Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16H—GEARING
  • F16H41/00—Rotary fluid gearing of the hydrokinetic type
  • F16H41/24—Details
  • F16H41/26—Shape of runner blades or channels with respect to function
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
  • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
  • F04D29/00—Details, component parts, or accessories
  • F04D29/40—Casings; Connections of working fluid
  • F04D29/52—Casings; Connections of working fluid for axial pumps
  • F04D29/54—Fluid-guiding means, e.g. diffusers
  • F04D29/541—Specially adapted for elastic fluid pumps
  • F04D29/542—Bladed diffusers
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
  • F16H—GEARING
  • F16H41/00—Rotary fluid gearing of the hydrokinetic type
  • F16H41/24—Details
  • F16H41/28—Details with respect to manufacture, e.g. blade attachment

Definitions

• the invention relates to improvements in a device for transmitting power between a rotary drive unit (for example the motor of a motor vehicle) and a rotationally driven unit (for example the automatic transmission in the motor vehicle).
• a rotary drive unit for example the motor of a motor vehicle
• a rotationally driven unit for example the automatic transmission in the motor vehicle.
• the invention relates to a stator blade with two separately formed axial segments for a torque converter.
• the stator has stamped axial halves, and the segments are formed as an integral part of the respective halves.
• One-piece blades in stators are known.
• Two-piece stator blades are also known, as described, for example, in US Patent Application No. US 2004/023575 A1 (Shin).
• Shin the blade segments of Shin are separated from each other in the radial direction. That is, one segment is connected to an outer periphery of the stator, and the other segment is connected to an inner circumference of the stator.
• the influence on the liquid flow through the blades is essentially limited to the flow along radial planes.
• the present invention generally includes a stator for a stator in a torque converter that includes a first vane segment connected to inner and outer circumferential portions of the stator and a second vane segment formed separately from the first vane segment and connected to the inner and outer circumferential portions.
• the first and second vane segments are in contact, the first and second vane segments include corresponding edges, and the first and second vane segments contact each other at the respective edges, or at least one of the corresponding first edges tapered wedge-shaped.
• the first and second blade segments include respective surfaces, and the corresponding surfaces at least partially overlap, or the first and second blade segments are offset from one another circumferentially.
• the first or second blade segments are at least partially folded, the blade is stamped, or the blade is cast.
• the stator includes performance characteristics
• the first and second blade segments are located in respective arrays, and the corresponding arrays are selected to vary the performance characteristics.
• performance characteristics such as torque ratio, efficiency, and power, and, among other things, arrangements such as axial location, radial location, and circumferential location are selected.
• first and second blade segments are circumferentially aligned, and the stator includes an alignment member that is operatively arranged to control alignment about the circumference.
• the torque converter includes a fluid, and the alignment member is arranged to control alignment in response to the pressure of the fluid on the blade.
• the stator includes a first axial half and a second axial half, the first and second axial halves are formed separately and fixedly connected together, the first vane segment is connected to the first axial half, and the second vane segment is connected to the first axial half second axial half connected.
• first vane segment is formed as an integral part of the first axial half
• second vane segment is formed as an integral part of the second axial half.
• the stator includes a clutch, and the first and second axial halves are formed to form first and second axial terminations of the clutch, respectively.
• the present invention generally includes a stator for a stator in a torque converter including a first vane segment formed integrally with the inner and outer peripheral portions of the stator and including a second vane segment separate from the first vane segment Blade segment and formed as an integral part together with the inner and outer peripheral portions.
• the present invention generally includes a stator for a stator in a torque converter including a first vane segment integrally formed with a first axial half of the stator and connected to first inner and outer peripheral portions of the first axial half, and which includes a second vane segment formed separately from the first vane segment and integral with a second axial half of the stator and connected to second inner and outer peripheral portions of the second axial half.
• the first and second axial halves are formed separately from each other and firmly connected.
• a general object of the present invention is to provide a blade for a stator that can be formed in a wide variety of arrangements.
• Another object of the present invention is to provide a blade for a stator that can be formed from axially separated segments.
• Yet another object of the present invention is to provide a multi-segment blade for a variable pitch stator between the segments.
• Fig. 1 is a front perspective view of a stator with a two-part blade according to the present invention
• Fig. 2 is an exploded front view of the stator in Fig. 1;
• Fig. 3 is a front view of the stator in Fig. 1;
• Fig. 4 is a side cross-sectional view of the stator in Fig. 3 taken along section line 4-4 in Fig. 3;
• Fig. 5 is a cross-sectional view of the stator in Fig. 4 from the rear taken along section line 5-5 in Fig. 4;
• FIGS 6 to 9 are partial cross-sectional views of stators with blades according to the present invention showing arrangements of respective stators and blades;
• FIGS 10 to 17 are plan views of blades in accordance with the present invention showing various arrangements of the blades
• Fig. 18A is a perspective view of a cylindrical coordinate system illustrating the spatial notation used in the present application.
• Fig. 18B is a perspective view of an object in the cylindrical coordinate system of Fig. 18A, illustrating the notation used in the present invention.
• Fig. 18A is a perspective view of a cylindrical coordinate system 280 illustrating the spatial notation used in the present application.
• the present invention will be described, at least in part, in connection with a cylindrical coordinate system.
• the system 280 has a longitudinal axis 281 which serves as a reference for the following spatial and directional designations.
• the adjectives "axial,”"radial,” and “circumferential” refer to an orientation parallel to axis 281, a radius 282 (which is perpendicular to axis 281), and a circumference 283, respectively.
• the adjectives "axial,”"radial,” and “ Circumferential also concern alignment parallel to corresponding planes.
• the objects 284, 285 and 286 serve to clarify the arrangement of the different planes.
• the surface 287 of the object 284 forms an axial plane. That is, the axis 281 forms a line along the surface.
• the surface 288 of the object 285 forms a radial plane. That is, the radius 282 is along a line the area.
• the surface 289 of the object 286 forms a peripheral surface. That is, the periphery 283 forms a line along the surface.
• an axial displacement or arrangement parallel to the axis 281 occurs, that a radial displacement or arrangement is parallel to the radius 282 and that a displacement or arrangement on the circumference parallel to the circumference 283 takes place.
• a rotation takes place about the axis 281.
• adverbs "axial,” “radial,” and “circumferential” refer to an orientation parallel to axis 281, radius 282, and circumference 284, respectively.
• the adverbs "axial,” “radial,” and “circumferential” also refer to a parallel alignment to corresponding planes.
• Fig. 18B is a perspective view of the object 290 in the cylindrical coordinate system 280 of Fig. 18A, illustrating the spatial notation used in the present application.
• the cylindrical object 290 represents a cylindrical object in a cylindrical coordinate system and should not be construed as limiting the present invention in any way.
• the object 290 includes an axial surface 291, a radial surface 292, and a peripheral surface 293.
• the surface 291 is part of an axial plane
• the surface 292 is part of a radial plane
• the surface 293 is part of a peripheral surface.
• FIG. 1 is a front perspective view of a stator having a two-piece blade 10 according to the present invention.
• FIG. 2 is an exploded front view of the stator in FIG. 1.
• FIG. 2 is an exploded front view of the stator in FIG. 1.
• FIG. 3 is a front view of the stator in FIG. 1.
• FIG. 4 is a side cross-sectional view of the stator in FIG. 3 taken along section line A-4 in FIG. 3.
• FIG. 4 is a side cross-sectional view of the stator in FIG. 3 taken along section line A-4 in FIG. 3.
• Fig. 5 is a cross-sectional view of the stator in Fig. 4 from the rear along the section line 5-5 in Fig. 4.
• blades 10 are shown.
• each blade 10 includes blade segments 14 and 16.
• Segments 14 and 16 are formed separately. That is, the segments 14 and 16 are individual parts.
• the stator 12 with The separate parts or segments may be interconnected, coupled, brought into contact, aligned or arranged in the manner described below
• the segments 14 and 16 are respectively is connected to an inner peripheral portion 18 and an outer peripheral portion 20 of the stator 12. That is, the segments are continuous between the portions 18 and 20.
• each blade 10 is shown with corresponding segments 14 and 16. It should be understood, however, that the present invention is not limited to a one to one ratio between segments 14 and 16. That is, the blades 10 may be formed with different numbers of segments 14 and 16. For example, a certain number of vanes 16 may be formed with both the segments 14 and the segments 16, a different number of vanes excluding segments 14, and still another number of vanes with segments 16 alone.
• the segments 14 and 16 may be arranged in a variety of ways to form the blade 10. For example, in some aspects, the segments contact each other along the lines 17 shown in FIGS. 1-3. For example, the segments 14 and 16 contact each other along radial edges 22 and 24. In some aspects, one or both edges 22 and 24 are wedge-shaped tapered, as described below. Segments 14 and 16 include radial surfaces 26 and 28, and 30 and 32, respectively. In some aspects, corresponding radial surfaces of segments 14 and 16 at least partially overlap, as described below. According to some aspects (not shown), the segments 14 and 16 are not circumferentially aligned, as described below.
• stators may be considered from the point of view of performance characteristics, including, but not limited to, torque ratio, efficiency, and performance.
• these characteristics are influenced by the blades of the stator, for example by the arrangement of the blades.
• corresponding arrangements of blades 10 and blade segments 14 and 16 can be selected.
• the arrangement of the blades and blade segments can be a - o -
• the stator 12 includes halves 36 and 38, for example, two axially separate halves as disclosed in commonly assigned U.S. Patent Application entitled “Integral Stator and One-Way Clutch” by George et al
• halves is meant that the structure of the stator, in particular the structure to which the blades are connected, is essentially formed by halves 36 and 38.
• the halves 36 and 38 can In other words, the halves 36 and 38 are interconnected along a radial plane with respect to the axis 34.
• the halves are each formed of individual parts, that is, the halves are formed separately 14 are connected to the half 36, and the vane segments 16 are connected to the half 38.
• the segments are integral with the half 36 and the blade segments 16 are integral with the half 38.
• the segments 14 and half 36 are formed of one piece of material.
• the halves are connected together and fixed in the axial direction. That is, the halves are connected in any way with each other and do not move in the axial direction against each other. In some aspects, the halves are firmly connected. That is, the halves shift neither in the axial nor in the direction of rotation against each other. In some aspects, the halves are arranged to translate in the direction of rotation, as described below. In FIGS. 1 to 4, fastening elements 40 and 42 are used to connect the halves. It should be understood, however, that other means may be used to join the halves, such as those described below, including, but not limited to, rivets, folded tongues, welds, adhesives, and beads.
• FIGS. 6 to 9 are partial cross-sectional views of stators with blades according to the present invention showing arrangements of respective stators and blades. The following description will be seen in conjunction with FIGS. 1-9. - -
• halves 36 and 38 are arranged to form part of a one-way clutch 44 described in commonly owned U.S. Patent Application entitled “Stator and One-Way Clutch Assembly for a Torque Converter” by Hemphill et
• the stators 12A-12D include a one-way clutch 44 having an inner race 46, rollers 48, and an outer race 50 with the halves 36 and 38 arranged such that in other words, the shutters 52 and 54 hold the races and the rollers of the clutch together in the axial direction
• the use of other one-way clutches in the stators in mind and Scope of the claimed invention are included.
• the blades 10, segments 14 and 16, and halves 26 and 38 are not limited to any particular arrangement, shape, size, orientation or connection.
• the axial orientation refers to the radial line 58 (which is shown only in FIG. 9, but also applies to the other figures), which passes in the axial direction through the center of the coupling 44.
• corresponding halves of the stators 12 are attached to the inner peripheral portion 62 and / or the outer peripheral portion 64.
• the halves 36A / 38A and 36D / 38D are formed so that the portions 62A and 62D are out of center in the axial direction.
• the halves 36A and 38A axially contact along the line 66 axially outward of the center. It follows that the axial dimension 68 is greater than the axial dimension 70, while maintaining a general axial alignment of the blades 10 on the line 58. This arrangement is useful for those aspects where it is desired to emphasize aspects of the front parts of the blades 10, for example to increase the area of the front part.
• the line 72 is substantially aligned with the line 58 in the axial direction, and the dimension 74 is also larger than the dimension 76, so that the front aspects of the blades 10 are more emphasized.
• FIGS. 7 and 8 the halves in the corresponding ring of the stator, that is, in the radial region in which the blades are located, are separated from one another in the axial direction. Ring 78 is shown in FIG. 1 for comparison.
• the regions 62B and 64B and 62C and 64C are substantially aligned with the line 58 in the axial direction.
• One effect of the arrangement shown in Figures 7 and 8 is that the vane segments, for example 14B and 16C, are connected at such locations to the respective halves located axially in the middle of the respective segments.
• the axial dimensions 80 and 82 are substantially the same for the segment 14B.
• the torque forces acting on the segments can be reduced by adjusting the distance between the connection points of the segments and corresponding edges of the segments, for example the distance 80 between the point 84 and the edge 86 of the segment 14B, is reduced.
• the segments 14C and 16C taper in the radial direction.
• an axial dimension 88 of the segment 14C near the region 64C is greater than near the region 62C.
• the dimension 88 near the region 62C may be greater than near the region 64C.
• Figures 6, 7 and 9 show a crimp connection, tongue or bead, while in Figure 8 rivets 90 are used.
• other means may be used, including but not limited to welds.
• FIGS. 10 to 17 are plan views of blades according to the present invention showing various arrangements of the blades. The following description will be seen in conjunction with FIGS. 1-17.
• Fig. 10 shows the blade 10 with the segments 14 and 16 in axial Direction along the line 17 are interconnected. This arrangement corresponds to the illustration in Figures 1 to 5.
• Figures 11 and 12 show the segments 14 and 16, which are offset from each other over the circumference. From FIGS. 11 and 12, it can be seen that the segment 16 can be displaced beyond the circumference of the segment 14 in any direction beyond the circumference. It should be understood that the offset may be related to the segment 16 as a reference.
• the bucket 10 is not on one limited amount of offset 100 between segments across the scope.
• Figures 13 and 14 show how the segments 14 and 16 are interconnected by an overlap.
• Fig. 13 shows a double overlap. That is, the portion 102 of the segment 14 and the portion 104 of the segment 16 are machined or deformed.
• Fig. 14 shows a simple overlap. That is, only the portion 106 of the segment 16 is machined or deformed. It should be understood that the overlap shown in Figs. 13 and 14 may be in the reverse direction, for example, a simple overlap may be formed by processing the segment 14.
• the blade 10 is not limited to any particular extent or arrangement of overlap.
• Fig. 15 shows segments 14 and 16 with wedge-shaped bevelled edges 108 and 110, respectively. It should be understood that other arrangements of segments may have wedge-shaped bevelled edges. For example, in Figures 11 or 14, segment 14 or 16 may be tapered in a wedge shape. Further, in Fig. 15, other combinations of wedge-shaped bevelled edges are possible. For example, the edges 112 or 114 may be tapered in a wedge shape.
• the bucket 10 is not limited to a particular type of bevel or a particular combination of wedge-shaped bevelled edges.
• Fig. 16 shows a blade 10 with at least partially folded segments 14 and 16.
• the leading edges 116 and 118 of the segments 14 and 16, respectively, have been folded over.
• the blade 10 is not limited to any particular type, degree, or arrangement of folding.
• dimensions 120 and 122 may be varied.
• only one of the segments 14 or 16 in the blade 10 may be folded while the other segment remains unfolded.
• Fig. 17 shows substantially teardrop-shaped segments formed by casting or molding. Such segments may be cast in a variety of sizes, shapes, and configurations to produce surfaces 124 having, for example, a desired curvature and surface property.
• the offset shown in FIGS. 11 and 12 may be adjusted circumferentially.
• at least parts of either Halves 36 and 38 or both halves over the circumference be adjusted.
• the setting may not be automatic.
• the location of halves 36 or 38 relative to each other in FIGS. 1 and 2 may be selected circumferentially, and thus the orientation of segments 14 and 16 in vanes 10 circumferentially, by adjusting one or both halves to the desired orientation rotated and then fastened using fasteners 40 and 42.
• the adjustment is made automatically. That is, the stator 12 includes an automatic alignment member or adjuster for at least a portion of one or both halves 36 and 38.
• the setting for the halves will be described in the following discussion, however, it should be understood that this setting is only for a part of the corresponding half is possible.
• the adjuster controls the rotation of the halves (to change the offset of the segments 14 and 16 in the blades 10 circumferentially) in response to selected control parameters.
• the device is of a mechanical nature, for example in the form of a resistive element, which provides "active" resistance to set a certain offset in the stator under certain operating conditions.
• a resistive element for example, a spring can be used, whereby the degree of compression of the spring changes depending on the fluid pressure on the blades of the stator
• any resistance device known in the art may be used.
• an electromechanical alignment element is used.
• halves 36 and 38 connect electrical actuators or electromechanical devices that rotate the halves in response to control signals.
• the control signals may be generated by any means known in the art, including, but not limited to, sensors for measuring parameters in the stator, such as fluid pressure or fluid flow, or sensors for monitoring operational parameters ⁇ o -
• Blades 10, segments 14 and 16, and halves 36 and 38 may be made using any means known in the art.
• the blades, segments or halves may be formed by stamping or casting. Several production tools can be used together.
• stamped blades 10 may be used in conjunction with casting blades.

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• Engineering & Computer Science (AREA)
• General Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Structures Of Non-Positive Displacement Pumps (AREA)
• Iron Core Of Rotating Electric Machines (AREA)
• Turbine Rotor Nozzle Sealing (AREA)
• Manufacture Of Motors, Generators (AREA)

Priority Applications (5)

Applications Claiming Priority (2)

Publications (1)

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Family Applications (1)

Country Status (7)

Cited By (2)

Families Citing this family (23)

Citations (10)

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• 2007
  • 2007-02-23 JP JP2009501831A patent/JP5286464B2/ja not_active Expired - Fee Related
  • 2007-02-23 WO PCT/DE2007/000354 patent/WO2007110019A1/de not_active Ceased
  • 2007-02-23 AT AT07711207T patent/ATE509217T1/de active
  • 2007-02-23 EP EP07711207A patent/EP2002151B1/de not_active Not-in-force
  • 2007-02-23 DE DE112007000496T patent/DE112007000496A5/de not_active Withdrawn
  • 2007-02-23 CN CN2007800106057A patent/CN101410654B/zh not_active Expired - Fee Related
  • 2007-03-23 US US11/728,066 patent/US7850420B2/en not_active Expired - Fee Related

Patent Citations (10)

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