WO2010058788A1 - Turbocompresseur variable à buse coulissante - Google Patents

Turbocompresseur variable à buse coulissante Download PDF

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Publication number
WO2010058788A1
WO2010058788A1 PCT/JP2009/069546 JP2009069546W WO2010058788A1 WO 2010058788 A1 WO2010058788 A1 WO 2010058788A1 JP 2009069546 W JP2009069546 W JP 2009069546W WO 2010058788 A1 WO2010058788 A1 WO 2010058788A1
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WO
WIPO (PCT)
Prior art keywords
nozzle
exhaust
variable turbocharger
slide
type variable
Prior art date
Application number
PCT/JP2009/069546
Other languages
English (en)
Japanese (ja)
Inventor
哲明 小川
優和 酒井
飯野　任久
文秀 佐藤
Original Assignee
株式会社小松製作所
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 株式会社小松製作所 filed Critical 株式会社小松製作所
Priority to JP2010539237A priority Critical patent/JP4956675B2/ja
Publication of WO2010058788A1 publication Critical patent/WO2010058788A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers

Definitions

  • the present invention relates to a slide nozzle type variable turbocharger.
  • an exhaust gas purification device in the exhaust path of a diesel engine.
  • an exhaust gas purifying apparatus there is one provided with a soot filter that captures particulate matter (PM) contained in exhaust gas.
  • PM particulate matter
  • a suit filter if the amount of trapped PM exceeds a predetermined amount, clogging occurs and the filter does not function as a filter.
  • the regeneration temperature required to reliably burn the PM is usually easily obtained when the engine is operated at a medium load or higher, but becomes low at no load or low load operation. May not be reached.
  • a turbocharger that supercharges intake air by utilizing fluid energy of exhaust gas has been known.
  • a variable turbocharger is also known in which the flow area of the exhaust gas to the exhaust turbine can be made variable. Therefore, in a no-load or low-load operation that does not require supercharging, the exhaust gas opening to the exhaust turbine is intentionally reduced compared to that during normal operation, and the exhaust pressure is increased at the same time. It has been proposed to raise the exhaust gas temperature above the regeneration temperature.
  • the structure of a nozzle portion for injecting exhaust gas into an exhaust turbine is formed by a pair of exhaust introduction walls facing each other, and one exhaust introduction wall is connected to the other exhaust introduction wall
  • the gap opening area of the nozzle part of the exhaust introduction wall
  • Patent Document 1 by moving one exhaust introduction wall toward the other position to the maximum proximity position, the flow of exhaust gas is suppressed and the exhaust temperature is raised to the regeneration temperature.
  • the exhaust pressure on the upstream side of the variable turbocharger also increases, so if the exhaust pressure becomes higher than necessary, the engine exhaust valve will malfunction. It can happen. And because of the need to avoid the occurrence of abnormalities on the engine side, if the exhaust pressure rises too much before the exhaust gas temperature reaches the regeneration temperature, it must be returned to the direction of widening the opening area of the nozzle portion, and the exhaust gas The temperature cannot be raised to the regeneration temperature.
  • Patent Document 1 adopts a structure in which the exhaust gas guided to the exhaust introduction path is bypassed to the downstream side of the nozzle portion when the exhaust introduction wall is positioned at the maximum proximity position. By bypassing the exhaust gas, the exhaust gas temperature is reliably raised to the regeneration temperature while preventing the exhaust pressure on the upstream side from rising excessively.
  • the exhaust introduction wall includes a slidable nozzle ring, and the nozzle ring and the surrounding turbine housing are sealed by a seal ring provided on the inner surface of the turbine housing.
  • the nozzle ring is provided with a slit for bypassing the exhaust gas.
  • the nozzle ring slides in the forward / backward direction as long as the slit does not exceed the seal ring, so the exhaust introduction path and the downstream side of the nozzle portion are not communicated by the slit.
  • the slit moves to the nozzle part side of the seal ring, and the exhaust introduction path communicates with the downstream side of the nozzle part through the slit. And exhaust gas bypasses.
  • Patent Document 1 exhaust gas is bypassed through the sliding portion of the nozzle ring, and whether or not to bypass is determined by the position of the nozzle ring with respect to the seal ring. If there is a minute gap between the seal ring and the nozzle ring due to wear of the seal surface, exhaust gas always bypasses through the gap regardless of the position of each other. There is concern that the performance during operation will be reduced.
  • An object of the present invention is to provide a variable turbocharger that can prevent exhaust gas from bypassing during normal operation due to aging of components and the like and maintain good performance.
  • the slide nozzle type variable turbocharger of the present invention includes a nozzle portion formed by a pair of exhaust introduction walls facing each other, a nozzle ring forming one of the exhaust introduction walls, and the nozzle ring as the other exhaust.
  • a slide mechanism for advancing and retreating with respect to the introduction wall a bypass passage for communicating the nozzle portion and an exhaust outlet for discharging exhaust gas downstream of the turbine wheel; a valve member for communicating and blocking the bypass passage; and the nozzle And a pressing portion provided on the ring, wherein the bypass passage is communicated when the valve member is pressed by the pressing portion.
  • the bypass flow path is formed in an annular recess that accommodates the nozzle portion.
  • the nozzle ring is provided with a plurality of nozzle vanes along a circumferential direction, and the pressing portion protruding in the advancing direction of the nozzle vanes. .
  • the slide mechanism is provided with a support rod that is connected to the nozzle ring and advances and retracts the nozzle ring, and the valve member is disposed at a position corresponding to the support rod. It is preferable that
  • the slide mechanism is preferably driven by a hydraulic actuator.
  • the valve member may be set to be opened and closed by the pressing portion at a position where the nozzle ring is closest to the other exhaust introduction wall.
  • exhaust gas can be bypassed to the exhaust outlet side without being effectively injected from the nozzle part to the turbine wheel, and before the exhaust gas temperature reaches the regeneration temperature of the suit filter, It is possible to prevent the exhaust pressure from rising excessively.
  • the valve member opens and closes by the pressing part that moves forward and backward with the nozzle ring, there is no worry of being affected by wear of the sliding part, etc., and it is possible to prevent the exhaust gas from bypassing during steady operation of the engine, It can be maintained well. It should be noted that a large amount of exhaust gas that does not cause the turbine wheel to work flows into the suit filter while maintaining its temperature at or above the regeneration temperature, and regeneration with the suit filter can be reliably performed.
  • the exhaust gas can be guided to the bypass flow path from many positions in the circumferential direction, and the exhaust gas can be discharged efficiently.
  • the length dimension as a press part can be shortened, the intensity
  • valve member at a position corresponding to the support rod of the slide mechanism, it is possible to prevent the nozzle ring from being distorted while the valve member is being pressed by the pressing portion, and also to improve durability.
  • the position of the nozzle ring can be controlled more accurately.
  • the pressing portion can be pressed with a larger pressing force.
  • the valve member can be reliably opened and closed by the hydraulic actuator even when the bypass flow path is blocked by a large force by the valve member.
  • the bypass flow path can be closed with a large force of the valve member, there is no concern that the on-off valve will open due to the pressure of the exhaust gas, such as when exhaust gas does not want to escape through the bypass flow path.
  • the flow path can be reliably blocked.
  • the hydraulic actuator may have a configuration in which the position of the nozzle ring is feedback-controlled by a hydraulic servo mechanism, or in which feed-forward control is performed without using the hydraulic servo mechanism.
  • FIG. 1 is a perspective view of a variable turbocharger according to a first embodiment of the present invention.
  • FIG. 2 is a cross-sectional view of the variable turbocharger and a cross-sectional view taken along arrow II-II in FIG. 1.
  • FIG. 3 is a cross-sectional view showing the main part of the slide mechanism, and is a cross-sectional view taken along arrow III-III in FIG.
  • FIG. 4 is a cross-sectional view taken along arrow IV-IV in FIG. 2.
  • Sectional drawing which expands and shows the principal part of 1st Embodiment.
  • FIG. 6 is a cross-sectional view taken along arrow VI-VI in FIG. 5.
  • FIG. 7 is a cross-sectional view taken along arrow VII-VII in FIG. 6.
  • FIG. 6 is a view seen from arrows VIII-VIII in FIG. 5. The whole perspective view which shows a valve member. Sectional drawing which shows the principal part of 2nd Embodiment of this invention.
  • FIG. 1 is a perspective view of a slide nozzle type variable turbocharger 1 according to a first embodiment of the present invention
  • FIG. 2 is a cross-sectional view of the variable turbocharger 1, and a cross-section taken along arrow II-II in FIG. FIG. 1 and 2
  • the variable turbocharger 1 includes a turbine 2 on the right side in the drawing, a compressor 3 on the left side, and a hydraulic servo drive device 40 between the turbine 2 and the compressor 3. Not attached to the engine body.
  • an exhaust gas purification device (not shown) having a PM capture suit filter is provided in the middle of the exhaust path of the engine provided with the variable turbocharger 1 of the present embodiment.
  • a turbine wheel 5 is accommodated in the turbine housing 4 on the turbine 2 side, and a compressor impeller 7 is accommodated in the compressor housing 6 on the compressor 3 side.
  • a shaft 8 is provided integrally with the turbine wheel 5, and a compressor impeller 7 is attached to the tip of the shaft 8.
  • the shaft 8 is rotatably supported by the center housing 9. Therefore, the rotation of the turbine wheel 5 rotated by the exhaust gas is transmitted to the compressor impeller 7 via the shaft 8, and the intake air is compressed and supercharged by the rotation of the compressor impeller 7.
  • the turbine housing 4 is provided with a volute-shaped exhaust introduction path 11 for introducing exhaust gas from the engine body.
  • a nozzle portion 12 for ejecting exhaust gas to the turbine wheel 5 side is continuously provided in the circumferential direction, and the exhaust gas ejected from the nozzle portion 12 rotates the turbine wheel 5. It is exhausted from the exhaust outlet 13 later.
  • the nozzle portion 12 is formed by a pair of exhaust introduction walls 14 and 15 that face each other.
  • One exhaust introduction wall 14 is formed by a side surface 17 of a nozzle ring 16 having a U-shaped cross section.
  • the nozzle ring 16 is housed in an annular housing space 18 provided in the center housing 9.
  • the housing space 18 and the nozzle portion 12 side are sealed by a pair of seal rings 18A and 18B provided in the center housing 9.
  • a plurality of nozzle vanes 19 projecting toward the other exhaust introduction wall 15 side are attached to the side surface 17 of the nozzle ring 16 at equal circumferential intervals.
  • the other exhaust introduction wall 15 is formed on the shroud plate 22.
  • the shroud plate 22 is formed with a plurality of cutout holes 23 through which the nozzle vanes 19 of the nozzle ring 16 are inserted along the circumferential direction. By inserting each nozzle vane 19 through the cutout hole 23, the tip of each nozzle vane 19 is shroud.
  • the plate 22 is accommodated in an annular recess 21 on the back side. In such a structure, by moving the nozzle ring 16 forward and backward by the slide mechanism 20, the exhaust introduction wall 14 is moved closer to and away from the exhaust introduction wall 15, and the opening area as the nozzle opening degree of the nozzle portion 12 is changed. .
  • FIG. 3 is a cross-sectional view showing the main part of the slide mechanism 20, and is a cross-sectional view taken along arrow III-III in FIG. 4 is a cross-sectional view taken along arrow IV-IV in FIG. 3 and 4,
  • the slide mechanism 20 has a structure for moving the nozzle ring 16 forward and backward by rotationally driving a drive shaft 24 inserted through the lower side of the center housing 9.
  • a pair of arms 25, 25 extending in an arc shape upward is fixed at an intermediate position in the axial direction of the drive shaft 24.
  • a pin 26 protruding outward in the horizontal direction is attached to the distal end side of each arm 25, and a slider 27 is fitted into the pin 26.
  • the slider 27 is slidably fitted in a sliding groove 29 on the base end side of the support rod 28 parallel to the shaft 8 described above.
  • the tip of the support rod 28 is joined to the back side of the nozzle ring 16.
  • the arm 25 swings along the axial direction of the shaft 8, the support rod 28 moves to move the nozzle ring 16, and one exhaust introduction wall 14 becomes the other exhaust introduction wall 15. It will advance and retreat. That is, the nozzle ring 16 is closely spaced from the shroud plate 22.
  • the drive shaft 24 of the slide mechanism 20 is rotationally driven by a hydraulic servo drive device 40 via an arm 31 provided at the end thereof.
  • the hydraulic servo drive device 40 has a structure that rotates the drive shaft 24 by moving the servo piston 41 up and down.
  • the outer periphery of the servo piston 41 is provided with a sliding groove 33 orthogonal to the axial direction, and the arm 31 on the drive shaft 24 side is provided with a pin 34 protruding to the sliding groove 33 side.
  • a slider 35 is fitted into the pin 34, and the slider 35 is slidably fitted into the sliding groove 33.
  • the slide mechanism 20 is driven as described above, the support rod 28 moves, and the nozzle ring 16 advances and retreats with respect to the shroud plate 22, whereby the nozzle of the variable turbocharger 1 is moved.
  • the nozzle opening degree of the part 12 is adjusted.
  • the side surface 17 of the nozzle ring 16 is provided with a communication opening 16A (FIG. 2) that allows the nozzle portion 12 and the accommodation space 18 to communicate with each other. Due to the communication opening 16A, when the nozzle ring 16 advances and retreats, the internal pressure in the accommodation space 18 and the static pressure acting on the side surface 17 become equal, and the nozzle ring 16 slides smoothly.
  • FIG. 5 is an enlarged cross-sectional view showing a main part of the present embodiment.
  • 6 is a cross-sectional view taken along arrows VI-VI in FIG. 5
  • FIG. 7 is a cross-sectional view taken along arrows VII-VII in FIG. 6
  • FIG. 8 is a view taken from arrows VIII-VIII in FIG.
  • the illustration of the shroud plate 22 is omitted.
  • a hollow portion 51 that is recessed in the advancing direction of the nozzle ring 16 is provided in the recess 21.
  • the hollow portion 51 has a long hole shape, and a pair is provided at a position corresponding to the support rod 28 (FIG. 4).
  • a communication groove 52 continuous along the circumferential direction is provided in the inner peripheral portion of the exhaust outlet 13 of the turbine housing 4.
  • the communication groove 52 and the hollow portion 51 communicate with each other through a pair of communication holes 53.
  • the opening portion of the hollow portion 51 on the shroud plate 22 side is closed with a cover plate 54 that is curved corresponding to the shape of the recess 21.
  • the cover plate 54 is provided with a rectangular opening 55, and at least one nozzle vane 19 faces the position of the opening 55.
  • valve member 60 formed of a spring material is accommodated in the hollow portion 51. Therefore, the valve member 60 in the hollow portion 51 is also disposed at a position corresponding to the support rod 28 of the slide mechanism 20.
  • the width dimension of the valve member 60 is substantially the same as the groove width dimension of the hollow portion 51, and there is no fear of displacement in the width direction when the valve member 60 is accommodated in the hollow portion 51.
  • such a valve member 60 includes a leaf spring portion 61 formed in a V shape and an opening / closing piece 62 fixed to one piece of the leaf spring portion 61. ing.
  • a round hole 63 is provided on the tip side of the other piece of the leaf spring part 61.
  • the round hole 63 is provided at a position extending from the tip of one piece.
  • a sleeve 64 is arranged at a position corresponding to the round hole 63 so as not to interfere with one piece and the opening / closing piece 62.
  • the valve member 60 is fixed in the hollow portion 51 by a screw 65 that passes through the insertion hole 56, the sleeve 64, and the round hole 63 of the cover plate 54 and is screwed into the screw hole 57 on the back side of the hollow portion 51. .
  • a pair of flow holes 66 are provided in the other piece of the leaf spring portion 61. As shown in FIGS. 6, 7, and 9, these flow holes 66 correspond to the above-described communication holes 53 that allow the hollow portion 51 and the communication groove 52 to communicate with each other. By providing the flow hole 66, there is no concern that the leaf spring portion 61 blocks the communication hole 53, and a good communication state between the hollow portion 51 and the communication groove 52 is ensured. As described above, when the valve member 60 is accommodated and fixed in the hollow portion 51, the opening / closing piece 62 is brought into contact with the cover plate 54 while being urged by the leaf spring portion 61 and closes the opening 55.
  • a pressing portion 58 protruding along the advance direction of the nozzle ring 16 is provided at the tip of the nozzle vane 19 positioned facing the opening 55.
  • the pressing portion 58 may be provided separately from the nozzle vane 19 and may be joined to the nozzle vane 19 by an appropriate joining means, or may be manufactured integrally with the nozzle vane 19 from the beginning.
  • Such a pressing portion 58 is provided at the position where the nozzle ring 16 slides to the position closest to the exhaust introduction wall 15 as shown by the two-dot chain line position in FIGS. 5 and 6. Is pressed against the urging force of the leaf spring portion 61 (two-dot chain line in FIG. 9), and the opening 55 of the cover plate 54 is opened.
  • the nozzle portion 12 communicates with the exhaust outlet 13 side through the gap between the shroud plate 22 and the nozzle vane 19, the concave portion 21, the hollow portion 51, the communication hole 53, and the communication groove 52. Most of the exhaust gas is discharged by bypassing the nozzle portion 12 without being injected into the turbine wheel 5. That is, in this embodiment, the bypass flow path 50 of the present invention is formed including the recess 21, and the valve member 60 is disposed so as to cut off the communication of the bypass flow path 50.
  • variable turbocharger 1 during steady operation, the nozzle ring 16 slides within a range that does not reach the maximum proximity position, and the opening area of the nozzle portion 12 is adjusted according to the engine speed and load.
  • the nozzle ring 16 is slid to the maximum proximity position, and the opening area of the nozzle portion 12 is minimized. Increase pressure.
  • the pressing portion 58 provided in the predetermined nozzle vane 19 is pressed against the valve member 60 and pressed, and the opening 55 is opened to exhaust the exhaust gas into the nozzle portion. Bypass to the exhaust outlet 13 without passing through 12.
  • the valve member 60 can be pressed with a sufficient pressing force against the urging force, and the opening 55 can be reliably opened.
  • the hydraulic servo drive device 40 as a hydraulic actuator that generates a large driving force
  • the nozzle ring 16 is slid to the maximum proximity position and stopped at the proximity position, for example, the nozzle ring
  • a protruding stopper 16 ⁇ / b> B is provided on the 16 side, and it is necessary to stop the stopper 16 ⁇ / b> B by contacting the shroud plate 22.
  • the stopper 16B comes into contact with the shroud plate 22 while maintaining a large driving force by the hydraulic servo drive device 40. May occur, which may affect durability and position control of the nozzle ring 16.
  • the pressing portion 58 of the nozzle vane 19 starts to press the valve member 60, so that a part of the driving force of the hydraulic servo drive device 40 is pressed. It is used as a pressure, so that the driving force when the stopper 16B comes into contact with the shroud plate 22 can be reduced to eliminate the impact, and the durability and accuracy during position control can be improved.
  • FIG. 10 shows a second embodiment of the present invention.
  • the valve member 60 in the first embodiment includes the V-shaped leaf spring portion 61
  • the valve member 70 of the present embodiment is a flat plate made entirely of a spring material, and is attached to the cover plate 54. It is fixed and functions as a reed valve.
  • the valve member 70 is pressed by the pressing portion 58 provided on the nozzle vane 19.
  • the hollow portion 51 and the exhaust outlet 13 are directly communicated with each other through the communication hole 53.
  • the communication groove 52 is provided in the exhaust outlet 13 as in the first embodiment, and this communication is performed.
  • the communication hole 53 may be communicated with the groove 52.
  • valve members 60 and 70 are pressed by the pressing portion 58 provided in the nozzle vane 19, but even when such a pressing portion 58 is directly provided in the nozzle ring 16, Included in the invention.
  • a configuration can be applied when the nozzle vane 19 is provided not on the nozzle ring 16 side but on the shroud plate 22 side. That is, a notch hole for avoiding interference with the nozzle vane 19 is provided on the nozzle ring 16 side, and the nozzle vane 19 penetrates into the accommodating space 18 through the notch hole as the nozzle ring 16 moves back and forth. This is the case.
  • valve members 60 and 70 are not limited to the structure accommodated in the hollow portion 51 provided in the recess 21, and the hollow portion 51 is provided at an arbitrary position facing the nozzle ring 16 in the turbine housing 4.
  • the valve members 60 and 70 may be accommodated in the hollow portion 51.
  • exhaust gas flows into the recesses 21 from around all the nozzle vanes 19, the exhaust when the exhaust gas is bypassed by providing the hollow portions 51 (bypass channels 50) in the recesses 21. There is an effect that the efficiency can be improved.
  • the present invention is an engine mounted on a construction machine, a civil engineering machine, a transportation vehicle, and a railway vehicle, and can be used effectively as a variable turbocharger for an engine that is used in combination with an exhaust gas purification device having a suit filter.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)

Abstract

L'invention porte sur un turbocompresseur variable à buse coulissante (1) qui est équipé : d’une partie buse (12) formée par une paire de parois d'échappement/injection opposées (14, 15) ; d’une bague de buse (16) qui forme une paroi d'échappement/injection (14) ; d’un mécanisme de coulissement qui amène la bague de buse (16) à avancer/reculer par rapport à l'autre paroi d'échappement/injection (15) ; d’un trajet d'écoulement de dérivation (50) qui relie la partie unité buse (12) et une sortie d'échappement (13) qui laisse échapper les gaz d'échappement ; d’un élément soupape (60) qui relie/bloque le trajet d'écoulement de dérivation (50), et d’une partie de compression (58) qui est utilisée pour ouvrir/fermer l'élément soupape et qui avance/recule avec la bague de buse (16), venant en contact avec l'élément soupape (60)/se séparant de celui-ci.
PCT/JP2009/069546 2008-11-19 2009-11-18 Turbocompresseur variable à buse coulissante WO2010058788A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2010539237A JP4956675B2 (ja) 2008-11-19 2009-11-18 スライドノズル形可変ターボ過給機

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JP2008295712 2008-11-19
JP2008-295712 2008-11-19

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WO2010058788A1 true WO2010058788A1 (fr) 2010-05-27

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Cited By (4)

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Publication number Priority date Publication date Assignee Title
CN104141513A (zh) * 2013-05-09 2014-11-12 株式会社Ihi 可变喷嘴单元及可变容量式增压器
GB2555872A (en) * 2016-11-15 2018-05-16 Cummins Ltd Vane arrangement for a turbo-machine
US10508592B2 (en) * 2018-05-04 2019-12-17 Hyundai Motor Company VGT for vehicle
CN111197526A (zh) * 2018-11-20 2020-05-26 现代自动车株式会社 涡轮增压器

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JP6165564B2 (ja) * 2013-09-05 2017-07-19 三菱重工業株式会社 軸流タービン、ターボ過給機、内燃機関、及び船舶

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JP2004169703A (ja) * 2002-11-19 2004-06-17 Holset Eng Co Ltd 可変形態タービン
JP2005320970A (ja) * 2004-05-06 2005-11-17 Cummins Inc 可変幾何学的形態タービンを使用する内燃機関におけるあと処理システム用の排ガスの温度を決定する方法
JP2008185019A (ja) * 2007-01-31 2008-08-14 Komatsu Ltd 可変ターボ過給機

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004169703A (ja) * 2002-11-19 2004-06-17 Holset Eng Co Ltd 可変形態タービン
JP2005320970A (ja) * 2004-05-06 2005-11-17 Cummins Inc 可変幾何学的形態タービンを使用する内燃機関におけるあと処理システム用の排ガスの温度を決定する方法
JP2008185019A (ja) * 2007-01-31 2008-08-14 Komatsu Ltd 可変ターボ過給機

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104141513A (zh) * 2013-05-09 2014-11-12 株式会社Ihi 可变喷嘴单元及可变容量式增压器
US9702264B2 (en) 2013-05-09 2017-07-11 Ihi Corporation Variable nozzle unit and variable geometry system turbocharger
GB2555872A (en) * 2016-11-15 2018-05-16 Cummins Ltd Vane arrangement for a turbo-machine
US11441435B2 (en) 2016-11-15 2022-09-13 Cummins Ltd Vane arrangement for a turbo-machine
US10508592B2 (en) * 2018-05-04 2019-12-17 Hyundai Motor Company VGT for vehicle
CN111197526A (zh) * 2018-11-20 2020-05-26 现代自动车株式会社 涡轮增压器

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