pulse is preferably substantially equal to the others, wherein in each case this ignition energy must be high enough to ignite the mixture located at the ignition location.
  • a mixture composition of the fuel at the ignition location can be determined or calculated by means of a model, and a criterion can thus be obtained in order to determine a time for a subsequent ignition pulse of the laser spark plug at the ignition location.
  • a boost pressure can be determined at an inlet of a cylinder of the internal combustion engine and, depending on the determined charge pressure, a time interval between two ignition pulses can be determined.
  • a gas pressure in the cylinder of the internal combustion engine can be evaluated to determine the time interval between at least two of the ignition pulses.
  • a speed of the internal combustion engine is suitable, the ignition of the invention
  • Torque or a size of an exhaust gas of the internal combustion engine are used as a criterion to determine the time interval between at least two of the firing pulses of the laser spark plug. Likewise, this can take place as a function of a temperature of the combustion chamber.
  • Mixture composition in the prechamber a very suitable criterion to determine the time interval between two ignition pulses.
  • the associated center of the flame core changes its position within the prechamber.
  • Time distance / speed can now be a time difference between two consecutive
  • the "speed" is the speed at which a previously generated flame kernel moves away from the ignition location.
  • This speed is also significantly influenced by a flow rate of the mixture.
  • the flow rate of the mixture may be between 5 m / s and 15 m / s (meters per second).
  • the time interval between 1000 sec 333 ⁇ (microseconds).
  • a flow rate of 5 m / s to 15 m / s is particularly suitable for a safe ignition of the mixture.
  • a meaningful boundary condition may be that a mixture currently present at the ignition location should be flammable at a respective ignition point.
  • time interval between two ignition pulses may be dependent on a geometry of the prechamber or the main combustion chamber. For example, it may be useful to set the time interval between two firing pulses also of a size of the prechamber, e.g. their volume, depending. Furthermore, a location of a flame core center may be added
  • the time intervals between each two consecutive ignition pulses need not necessarily be set equal. For example, it may be useful to choose a time interval between a first and a second ignition pulse greater than a time interval between the second and a third ignition pulse, or vice versa.
  • characteristic curves and / or characteristic diagrams of a control and / or regulating device are used to determine and / or evaluate the variables and to determine the number of ignition pulses and / or their time intervals.
  • the plurality of variables influencing the ignition can advantageously be taken into account by means of maps or tables, and computing power can be saved and costs can be reduced.
  • the invention proposes that in an idle mode and / or a lean set full load operation of the engine about two to about five firing pulses are generated during a work cycle. Likewise, the invention provides that in a full-load operation of the internal combustion engine a maximum of about two ignition pulses are generated during a work cycle
  • the ignition are designed so that three firing pulses are delivered, with a maximum pressure increase can be achieved.
  • a number of three or four ignition pulses may be optimal, while in a full load operation, a single ignition pulse may be sufficient. In the latter case, a range of emerging from the antechamber ignition flares can be reduced.
  • a following second ignition pulse is generated when the flame core center generated by a preceding first ignition pulse has a first distance a in the propagation direction to a wall section of the pre-chamber and has a second distance b to the ignition point (ZP), wherein a Ratio of the first distance a to the second distance b is about 1: 5 to about 5: 1.
  • ZP ignition point
  • a Ratio of the first distance a to the second distance b is about 1: 5 to about 5: 1.
  • the prechamber preferably has a substantially cylindrical shape to a longitudinal axis.
  • a particularly simple form of the pre-chamber is indicated, by means of which the method can be carried out. As a result, manufacturing costs of the laser spark plug or the pre-chamber can be reduced.
  • An embodiment of the laser spark plug according to the invention provides that the prechamber has a substantially rotationally symmetrical shape relative to a longitudinal axis of the laser spark plug, wherein along a first axial path a wall section of the prechamber substantially has a first radius and along a second axial route a wall section of the prechamber in Essentially having a second radius.
  • a particularly suitable embodiment of the antechamber of the laser spark plug according to the invention is described. Accordingly, the prechamber essentially has two different radii, with the prechamber as a whole
  • the portions of the pre-chamber having a first radius and a second radius merge into one another continuously.
  • the first wall section of the prechamber, which faces the combustion chamber has a smaller first radius than a second wall section of the prechamber, which faces away from the combustion chamber and has a radius. It can be facing the combustion chamber
  • the pre-chamber thus has an approximately pear-shaped geometry and is particularly suitable for ignition by a plurality of time-delayed ignition pulses.
  • an embodiment of the laser spark plug according to the invention provides that a ratio of the first axial distance to the second axial distance is about 1: 2 to about 2: 1 and a ratio of the first radius to the second radius about 1: 3 to about 3: 1 is. This will be a special suitable value range for the dimensions of an antechamber of the
  • FIG. 1 shows a first sectional view through an antechamber of a laser spark plug with an ignition location and three flame cores generated with a time offset
  • Figure 2 is a second sectional view of the pre-chamber of Figure 1 with a
  • Figure 3 is a timing diagram with a pump pulse and two firing pulses of the laser spark plug.
  • FIG. 4 shows a third sectional view of the pre-chamber of FIG. 1 with two ignition locations and three flame cores produced in each case.
  • FIG. 1 shows a sectional representation of an antechamber 12 of a laser spark plug 10.
  • the prechamber 12 has a longitudinal axis 13 and is connected in a manner known per se to the laser spark plug 10 in a detachable or non-detachable manner.
  • Laser spark plug 10 is arranged in a manner also known per se at a portion of a cylinder head 14, not further explained, in the upper region of FIG.
  • the laser spark plug 10 has a combustion chamber window 16 through which laser light concentrated in the direction of an arrow 18 is emitted into the pre-chamber 12.
  • the laser light is focused on an ignition ZP.
  • Laser light can, for example, by means of a Q-switched solid-state laser generated directly in the laser spark plug 10 or the laser spark plug 10 are also supplied from a remote laser source.
  • Two lines 26a and 26b circumscribe a cone of light of the incoming laser light.
  • the pre-chamber 12 has three approximately similar overflow holes 20. Further overflow holes of the pre-chamber 12 are present, but are not visible in the present sectional view.
  • Arrows 22 enter a mixture of the combustion chamber in the interior of the prechamber 12.
  • the entering in the arrow direction of the arrow 18 in the antechamber 12 laser light is focused on the ignition ZP and can ignite a part of the mixture located in the pre-chamber 12. In this state usually continues to penetrate a mixture through the overflow holes 20 according to the arrows 22 in the pre-chamber 12 a.
  • a fluid flow is made upwards.
  • a flame kernel generated at the ignition location ZP by a laser ignition pulse 34 moves in accordance with the flow direction of the further inflowing flame
  • the flame kernel has at least initially an approximately spherical shape.
  • three flame cores 24a, 24b and 24c are shown by way of example. In this case, the drawn in the figure 1 describe
  • Flame cores 24a to 24c either a temporal propagation of a single flame kernel generated in the ignition ZP, or just as well a simultaneous arrangement of the invention according to the invention three temporally successively generated
  • FIG. 2 shows an antechamber 12 which is the same as in FIG. 1. Shown and referenced to the longitudinal axis 13 are a radius R 1 for one in the drawing of FIG. 1.
  • FIG. 2 shows a first axial distance 28 of the prechamber 12 and a radius R2 for a second axial distance 30 of the pre-chamber 12 in the drawing.
  • a ratio of the radius R1 to the radius R2 is approximately 1: 3. Shown in FIG. 2 is a moment in which a time previously generated
  • Flame core with its center of flame core 24 has already removed in the drawing up from the ignition ZP by a second distance b.
  • the flame core center 24 at this time has a first distance a from the combustion chamber window 16 of the cylinder head 14.
  • a first distance a from the combustion chamber window 16 of the cylinder head 14. In the present case is one
  • the flame kernel shown in FIG. 2 is the first of a series of two flame kernels or ignition pulses to be produced.
  • a third distance c which describes a smallest distance between the ignition point ZP and a wall 29 of the prechamber 12.
  • the third distance c can be used to obtain a reference value for the dimensioning of the distance a and thus for the time sequence of the laser ignition pulses. It is important that the flame cores reach the wall 29 of the prechamber 12 as simultaneously as possible and as late as possible and thus a faster burnout is achieved.
  • FIG. 2 shows the instant in which a second flame kernel with another (not shown) flame core center 24 can be generated at the ignition location ZP.
  • a suitable point in time can therefore be specified for the second laser ignition pulse.
  • the ratio a to b is advantageously determined taking into account the following parameters of the internal combustion engine:
  • Internal combustion engine to be used to specify a respective optimum number and optimal time intervals between the laser ignition pulses of the laser spark plug 10.
  • FIG. 3 shows a time diagram of a normalized amplitude NA of a laser pump pulse 32 and two ignition pulses 34 and 36 generated therefrom, as they are when a passively Q-switched one known per se is applied
  • a pump pulse 32 is generated, which in FIG. 3 has a time span tp. After a time t1, starting from the time t0, a first laser ignition pulse 34 is generated. After a time t2, a second laser ignition pulse 36 is generated.
  • Laser ignition pulses 34 and 36 thus have a time interval dt in the present case
  • Laser spark plug 10 (Figure 1) is caused to a multiple breakthrough. It is also possible by a dynamic change in the power of the pump pulse 32 during the period tp and the time interval dt the generated Laserzündimpulse 34 and 36 change. However, this is not shown in the drawing of Figure 3.
  • durations of the firing pulses 34 and 36 and / or the duration of the pump pulse 32 to each other may not be shown to scale.
  • the firing pulses 34 and 36 have a duration of 1 ns to 10 ns (nanoseconds)
  • the pump pulse 32 has a duration of 100 s (microseconds) to 1000 s.
  • FIG. 4 shows a mechanical one similar to FIGS. 1 and 2
  • Embodiment of the antechamber 12 the laser light irradiated by the laser spark plug 10 is bundled in such a way that two different ignition locations ZP1 and ZP2 thereof are applied thereto.
  • the timing of the ignition pulses are similar to those of Figures 1 and 2. The generated
  • the formation of two different ignition ZP1 and ZP2 ignition of the mixture located in the pre-chamber 12 can be improved by a double number of flame cores or
  • Flammenkernzentren is generated. Accordingly, a faster
  • Burning of the mixture located in the prechamber 12 advantageously takes place and the fuel consumption of the internal combustion engine and a tendency to knock are further reduced.
  • the at least one flame core is at least initially moved approximately perpendicular to the longitudinal axis 13.
  • the inventive principle of temporal multiple ignition is generally applicable to laser spark plugs without prechamber.

Landscapes

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

Abstract

L'invention concerne un procédé pour faire fonctionner une bougie d'allumage laser (10) pour un moteur à combustion interne, la bougie d'allumage laser (10) présentant une préchambre (12). Selon l'invention, la bougie d'allumage laser (10) émet au cours d'un cycle de travail du moteur à combustion interne une pluralité d'impulsions d'allumage laser (34, 36) décalées les unes des autres dans le temps vers un lieu d'allumage (ZP) situé à l'intérieur de la préchambre (12).
EP11711496A 2010-04-20 2011-03-22 Procédé pour faire fonctionner une bougie d'allumage laser pour un moteur à combustion interne Withdrawn EP2561214A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010027943A DE102010027943A1 (de) 2010-04-20 2010-04-20 Verfahren zum Betreiben einer Laserzündkerze für eine Brennkraftmaschine
PCT/EP2011/054349 WO2011131437A2 (fr) 2010-04-20 2011-03-22 Procédé pour faire fonctionner une bougie d'allumage laser pour un moteur à combustion interne

Publications (1)

Publication Number Publication Date
EP2561214A2 true EP2561214A2 (fr) 2013-02-27

Family

ID=44314517

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11711496A Withdrawn EP2561214A2 (fr) 2010-04-20 2011-03-22 Procédé pour faire fonctionner une bougie d'allumage laser pour un moteur à combustion interne

Country Status (4)

Country Link
US (1) US20130098331A1 (fr)
EP (1) EP2561214A2 (fr)
DE (1) DE102010027943A1 (fr)
WO (1) WO2011131437A2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10584639B2 (en) 2014-08-18 2020-03-10 Woodward, Inc. Torch igniter
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012223640B4 (de) * 2012-12-18 2020-07-09 Mtu Friedrichshafen Gmbh Zündeinrichtung für einen Verbrennungsmotor und Verbrennungsmotor
US9617967B2 (en) 2013-06-28 2017-04-11 Ford Global Technologies, Llc Method and system for laser ignition control
RU2531473C1 (ru) * 2013-07-17 2014-10-20 Николай Борисович Болотин Двигатель внутреннего сгорания и способ работы двигателя внутреннего сгорания
JP6478509B2 (ja) * 2014-07-31 2019-03-06 株式会社Ｓｏｋｅｎ レーザ点火装置
WO2016075358A1 (fr) * 2014-11-12 2016-05-19 Wärtsilä Finland Oy Ensemble chambre de précombustion adaptable dans une culasse d'un moteur à combustion interne, et culasse
EP3045713A1 (fr) 2015-01-16 2016-07-20 Caterpillar Energy Solutions GmbH Ensemble chambre de précombustion à allumage laser
EP3045715A1 (fr) 2015-01-16 2016-07-20 Caterpillar Energy Solutions GmbH Ensemble chambre de précombustion à allumage laser
WO2017093598A1 (fr) * 2015-12-04 2017-06-08 Wärtsilä Finland Oy Ensemble d'allumage à plasma par micro-ondes
JP2020165332A (ja) * 2019-03-28 2020-10-08 株式会社Ihi レーザ点火装置、宇宙用エンジン及び航空用エンジン
JP7150095B1 (ja) * 2021-05-17 2022-10-07 三菱電機株式会社 内燃機関の制御装置及び制御方法

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4726336A (en) * 1985-12-26 1988-02-23 Eaton Corporation UV irradiation apparatus and method for fuel pretreatment enabling hypergolic combustion
US5756924A (en) * 1995-09-28 1998-05-26 The Regents Of The University Of California Multiple laser pulse ignition method and apparatus
JP4617061B2 (ja) * 2001-05-24 2011-01-19 サウスウエスト・リサーチ・インスティチュート レーザ点火エンジンのための方法および装置
EP1329631A3 (fr) * 2002-01-22 2003-10-22 Jenbacher Zündsysteme GmbH Moteur à combustion
AT412167B (de) * 2002-10-31 2004-10-25 Ge Jenbacher Gmbh & Co Ohg Verbrennungsmotor
JP2005090381A (ja) * 2003-09-18 2005-04-07 Niigata Power Systems Co Ltd パイロット油着火ガスエンジン
FR2873763B1 (fr) * 2004-07-29 2009-06-12 Peugeot Citroen Automobiles Sa Dispositif d'allumage pour moteur a combustion interne et moteur comportant un tel dispositif
DE102006031768B4 (de) * 2006-07-10 2018-10-25 Robert Bosch Gmbh Zündeinrichtung für eine Brennkraftmaschine
DE102007015036B4 (de) * 2007-03-29 2008-11-20 Multitorch Gmbh Laserzündung für Gasgemische
US7770552B2 (en) * 2007-10-31 2010-08-10 Caterpillar Inc. Laser igniter having integral pre-combustion chamber
DE102007053414A1 (de) * 2007-11-09 2009-05-14 Robert Bosch Gmbh Verfahren und Vorrichtung zur Zündung eines Kraftstoff-Luftgemisches in einem Brennraum einer Brennkraftmaschine
JP2009127584A (ja) * 2007-11-27 2009-06-11 Nippon Soken Inc レーザ点火装置
AT506200B1 (de) * 2007-12-19 2009-09-15 Ge Jenbacher Gmbh & Co Ohg Vorrichtung zur zündung eines brennstoff/luftgemischs im brennraum einer brennkraftmaschine
AT506201B1 (de) * 2007-12-20 2009-09-15 Ge Jenbacher Gmbh & Co Ohg Laserzündeinrichtung
PL384721A1 (pl) * 2008-03-17 2009-09-28 Wiesław Olędzki Urządzenie zapłonu laserowego do silnika spalinowego w szczegółności silnika czterosuwowego, zasilanego alkoholem etylowym, metylowym oraz benzyną, naftą i benzelem(benzenem)
DE102008040429A1 (de) * 2008-07-15 2010-01-28 Ge Jenbacher Gmbh & Co. Ohg Strömungsschutzvorrichtung an einer Laserzündkerze zur Verbesserung des Entflammungsverhaltens
DE102009047021A1 (de) * 2009-11-23 2011-05-26 Robert Bosch Gmbh Laserzündkerze

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2011131437A2 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10584639B2 (en) 2014-08-18 2020-03-10 Woodward, Inc. Torch igniter
US11421601B2 (en) 2019-03-28 2022-08-23 Woodward, Inc. Second stage combustion for igniter
US11965466B2 (en) 2019-03-28 2024-04-23 Woodward, Inc. Second stage combustion for igniter

Also Published As

Publication number Publication date
DE102010027943A1 (de) 2011-10-20
US20130098331A1 (en) 2013-04-25
WO2011131437A2 (fr) 2011-10-27
WO2011131437A3 (fr) 2012-07-05

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