US20170081975A1 - Geometry for increasing torque capacity of riveted vane lever - Google Patents
Geometry for increasing torque capacity of riveted vane lever Download PDFInfo
- Publication number
- US20170081975A1 US20170081975A1 US14/858,223 US201514858223A US2017081975A1 US 20170081975 A1 US20170081975 A1 US 20170081975A1 US 201514858223 A US201514858223 A US 201514858223A US 2017081975 A1 US2017081975 A1 US 2017081975A1
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- US
- United States
- Prior art keywords
- vane
- cylindrical
- lever
- opening
- lobed
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 claims description 12
- 230000007704 transition Effects 0.000 claims description 3
- 229910003460 diamond Inorganic materials 0.000 claims description 2
- 239000010432 diamond Substances 0.000 claims description 2
- 239000000463 material Substances 0.000 description 4
- 230000001788 irregular Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
Images
Classifications
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- 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
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
-
- 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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
- F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
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- 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
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
Definitions
- the field to which the disclosure generally relates to includes vane levers and vane shafts for a turbine.
- a turbocharger may include variable turbine geometry using vanes in front of a turbine wheel.
- a number of variations may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bottom surface of the second end, and wherein at least a portion of the inner surface comprises a non-cylindrical, multi-lobed shape.
- a number of variations may include a vane pack assembly comprising: an upper vane ring; a lower vane ring; a plurality of vane components each having a vane shaft and a vane interposed between the upper vane ring and the lower vane ring; an adjustment ring surrounding a portion of the upper vane ring having a plurality of openings; and a plurality of vane levers each having a non-cylindrical, multi-lobed opening defined by an inner surface at a second end of the vane lever, wherein the non-cylindrical, multi-lobed opening surrounds a portion of the vane shaft and wherein the first end of the vane lever attaches to the adjustment ring.
- a number of variations may include a method of joining a vane lever and a vane shaft of a vane pack assembly together comprising: providing a vane lever having a non-cylindrical, multi-lobed opening defined by an inner surface; fitting the vane lever onto a vane shaft; and riveting the vane shaft to the vane lever.
- FIG. 1 illustrates a perspective view of a vane lever according to a number of variations.
- FIG. 2 illustrates a perspective view of a vane lever according to a number of variations.
- FIG. 3 illustrates a top view of a vane lever according to a number of variations.
- FIG. 4 illustrates a perspective view of a vane lever according to a number of variations.
- FIG. 5 illustrates a top view of a vane lever according to a number of variations.
- FIG. 6 illustrates a perspective view of a vane lever according to a number of variations.
- FIG. 7 illustrates a perspective view of vane lever according to a number of variations.
- FIG. 8 illustrated a perspective bottom view of a vane lever according to a number of variations.
- FIG. 9 illustrates a perspective view of a vane lever according to a number of variations.
- FIG. 10 illustrates a perspective view of a vane component according to a number of variations.
- FIG. 11 illustrates a perspective view of a vane component according to a number of variations.
- FIG. 12 illustrates a top view of a vane lever positioned onto a vane shaft according to a number of variations.
- FIG. 13 illustrates an exploded view of a vane pack assembly according to a number of variations.
- FIG. 14 illustrates a perspective view of a vane pack according to a number of variations.
- FIG. 15 illustrates a close-up perspective view of a vane pack assembly according to a number of variations.
- FIG. 16 illustrates a close-up perspective view of a vane pack assembly according to a number of variations.
- FIG. 17 illustrates a close-up perspective view of a vane pack assembly according to a number of variations.
- FIG. 18 illustrates a close-up perspective view of a vane pack assembly according to a number of variations.
- FIG. 19 illustrates a section view of a vane pack assembly according to a number of variations.
- FIG. 20 illustrates a perspective view of a vane component according to a number of variations.
- FIG. 21 illustrates a perspective view of a vane component according to a number of variations.
- a variable turbine geometry (VTG) turbocharger may be used to expand the usable flow rate range of an engine while at the same time maintaining a high level of efficiency.
- a VTG turbocharger may regulate the turbine output by changing the inflow angle and the inflow speed at the turbine inlet. The change in the inflow angle and inflow speed at the turbine inlet may be done using a vane pack assembly 30 , a variation of which is illustrated in FIG. 14 . As temperatures and aero loads of the VTG turbocharger are increased, the torque transfer capability through the vane levers 32 and the vane shafts 64 of the vane pack assembly 30 may need to be increased.
- a cylindrical (or non-cylindrical) vane shaft and non-circular, multi-lobed lever opening may be joined together using a riveting process which may form a high torque capacity joint which may withstand the temperatures and aero loads of the VTG turbocharger, as will be discussed below.
- a vane lever 32 may include a first end 34 , a second end 36 , a top surface 38 , and a bottom surface 40 .
- the vane lever 32 may also include an opening 44 which may extend through the top surface 38 and the bottom surface 40 at the second end 36 of the vane lever 32 , and which may be defined by an inner surface 52 of the vane lever 32 .
- the inner surface 52 may be constructed and arranged to accommodate a portion of the outer perimeter of the vane shaft 64 .
- the vane lever opening 44 may be any number of non-cylindrical multi-lobed shapes.
- the vane lever opening 44 may include a four sided multi-lobe interface 46 including, but not limited to, a diamond-like or square shape, through the entire interface from the top surface 38 to the bottom surface 40 , a variation of which is illustrated in FIG. 1 .
- the vane lever opening 44 may be a three sided multi-lobe interface 48 including, but not limited to, a triangular or trilobe shape, through the entire interface from the top surface 38 to the bottom surface 40 , a variation of which is illustrated in FIG. 2 .
- the vane lever opening 44 may transition from cylindrical 49 at the bottom surface 40 to non-cylindrical shapes 46 , 48 described above and hereafter at the top surface 38 , variations of which are illustrated in FIGS. 3-7 and 9 .
- the vane lever opening 44 may include a four sided multi-lobe interface 46 at the top surface 38 , transitioning to a circular interface 49 at the bottom surface 40 , variations of which are illustrated in FIGS. 3, 4, and 9 .
- the vane lever opening 44 may include a three sided multi-lobe interface 48 on the top surface 38 , transitioning to a circular interface 49 at the bottom surface 40 , variations of which are illustrated in FIGS. 5 and 6 .
- the vane lever opening 44 may include a knurled four sided multi-lobe interface 46 at the top surface 38 , transitioning to a circular interface 49 at the bottom surface 40 , a variation of which is illustrated in FIG. 7 .
- the top edge 50 of the inner surface 52 may be rounded or chamfered 54 , variations of which are illustrated in FIGS. 1-2 .
- the top edge 50 of the inner surface 52 may include a groove 56 at each of the lobes 58 , variations of which are illustrated in FIGS. 3-6 and 9 .
- the top edge 50 of the inner surface 52 may include a plurality of ridges or grooves 60 which may extend around the perimeter of the top edge 50 , a variation of which is illustrated in FIG. 7 .
- the bottom edge 51 of the inner surface 52 may also be rounded or may include a chamfer.
- the vane lever 32 may also include a tab 42 which may extend downward from the first end 34 and may be constructed and arranged to mate with an opening/cutout 90 in an adjustment ring 88 , as will be discussed hereafter.
- the tab 42 may include a cutout or grooved surface 43 , a variation of which is illustrated in FIG. 8 .
- the bottom surface 40 may include a standoff 100 which may be located between the first end 34 and the second end 36 , a variation of which is also illustrated in FIG. 8 .
- the standoff 100 may be constructed and arranged so that it may sit on the top surface 89 of the adjustment ring 88 , variations of which are illustrated in FIGS. 15 and 19 .
- the first end 34 of the vane lever 32 may be constructed and arranged as a fork end 91 having a first and second protrusion 93 .
- the fork end 91 of the vane lever 32 may be constructed and arranged to attach to an adjustment ring 88 , as will be discussed hereafter.
- vane lever configurations may include any of the above vane lever opening 44 configurations without departing from the spirit and scope of the invention.
- a vane component 62 may include a vane 66 and a vane shaft 64 . Any number of vane 66 configurations may be used.
- the vane shaft 64 may extend through the vane 66 so that the vane 66 may rotate around the vane shaft 64 .
- a first portion 68 of the vane shaft 64 may be constructed and arranged to extend within an opening 81 in a lower vane ring 80 , as will be discussed hereafter.
- a second portion 70 of the vane shaft 64 may be constructed and arranged to extend through an opening 83 in an upper vane ring 82 , as will be discussed hereafter.
- the vane shaft 64 may be cylindrical and may include a shouldered step 72 which may be constructed and arranged to fit within the vane lever opening 44 , as will be discussed hereafter.
- the shouldered step 72 may be cylindrical 74 , a variation of which is illustrated in FIG. 10 , and may be subsequently deformed to conform to a non-circular vane lever opening 44 interface, variations of which are illustrated in FIGS. 20-21 .
- the shouldered step 72 may be non-cylindrical 76 to mate with the non-cylindrical shape of the vane lever opening 44 , a variation of which is illustrated in FIG. 11 , and may be subsequently deformed to conform to the non-circular lever interface.
- a plurality of vane components 62 may be spaced circumferentially between the lower vane ring 80 and the upper vane ring 82 so that the vanes 66 are positioned between the lower vane ring 80 and the upper vane ring 82 and so that the shouldered step 72 extends above the upper vane ring 82 .
- the upper vane ring 82 may include a stepped portion 84 which may extend around the outer perimeter 86 of the upper vane ring 82 and may be constructed and arranged to accommodate a portion of an adjustment ring 88 .
- the first end 34 of the vane lever 32 may be attached to the adjustment ring 88 .
- the adjustment ring 88 may include a plurality of cutouts/openings 90 which may be constructed and arranged to accommodate a tab 42 on the vane lever 32 , a variation of which is illustrated in FIG. 15 , or a block 102 which may be located within the cutout/opening 90 and which may be constructed and arranged to accommodate the tab 42 , a variation of which is illustrated in FIG. 17 , which may secure the adjustment ring 88 to the upper vane ring 82 .
- the vane levers 32 may be positioned onto the vane shafts 64 so that the vane shaft 64 extends through the vane lever openings 44 and so that the lever tabs 42 extend through the cutouts/openings 90 (or blocks 102 ) on the adjustment ring 88 , variations of which are illustrated in FIGS. 15 and 17 .
- a vane lever 32 having a fork end 91 may be positioned between the adjustment ring 88 and the upper vane ring 82 so that the first and second protrusions 93 surround a pin 104 which may be riveted or welded to the adjustment ring 88 to attach the vane lever 32 to the adjustment ring 88 , a variation of which is illustrated in FIG. 16 .
- a combination of pins and rotating blocks may be used to secure the vane lever 32 to the adjustment ring 88 . It is noted that any number of attachment methods between the vane lever 32 and the adjustment ring 88 may be used.
- a press-fit may be used for accurate positioning if desired, a variation of which is illustrated in FIG. 12 .
- Press-fitting the vane lever 32 onto the vane shaft 64 may cause irregular radial material deformation at the top edge 50 of the inner surface 52 which may further increase torque capacity before riveting.
- external fixturing may be used to accomplish vane lever 32 to vane shaft 64 orientation for assemblies using vane shafts 64 having a cylindrical 74 shouldered step 72 .
- vane lever 32 to vane shaft 64 orientation may be accomplished using similar non-cylindrical shapes 46 , 76 on the inner surface 52 and the shouldered step 72 of the vane shaft 64 , variations of which are illustrated in FIGS. 1 and 11 .
- the vane shafts 64 may be riveted 92 to the vane levers 32 to secure the vane shafts 64 in place.
- the riveting of the vane shafts 64 may cause the material of the vane shaft 64 to form into the shape of the inner surface 52 so that the vane shaft 64 contours the shape of the inner surface 52 , variations of which are illustrated in FIGS. 20 and 21 .
- the interface between the non-cylindrical inner surface 52 and the dilated vane shaft 78 material may provide additional grip between the vane lever 32 and the vane shaft 64 which may increase the torque capacity of the joint.
- any number of combinations of the above geometries and differing edge conditions at the top of the rivet interface may be used to accommodate the riveting process. It is noted that more irregular or aggressive geometries may be used with advanced riveting processes capable of exaggerated deformations of the vane shaft material.
- Variation 1 may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bottom surface of the second end, and wherein at least a portion of the inner surface comprises a non-cylindrical, multi-lobed shape.
- Variation 2 may include a product as set forth in Variation 1 wherein the inner surface transitions from a cylindrical shape at the bottom surface to the non-cylindrical, multi-lobed shape at the top surface.
- Variation 3 may include a product as set forth in Variation 1 wherein a top edge of the inner surface is at least one of rounded or includes a groove at each of the lobes
- Variation 4 may include a product as set forth in Variation 1 wherein a top edge of the inner surface includes a plurality of ridges.
- Variation 5 may include a product as set forth in any of Variations 1-4 further comprising a vane component, wherein the vane component comprises a vane rotatably mounted to a vane shaft, wherein the vane shaft includes a stepped portion; and wherein the stepped portion extends through the non-cylindrical, multi-lobed opening of the vane lever and is attached to the vane lever.
- the vane component comprises a vane rotatably mounted to a vane shaft, wherein the vane shaft includes a stepped portion; and wherein the stepped portion extends through the non-cylindrical, multi-lobed opening of the vane lever and is attached to the vane lever.
- Variation 6 may include a product as set forth in Variation 5 wherein the stepped portion is cylindrical.
- Variation 7 may include a product as set forth in Variation 5 wherein the stepped portion is non-cylindrical.
- Variation 8 may include a product as set forth in any of Variations 5-7 wherein the vane shaft is riveted to the vane lever.
- Variation 9 may include a vane pack assembly comprising: an upper vane ring; a lower vane ring; a plurality of vane components each having a vane shaft and a vane interposed between the upper vane ring and the lower vane ring; an adjustment ring surrounding a portion of the upper vane ring having a plurality of openings; and a plurality of vane levers each having a non-cylindrical, multi-lobed opening defined by an inner surface at a second end of the vane lever, wherein the non-cylindrical, multi-lobed opening surrounds a portion of the vane shaft and wherein the first end of the vane lever attaches to the adjustment ring.
- Variation 10 may include a vane pack assembly as set forth in Variation 9 wherein a portion of the vane shaft is riveted to the vane lever and conforms to the shape of the inner surface.
- Variation 11 may include a vane pack assembly as set forth in any of Variations 9-10 wherein the non-cylindrical, multi-lobed opening is at least one of a diamond shape, a square shape, a triangular shape, or other polygon shape.
- Variation 12 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface has at least one of a rounded or a chamfered top edge.
- Variation 13 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface includes a top edge having a groove at each lobe.
- Variation 14 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface includes a top edge having a plurality of ridges.
- Variation 15 may include a vane pack assembly as set forth in any of Variations 9-14 where the vane shaft includes a stepped portion which is constructed and arranged to extend within the vane lever opening.
- Variation 16 may include a vane pack assembly as set forth in Variation 15 wherein the stepped portion is cylindrical.
- Variation 17 may include a vane pack assembly as set forth in Variation 15 wherein the stepped portion is non-cylindrical.
- Variation 18 may include a method of joining a vane lever and a vane shaft of a vane pack assembly together comprising: providing a vane lever having a non-cylindrical, multi-lobed opening defined by an inner surface; fitting the vane lever onto a vane shaft; and riveting the vane shaft to the vane lever.
- Variation 19 may include a method as set forth in Variation 18 wherein the vane shaft further comprises a stepped portion having a non-cylindrical multi-lobed shape to match the non-cylindrical, multi-lobed opening for orienting the vane lever during assembly.
- Variation 20 may include a method as set forth in any of Variations 18-19 wherein a top edge of the inner surface is at least one of rounded or grooved causing the vane shaft to conform to the shape of the inner surface when riveted.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Insertion Pins And Rivets (AREA)
Abstract
Description
- The field to which the disclosure generally relates to includes vane levers and vane shafts for a turbine.
- A turbocharger may include variable turbine geometry using vanes in front of a turbine wheel.
- A number of variations may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bottom surface of the second end, and wherein at least a portion of the inner surface comprises a non-cylindrical, multi-lobed shape.
- A number of variations may include a vane pack assembly comprising: an upper vane ring; a lower vane ring; a plurality of vane components each having a vane shaft and a vane interposed between the upper vane ring and the lower vane ring; an adjustment ring surrounding a portion of the upper vane ring having a plurality of openings; and a plurality of vane levers each having a non-cylindrical, multi-lobed opening defined by an inner surface at a second end of the vane lever, wherein the non-cylindrical, multi-lobed opening surrounds a portion of the vane shaft and wherein the first end of the vane lever attaches to the adjustment ring.
- A number of variations may include a method of joining a vane lever and a vane shaft of a vane pack assembly together comprising: providing a vane lever having a non-cylindrical, multi-lobed opening defined by an inner surface; fitting the vane lever onto a vane shaft; and riveting the vane shaft to the vane lever.
- Other illustrative variations within the scope of the invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while disclosing variations within the scope of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
- Select examples of variations within the scope of the invention will become more fully understood from the detailed description and the accompanying drawings, wherein:
-
FIG. 1 illustrates a perspective view of a vane lever according to a number of variations. -
FIG. 2 illustrates a perspective view of a vane lever according to a number of variations. -
FIG. 3 illustrates a top view of a vane lever according to a number of variations. -
FIG. 4 illustrates a perspective view of a vane lever according to a number of variations. -
FIG. 5 illustrates a top view of a vane lever according to a number of variations. -
FIG. 6 illustrates a perspective view of a vane lever according to a number of variations. -
FIG. 7 illustrates a perspective view of vane lever according to a number of variations. -
FIG. 8 illustrated a perspective bottom view of a vane lever according to a number of variations. -
FIG. 9 illustrates a perspective view of a vane lever according to a number of variations. -
FIG. 10 illustrates a perspective view of a vane component according to a number of variations. -
FIG. 11 illustrates a perspective view of a vane component according to a number of variations. -
FIG. 12 illustrates a top view of a vane lever positioned onto a vane shaft according to a number of variations. -
FIG. 13 illustrates an exploded view of a vane pack assembly according to a number of variations. -
FIG. 14 illustrates a perspective view of a vane pack according to a number of variations. -
FIG. 15 illustrates a close-up perspective view of a vane pack assembly according to a number of variations. -
FIG. 16 illustrates a close-up perspective view of a vane pack assembly according to a number of variations. -
FIG. 17 illustrates a close-up perspective view of a vane pack assembly according to a number of variations. -
FIG. 18 illustrates a close-up perspective view of a vane pack assembly according to a number of variations. -
FIG. 19 illustrates a section view of a vane pack assembly according to a number of variations. -
FIG. 20 illustrates a perspective view of a vane component according to a number of variations. -
FIG. 21 illustrates a perspective view of a vane component according to a number of variations. - The following description of the variations is merely illustrative in nature and is in no way intended to limit the scope of the invention, its application, or uses.
- A variable turbine geometry (VTG) turbocharger may be used to expand the usable flow rate range of an engine while at the same time maintaining a high level of efficiency. A VTG turbocharger may regulate the turbine output by changing the inflow angle and the inflow speed at the turbine inlet. The change in the inflow angle and inflow speed at the turbine inlet may be done using a
vane pack assembly 30, a variation of which is illustrated inFIG. 14 . As temperatures and aero loads of the VTG turbocharger are increased, the torque transfer capability through the vane levers 32 and thevane shafts 64 of thevane pack assembly 30 may need to be increased. In a number of variations, a cylindrical (or non-cylindrical) vane shaft and non-circular, multi-lobed lever opening may be joined together using a riveting process which may form a high torque capacity joint which may withstand the temperatures and aero loads of the VTG turbocharger, as will be discussed below. - Referring to
FIGS. 1-9 , in a number of variations, avane lever 32 may include afirst end 34, asecond end 36, atop surface 38, and abottom surface 40. Thevane lever 32 may also include anopening 44 which may extend through thetop surface 38 and thebottom surface 40 at thesecond end 36 of thevane lever 32, and which may be defined by aninner surface 52 of thevane lever 32. Theinner surface 52 may be constructed and arranged to accommodate a portion of the outer perimeter of thevane shaft 64. The vane lever opening 44 may be any number of non-cylindrical multi-lobed shapes. In one variation, thevane lever opening 44 may include a four sidedmulti-lobe interface 46 including, but not limited to, a diamond-like or square shape, through the entire interface from thetop surface 38 to thebottom surface 40, a variation of which is illustrated inFIG. 1 . In another variation, thevane lever opening 44 may be a three sidedmulti-lobe interface 48 including, but not limited to, a triangular or trilobe shape, through the entire interface from thetop surface 38 to thebottom surface 40, a variation of which is illustrated inFIG. 2 . In a number of variations, the vane lever opening 44 may transition from cylindrical 49 at thebottom surface 40 to 46, 48 described above and hereafter at thenon-cylindrical shapes top surface 38, variations of which are illustrated inFIGS. 3-7 and 9 . In one variation, thevane lever opening 44 may include a four sidedmulti-lobe interface 46 at thetop surface 38, transitioning to acircular interface 49 at thebottom surface 40, variations of which are illustrated inFIGS. 3, 4, and 9 . In another variation, thevane lever opening 44 may include a three sidedmulti-lobe interface 48 on thetop surface 38, transitioning to acircular interface 49 at thebottom surface 40, variations of which are illustrated inFIGS. 5 and 6 . In another variation, thevane lever opening 44 may include a knurled four sidedmulti-lobe interface 46 at thetop surface 38, transitioning to acircular interface 49 at thebottom surface 40, a variation of which is illustrated inFIG. 7 . In one variation, thetop edge 50 of theinner surface 52 may be rounded or chamfered 54, variations of which are illustrated inFIGS. 1-2 . In another variation, thetop edge 50 of theinner surface 52 may include agroove 56 at each of thelobes 58, variations of which are illustrated inFIGS. 3-6 and 9 . In yet another variation, thetop edge 50 of theinner surface 52 may include a plurality of ridges orgrooves 60 which may extend around the perimeter of thetop edge 50, a variation of which is illustrated inFIG. 7 . Referring toFIG. 8 , in a number of variations, thebottom edge 51 of theinner surface 52 may also be rounded or may include a chamfer. - Referring to
FIGS. 1-8 , in one variation, thevane lever 32 may also include atab 42 which may extend downward from thefirst end 34 and may be constructed and arranged to mate with an opening/cutout 90 in anadjustment ring 88, as will be discussed hereafter. In a number of variations, thetab 42 may include a cutout orgrooved surface 43, a variation of which is illustrated inFIG. 8 . Thebottom surface 40 may include astandoff 100 which may be located between thefirst end 34 and thesecond end 36, a variation of which is also illustrated inFIG. 8 . Thestandoff 100 may be constructed and arranged so that it may sit on thetop surface 89 of theadjustment ring 88, variations of which are illustrated inFIGS. 15 and 19 . - Referring to
FIG. 9 , in another variation, thefirst end 34 of thevane lever 32 may be constructed and arranged as afork end 91 having a first andsecond protrusion 93. Thefork end 91 of thevane lever 32 may be constructed and arranged to attach to anadjustment ring 88, as will be discussed hereafter. - It is noted that any number of vane lever configurations may include any of the above vane lever opening 44 configurations without departing from the spirit and scope of the invention.
- Referring to
FIGS. 10-11 , in a number of variations, avane component 62 may include avane 66 and avane shaft 64. Any number ofvane 66 configurations may be used. Thevane shaft 64 may extend through thevane 66 so that thevane 66 may rotate around thevane shaft 64. Afirst portion 68 of thevane shaft 64 may be constructed and arranged to extend within an opening 81 in alower vane ring 80, as will be discussed hereafter. Asecond portion 70 of thevane shaft 64 may be constructed and arranged to extend through anopening 83 in anupper vane ring 82, as will be discussed hereafter. In a number of variations, thevane shaft 64 may be cylindrical and may include a shoulderedstep 72 which may be constructed and arranged to fit within thevane lever opening 44, as will be discussed hereafter. In one variation, the shoulderedstep 72 may be cylindrical 74, a variation of which is illustrated inFIG. 10 , and may be subsequently deformed to conform to a non-circularvane lever opening 44 interface, variations of which are illustrated inFIGS. 20-21 . In another variation, the shoulderedstep 72 may be non-cylindrical 76 to mate with the non-cylindrical shape of thevane lever opening 44, a variation of which is illustrated inFIG. 11 , and may be subsequently deformed to conform to the non-circular lever interface. - Referring to
FIGS. 13-14 , in a number of variations, a plurality ofvane components 62 may be spaced circumferentially between thelower vane ring 80 and theupper vane ring 82 so that thevanes 66 are positioned between thelower vane ring 80 and theupper vane ring 82 and so that the shoulderedstep 72 extends above theupper vane ring 82. In a number of variations, theupper vane ring 82 may include a steppedportion 84 which may extend around theouter perimeter 86 of theupper vane ring 82 and may be constructed and arranged to accommodate a portion of anadjustment ring 88. - Referring to
FIGS. 15-17 , in a number of variations, thefirst end 34 of thevane lever 32 may be attached to theadjustment ring 88. In one variation, theadjustment ring 88 may include a plurality of cutouts/openings 90 which may be constructed and arranged to accommodate atab 42 on thevane lever 32, a variation of which is illustrated inFIG. 15 , or ablock 102 which may be located within the cutout/opening 90 and which may be constructed and arranged to accommodate thetab 42, a variation of which is illustrated inFIG. 17 , which may secure theadjustment ring 88 to theupper vane ring 82. In this variation, the vane levers 32 may be positioned onto thevane shafts 64 so that thevane shaft 64 extends through thevane lever openings 44 and so that thelever tabs 42 extend through the cutouts/openings 90 (or blocks 102) on theadjustment ring 88, variations of which are illustrated inFIGS. 15 and 17 . In another variation, avane lever 32 having afork end 91 may be positioned between theadjustment ring 88 and theupper vane ring 82 so that the first andsecond protrusions 93 surround apin 104 which may be riveted or welded to theadjustment ring 88 to attach thevane lever 32 to theadjustment ring 88, a variation of which is illustrated inFIG. 16 . In another variation, a combination of pins and rotating blocks may be used to secure thevane lever 32 to theadjustment ring 88. It is noted that any number of attachment methods between thevane lever 32 and theadjustment ring 88 may be used. - In one variation, a press-fit may be used for accurate positioning if desired, a variation of which is illustrated in
FIG. 12 . Press-fitting thevane lever 32 onto thevane shaft 64 may cause irregular radial material deformation at thetop edge 50 of theinner surface 52 which may further increase torque capacity before riveting. In a number of variations, external fixturing may be used to accomplishvane lever 32 tovane shaft 64 orientation for assemblies usingvane shafts 64 having a cylindrical 74 shoulderedstep 72. In another variation,vane lever 32 tovane shaft 64 orientation may be accomplished using similar 46, 76 on thenon-cylindrical shapes inner surface 52 and the shoulderedstep 72 of thevane shaft 64, variations of which are illustrated inFIGS. 1 and 11 . - Referring to
FIGS. 18-21 , in a number of variations, thevane shafts 64 may be riveted 92 to the vane levers 32 to secure thevane shafts 64 in place. The riveting of thevane shafts 64 may cause the material of thevane shaft 64 to form into the shape of theinner surface 52 so that thevane shaft 64 contours the shape of theinner surface 52, variations of which are illustrated inFIGS. 20 and 21 . The interface between the non-cylindricalinner surface 52 and the dilatedvane shaft 78 material may provide additional grip between thevane lever 32 and thevane shaft 64 which may increase the torque capacity of the joint. - Any number of combinations of the above geometries and differing edge conditions at the top of the rivet interface may be used to accommodate the riveting process. It is noted that more irregular or aggressive geometries may be used with advanced riveting processes capable of exaggerated deformations of the vane shaft material.
- The following description of variants is only illustrative of components, elements, acts, products and methods considered to be within the scope of the invention and are not in any way intended to limit such scope by what is specifically disclosed or not expressly set forth. The components, elements, acts, products and methods as described herein may be combined and rearranged other than as expressly described herein and still are considered to be within the scope of the invention.
- Variation 1 may include a product comprising: a vane lever comprising a first end; a second end; a top surface; and a bottom surface; and an opening defined by an inner surface which extends through the top surface and the bottom surface of the second end, and wherein at least a portion of the inner surface comprises a non-cylindrical, multi-lobed shape.
- Variation 2 may include a product as set forth in Variation 1 wherein the inner surface transitions from a cylindrical shape at the bottom surface to the non-cylindrical, multi-lobed shape at the top surface.
- Variation 3 may include a product as set forth in Variation 1 wherein a top edge of the inner surface is at least one of rounded or includes a groove at each of the lobes
- Variation 4 may include a product as set forth in Variation 1 wherein a top edge of the inner surface includes a plurality of ridges.
- Variation 5 may include a product as set forth in any of Variations 1-4 further comprising a vane component, wherein the vane component comprises a vane rotatably mounted to a vane shaft, wherein the vane shaft includes a stepped portion; and wherein the stepped portion extends through the non-cylindrical, multi-lobed opening of the vane lever and is attached to the vane lever.
- Variation 6 may include a product as set forth in Variation 5 wherein the stepped portion is cylindrical.
- Variation 7 may include a product as set forth in Variation 5 wherein the stepped portion is non-cylindrical.
- Variation 8 may include a product as set forth in any of Variations 5-7 wherein the vane shaft is riveted to the vane lever.
- Variation 9 may include a vane pack assembly comprising: an upper vane ring; a lower vane ring; a plurality of vane components each having a vane shaft and a vane interposed between the upper vane ring and the lower vane ring; an adjustment ring surrounding a portion of the upper vane ring having a plurality of openings; and a plurality of vane levers each having a non-cylindrical, multi-lobed opening defined by an inner surface at a second end of the vane lever, wherein the non-cylindrical, multi-lobed opening surrounds a portion of the vane shaft and wherein the first end of the vane lever attaches to the adjustment ring.
- Variation 10 may include a vane pack assembly as set forth in Variation 9 wherein a portion of the vane shaft is riveted to the vane lever and conforms to the shape of the inner surface.
- Variation 11 may include a vane pack assembly as set forth in any of Variations 9-10 wherein the non-cylindrical, multi-lobed opening is at least one of a diamond shape, a square shape, a triangular shape, or other polygon shape.
- Variation 12 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface has at least one of a rounded or a chamfered top edge.
- Variation 13 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface includes a top edge having a groove at each lobe.
- Variation 14 may include a vane pack assembly as set forth in any of Variations 9-11 wherein the inner surface includes a top edge having a plurality of ridges.
- Variation 15 may include a vane pack assembly as set forth in any of Variations 9-14 where the vane shaft includes a stepped portion which is constructed and arranged to extend within the vane lever opening.
- Variation 16 may include a vane pack assembly as set forth in Variation 15 wherein the stepped portion is cylindrical.
- Variation 17 may include a vane pack assembly as set forth in Variation 15 wherein the stepped portion is non-cylindrical.
- Variation 18 may include a method of joining a vane lever and a vane shaft of a vane pack assembly together comprising: providing a vane lever having a non-cylindrical, multi-lobed opening defined by an inner surface; fitting the vane lever onto a vane shaft; and riveting the vane shaft to the vane lever.
- Variation 19 may include a method as set forth in Variation 18 wherein the vane shaft further comprises a stepped portion having a non-cylindrical multi-lobed shape to match the non-cylindrical, multi-lobed opening for orienting the vane lever during assembly.
- Variation 20 may include a method as set forth in any of Variations 18-19 wherein a top edge of the inner surface is at least one of rounded or grooved causing the vane shaft to conform to the shape of the inner surface when riveted.
- The above description of select variations within the scope of the invention is merely illustrative in nature and, thus, variations or variants thereof are not to be regarded as a departure from the spirit and scope of the invention.
Claims (21)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/858,223 US9611751B1 (en) | 2015-09-18 | 2015-09-18 | Geometry for increasing torque capacity of riveted vane lever |
| CN201680053244.3A CN108026783B (en) | 2015-09-18 | 2016-09-12 | Product for forming a blade assembly, blade assembly and related method |
| PCT/US2016/051219 WO2017048611A1 (en) | 2015-09-18 | 2016-09-12 | Geometry for increasing torque capacity of riveted vane lever |
| JP2018513829A JP2018532067A (en) | 2015-09-18 | 2016-09-12 | Geometry to increase the torque capacity of the rivet vane lever |
| KR1020187009060A KR20180054652A (en) | 2015-09-18 | 2016-09-12 | Geometry to increase the torque capacity of the rivet vane lever |
| EP16770159.8A EP3350419B1 (en) | 2015-09-18 | 2016-09-12 | Vane lever for a variable-geometry turbocharger with geometry for increased torque capacity |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/858,223 US9611751B1 (en) | 2015-09-18 | 2015-09-18 | Geometry for increasing torque capacity of riveted vane lever |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US20170081975A1 true US20170081975A1 (en) | 2017-03-23 |
| US9611751B1 US9611751B1 (en) | 2017-04-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/858,223 Active US9611751B1 (en) | 2015-09-18 | 2015-09-18 | Geometry for increasing torque capacity of riveted vane lever |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US9611751B1 (en) |
| EP (1) | EP3350419B1 (en) |
| JP (1) | JP2018532067A (en) |
| KR (1) | KR20180054652A (en) |
| CN (1) | CN108026783B (en) |
| WO (1) | WO2017048611A1 (en) |
Cited By (7)
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|---|---|---|---|---|
| EP3473814A1 (en) * | 2017-10-17 | 2019-04-24 | United Technologies Corporation | Vane arm with tri-wedge circular pocket |
| US20190136709A1 (en) * | 2017-11-03 | 2019-05-09 | Borgwarner Inc. | Variable Turbine Geometry Vane Lever |
| JP2020067085A (en) * | 2018-10-19 | 2020-04-30 | ボーグワーナー インコーポレーテッド | Turbocharger having variable turbine geometrical shape |
| US10982558B2 (en) * | 2017-12-07 | 2021-04-20 | MTU Aero Engines AG | Guide vane connection |
| US11076530B2 (en) | 2019-03-15 | 2021-08-03 | Honda Motor Co., Ltd. | Riveted joint and method of forming the same |
| US20230043732A1 (en) * | 2021-08-05 | 2023-02-09 | MTU Aero Engines AG | Connecting device for an adjustable blade of a gas turbine and gas turbine |
| DE112020000651B4 (en) | 2019-01-31 | 2024-10-02 | Kabushiki Kaisha Toyota Jidoshokki | Variable nozzle unit |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108291564B (en) * | 2015-11-13 | 2021-04-27 | Nec平台株式会社 | Fixed Objects, Fixed Objects, Fixed Methods and Evaluation Methods |
| US20170234153A1 (en) * | 2016-02-17 | 2017-08-17 | Borgwarner Inc. | Guide Apparatus for a Turbocharger Including a Vane Lever Integrated Adjustment Ring Axial Travel Stop |
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| US4979874A (en) * | 1989-06-19 | 1990-12-25 | United Technologies Corporation | Variable van drive mechanism |
| US5092723A (en) * | 1989-06-30 | 1992-03-03 | Vsi Corporation | Engine clip bolt |
| US5492446A (en) * | 1994-12-15 | 1996-02-20 | General Electric Company | Self-aligning variable stator vane |
| US5690459A (en) * | 1996-05-29 | 1997-11-25 | Textron Inc. | Plate and riveted stud assembly |
| US6019574A (en) * | 1998-08-13 | 2000-02-01 | General Electric Company | Mismatch proof variable stator vane |
| JP2001329851A (en) * | 2000-05-19 | 2001-11-30 | Mitsubishi Heavy Ind Ltd | Variable nozzle mechanism for variable displacement turbine |
| JP3735262B2 (en) * | 2001-02-27 | 2006-01-18 | 三菱重工業株式会社 | Variable nozzle mechanism for variable capacity turbine and manufacturing method thereof |
| DE60232889D1 (en) * | 2001-08-03 | 2009-08-20 | Akita Fine Blanking Co Ltd | METHOD FOR PRODUCING A COMPONENT IN A VARIABLE GEOMETRY TURBOLADER AND A COMPONENT MADE BY THE METHOD |
| GB0312098D0 (en) * | 2003-05-27 | 2004-05-05 | Rolls Royce Plc | A variable arrangement for a turbomachine |
| DE102004048835B4 (en) * | 2004-09-30 | 2006-09-28 | Faurecia Innenraum Systeme Gmbh | Rivet or screw connection of a plastic part with another part |
| DE102004057864A1 (en) * | 2004-11-30 | 2006-06-01 | Borgwarner Inc.(N.D.Ges.D.Staates Delaware), Auburn Hills | Exhaust gas turbocharger, distributor for an exhaust gas turbocharger and blade lever for a distributor |
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| FR2921100B1 (en) * | 2007-09-13 | 2009-12-04 | Snecma | ROTATIONAL DRIVE LEVER AROUND A VARIABLE TURBOMACHINE STATOR VANE PIVOT |
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| DE112011100758B4 (en) * | 2010-03-03 | 2022-10-06 | Borgwarner Inc. | Reduced cost variable geometry turbocharger with stamped adjuster ring assembly |
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| CN102383872A (en) * | 2011-10-18 | 2012-03-21 | 湖南天雁机械有限责任公司 | Turbocharger variable nozzle with limit pin |
| DE102012201135A1 (en) * | 2012-01-26 | 2013-08-01 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Charging device i.e. exhaust gas turbocharger for combustion engine, has guide vane lever rotatably connected to guide vane pin and to vane lever pin, and adjusting ring connected to blade lever pin by positive connections |
| KR102035198B1 (en) | 2012-04-27 | 2019-11-08 | 보르그워너 인코퍼레이티드 | Exhaust-gas turbocharger |
| WO2014158455A1 (en) * | 2013-03-13 | 2014-10-02 | United Technologies Corporation | Machined vane arm of a variable vane actuation system |
-
2015
- 2015-09-18 US US14/858,223 patent/US9611751B1/en active Active
-
2016
- 2016-09-12 EP EP16770159.8A patent/EP3350419B1/en active Active
- 2016-09-12 WO PCT/US2016/051219 patent/WO2017048611A1/en not_active Ceased
- 2016-09-12 CN CN201680053244.3A patent/CN108026783B/en active Active
- 2016-09-12 JP JP2018513829A patent/JP2018532067A/en active Pending
- 2016-09-12 KR KR1020187009060A patent/KR20180054652A/en not_active Withdrawn
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3473814A1 (en) * | 2017-10-17 | 2019-04-24 | United Technologies Corporation | Vane arm with tri-wedge circular pocket |
| US10590795B2 (en) * | 2017-10-17 | 2020-03-17 | United Technologies Corporation | Vane arm with tri-wedge circular pocket |
| US20190136709A1 (en) * | 2017-11-03 | 2019-05-09 | Borgwarner Inc. | Variable Turbine Geometry Vane Lever |
| WO2019090018A1 (en) * | 2017-11-03 | 2019-05-09 | Borgwarner Inc. | Variable turbine geometry vane lever |
| US10619508B2 (en) * | 2017-11-03 | 2020-04-14 | Borgwarner, Inc. | Variable turbine geometry vane lever |
| US10982558B2 (en) * | 2017-12-07 | 2021-04-20 | MTU Aero Engines AG | Guide vane connection |
| JP2020067085A (en) * | 2018-10-19 | 2020-04-30 | ボーグワーナー インコーポレーテッド | Turbocharger having variable turbine geometrical shape |
| DE112020000651B4 (en) | 2019-01-31 | 2024-10-02 | Kabushiki Kaisha Toyota Jidoshokki | Variable nozzle unit |
| US11076530B2 (en) | 2019-03-15 | 2021-08-03 | Honda Motor Co., Ltd. | Riveted joint and method of forming the same |
| US20230043732A1 (en) * | 2021-08-05 | 2023-02-09 | MTU Aero Engines AG | Connecting device for an adjustable blade of a gas turbine and gas turbine |
Also Published As
| Publication number | Publication date |
|---|---|
| KR20180054652A (en) | 2018-05-24 |
| CN108026783B (en) | 2021-01-05 |
| EP3350419A1 (en) | 2018-07-25 |
| US9611751B1 (en) | 2017-04-04 |
| EP3350419B1 (en) | 2022-09-07 |
| WO2017048611A1 (en) | 2017-03-23 |
| CN108026783A (en) | 2018-05-11 |
| JP2018532067A (en) | 2018-11-01 |
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