JP2012122527A - Cardan universal joint - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a Cardan universal joint including a thrust piece capable of giving an appropriate preload in the thrust direction by absorbing a dimensional error and allowing a large thrust load applied to a shaft part of a cross shaft to be supported.SOLUTION: The shaft center of a low-rigid thrust piece 71 is formed with a through-hole 718, and a small-diameter bar-like high-rigid thrust piece 72 is fitted in the through-hole 718. The diameter of the high-rigid thrust piece 72 is formed a little smaller than the inner diameter of the through-hole 718. The axial length L2 of the high-rigid thrust piece 72 is formed a little shorter than the axial length L1 of the low-rigid thrust piece 71.

Description

  The present invention relates to a cruciform universal joint, and more particularly to a cruciform universal joint incorporated in a vehicle steering apparatus.

  The steering device has a cross joint between the upper shaft and the lower shaft that transmits the rotation of the steering wheel to the steering gear, so that rotational torque can be transmitted between two shafts that are not on the same axis. ing. In the cross shaft universal joint, a cross shaft having four shaft portions arranged in a cross shape is rotatably supported in a bearing hole of a yoke via a needle bearing having a plurality of needles.

  In such a cross shaft universal joint, as shown in the cross shaft universal joint of Patent Document 1, a thrust piece made of synthetic resin is inserted into a bottomed axial hole formed in the shaft center of the shaft portion of the cross shaft. The thrust piece is sandwiched between the inner surface of the bottom of the cup-shaped outer ring of the needle bearing and the bottom of the axial hole with an appropriate preload in the thrust direction. This prevents excessive movement of the cross shaft in the thrust direction with respect to the needle bearing, absorbs dimensional errors due to manufacturing errors, etc., prevents deformation of the seal, and maintains good sealing performance. .

  However, if a large torque is applied to the cross joint by applying a stationary stop or the steering assist torque of the electric power steering device, a large thrust load acts on the synthetic resin thrust piece and plastically deforms. There is. Then, the bottom inner surface of the outer ring of the needle bearing and the tip end surface of the shaft portion of the cross shaft are in metal contact, the frictional resistance is increased, the steering torque is increased, the seal is deformed, and the sealing performance is deteriorated. was there. However, if the rigidity of the thrust piece is increased in order to prevent plastic deformation of the thrust piece, the elastic deformation amount of the thrust piece is reduced, so that a dimensional error can be absorbed and an appropriate preload in the thrust direction can be applied. It becomes difficult.

  The universal joints of Patent Literature 2 and Patent Literature 3 are provided with a low-rigidity thrust piece that is flexibly deformed and a high-rigidity thrust piece that is compressively deformed. After the contact, the highly rigid thrust piece is compressed and deformed to support a large thrust load.

  However, the cross shaft universal joints of Patent Document 2 and Patent Document 3 store two types of thrust pieces in a narrow space between the tip surface of the shaft portion of the cross shaft and the bottom inner surface of the cup-shaped outer ring of the needle bearing. Yes. Therefore, it is difficult to ensure the amount of bending deformation of the low-rigidity thrust piece, and the space for disposing the high-rigidity thrust piece is also limited, so it is difficult to support a large thrust load.

Japanese Utility Model Publication No. 7-24661 JP 2009-192063 A JP 2010-84818 A

  The present invention is a cross shaft provided with a thrust piece capable of absorbing a dimensional error and applying an appropriate preload in the thrust direction and supporting a large thrust load acting on the shaft portion of the cross shaft. It is an object to provide a universal joint.

  The above problem is solved by the following means. That is, the first invention is a bearing hole formed in the yoke, a bearing having a bottomed cylindrical outer ring fitted into the bearing hole, a cross shaft having a cross-shaped shaft portion fitted into the bearing, A bottomed axial hole formed in the shaft center of the shaft of the cross shaft, fitted into the bottomed axial hole, abutted against the inner surface of the bottom of the bearing outer ring, and axially compressed and thrust A low-rigidity thrust piece that supports the load is fitted into a through-hole formed in the shaft center of the low-rigidity thrust piece, and after the low-rigidity thrust piece is compressed in the axial direction, it contacts the bottom inner surface of the bearing outer ring. A cross-shaft universal joint comprising a high-rigidity thrust piece that comes into contact with the low-rigidity thrust piece and is axially compressed to support a thrust load.

  A second invention is a cross shaft universal joint according to the first invention, wherein the high-rigidity thrust piece is a small-diameter rod-like body fitted into the through hole.

  According to a third invention, in the cross joint according to the first invention, the high-rigidity thrust piece is fitted into the small-diameter rod-like body fitted into the through-hole, the axial hole, and the axial direction. A cross-shaft universal joint characterized in that a large-diameter shaft portion that abuts against the bottom of the hole is integrally formed.

  According to a fourth aspect of the present invention, in the cross joint according to the third aspect, the small-diameter rod-shaped body has a spherical surface that contacts the inner surface of the bottom of the bearing outer ring. It is a joint.

  According to a fifth invention, in the cross joint according to the third invention, the small-diameter rod-shaped body is engaged with the low-rigidity thrust piece to couple the high-rigidity thrust piece to the low-rigidity thrust piece. It is a cross shaft universal joint characterized in that a pawl is formed.

  According to a sixth aspect of the present invention, in the cross joint according to the first aspect, the low-rigidity thrust piece and the high-rigidity thrust piece have a shape on the bottom side of the axial hole and a shape on the bottom inner surface side of the bearing outer ring. Are universal cross joints characterized in that they are symmetrical with each other.

  The cross shaft universal joint of the present invention is fitted into a bottomed axial hole formed at the shaft center of the cross shaft, is in contact with the bottom inner surface of the bearing outer ring, is compressed in the axial direction, and is subjected to a thrust load. The low-rigidity thrust piece that supports the shaft and the through-hole formed in the shaft center of the low-rigidity thrust piece, and after the low-rigidity thrust piece is compressed in the axial direction, contact the bottom inner surface of the bearing outer ring, A high-rigidity thrust piece that is compressed in the axial direction together with the low-rigidity thrust piece and supports a thrust load.

  Therefore, since the low-rigidity thrust piece and the high-rigidity thrust piece are stored in the axial hole formed in the shaft core of the shaft portion and compressed in the axial direction to support the thrust load, the amount of compressive deformation of the low-rigidity thrust piece is reduced. Since it is easy to ensure and can suppress the plastic deformation and creep of the low-rigidity thrust piece, the durability of the cross shaft universal joint is improved. In addition, since a space for arranging the high-rigidity thrust piece is secured, a large thrust load can be supported.

BRIEF DESCRIPTION OF THE DRAWINGS The steering apparatus which has the cross-axis universal joint of this invention is shown whole, it is the front view which carried out the cross section, Comprising: The Example applied to the electric power steering apparatus is shown. It is the side view which carried out the cross section of a part of cross shaft universal joint of Example 1 of this invention. FIG. 3 is an enlarged sectional view in which a part of a shaft portion of the cross shaft universal joint of FIG. 2 is cut. (A) is a front view which shows the thrust piece of Example 1 of this invention, (b) is a front view which takes out and shows the high-rigidity thrust piece internally fitted in the through-hole of the low-rigidity thrust piece of (a). . FIG. 4 is a view corresponding to FIG. 3 showing a state in which a large thrust load is applied to the shaft portion. It is the expanded sectional view which carried out the cross section of a part of shaft part of the cross axis universal joint of Example 2 of the present invention. (A) is the front view which shows the thrust piece of Example 2 of this invention, (b) is the front view which shows the low-rigidity thrust piece of (a), (c) is the front which shows the high-rigidity thrust piece of (a). FIG. It is the expanded sectional view which carried out the cross section of a part of shaft part of the cross axis universal joint of Example 3 of the present invention. (A) is the front view which shows the thrust piece of Example 3 of this invention, (b) is the front view which shows the low-rigidity thrust piece of (a), (c) is the front which shows the high-rigidity thrust piece of (a). FIG.

    Embodiments 1 to 3 of the present invention will be described below with reference to the drawings.

  FIG. 1 is an overall view of a steering apparatus having a cross joint according to the present invention, and is a partially sectional front view showing an embodiment applied to an electric power steering apparatus.

  As shown in FIG. 1, a steering apparatus having a cross joint according to the present invention includes a steering shaft 12 on which a steering wheel 11 can be mounted on the rear side of the vehicle body (right side in FIG. 1), and a steering through which the steering shaft 12 is inserted. A column 13, an assist device (steering assisting portion) 20 for applying auxiliary torque to the steering shaft 12, and a rack / pinion mechanism (not shown) are provided on the vehicle body front side (left side in FIG. 1) of the steering shaft 12. And a steering gear 30 connected to each other.

  The steering shaft 12 is spline-fitted between a female steering shaft 12A and a male steering shaft 12B so as to be able to transmit rotational torque and to be relatively movable in the axial direction. Therefore, when the female steering shaft 12A and the male steering shaft 12B collide, the spline fitting portion moves relative to each other so that the total length can be shortened.

  Further, the cylindrical steering column 13 inserted through the steering shaft 12 combines the outer column 13A and the inner column 13B so that they can be telescopically moved. It has a so-called collapsible structure in which the entire length is shortened while absorbing water.

  The vehicle body front side end portion of the inner column 13B is press-fitted and fixed to the vehicle body rear side end portion of the gear housing 21. Further, the front end portion of the male steering shaft 12B on the vehicle body is passed through the inside of the gear housing 21 and connected to the rear end portion of the assist device 20 on the rear side of the input shaft (not shown).

  The steering column 13 is supported by a support bracket 14 at a middle portion thereof on a part of the vehicle body 18 such as a lower surface of the dashboard. Further, a locking portion (not shown) is provided between the support bracket 14 and the vehicle body 18, and when an impact in a direction toward the front side of the vehicle body is applied to the support bracket 14, the support bracket 14 is locked to the locking bracket 14. It moves away from the vehicle and moves to the front side of the vehicle.

  The upper end portion of the gear housing 21 is also supported on a part of the vehicle body 18. In the case of this embodiment, by providing a tilt mechanism and a telescopic mechanism, the position of the steering wheel 11 in the longitudinal direction of the vehicle body and the height position can be freely adjusted. Such a tilt mechanism and a telescopic mechanism are well known in the art and are not characteristic features of the present invention, and thus detailed description thereof is omitted.

  The output shaft 23 protruding from the end face on the vehicle body front side of the gear housing 21 is connected to the rear end portion of the intermediate shaft 16 via the cross shaft universal joint 15. Further, the input shaft 31 of the steering gear 30 is coupled to the front end portion of the intermediate shaft 16 via another cross shaft universal joint 15. The intermediate shaft 16 is fitted on the vehicle body front side of the male intermediate shaft (male shaft) 16A on the vehicle body rear side of the female intermediate shaft (female shaft) 16B, so that rotational torque can be transmitted and relative movement in the axial direction is possible. Is fitted.

  A pinion (not shown) is coupled to the input shaft 31. A rack (not shown) meshes with the pinion, and the rotation of the steering wheel moves the tie rod 32 to steer a wheel (not shown).

  A case 261 of an electric motor 26 is fixed to the gear housing 21 of the assist device 20, and a worm is coupled to a rotating shaft (not shown) of the electric motor 26. A worm wheel (not shown) is attached to the output shaft 23, and the worm of the rotating shaft of the electric motor 26 is engaged with the worm wheel.

  A torque sensor (not shown) is provided around the intermediate portion of the output shaft 23. The direction and magnitude of the torque applied from the steering wheel 11 to the steering shaft 12 is detected by a torque sensor, and the electric motor 26 is driven in accordance with the detected value via a reduction mechanism comprising a worm and a worm wheel. Then, the output shaft 23 is caused to generate auxiliary torque with a predetermined magnitude in a predetermined direction.

  2 is a side view in which a part of the cross shaft universal joint according to the first embodiment of the present invention is sectioned, and FIG. 3 is an enlarged sectional view in which a part of the shaft portion of the cross shaft universal joint in FIG. 4A is a front view showing the thrust piece according to the first embodiment of the present invention, and FIG. 4B is a drawing showing a high-rigidity thrust piece fitted in the through hole of the low-rigidity thrust piece of FIG. FIG. FIG. 5 is a view corresponding to FIG. 3 showing a state in which a large thrust load is applied to the shaft portion.

  As shown in FIGS. 2 to 4, the cruciform universal joint 15 has a cruciform cross shaft 5 interposed between a pair of yokes 4, 4 having arms that have bifurcated ends. That is, the shaft portions 51 and 51 at both ends of the cross shaft 5 are fitted in the bearing hole 41 of the yoke 4 through the needle bearing 6 so as to be swingable. The yoke 4 of this embodiment may be manufactured by any of sheet metal, forging, or casting, and the material of the yoke 4 may be either iron-based or aluminum-based.

  The outer ring 61 of the needle bearing 6 is made of a bottomed cylindrical (cylindrical cup-shaped) metal, and has a cylindrical portion 63 that fits into the bearing hole 41 and a top end of the cylindrical portion 63 as viewed in FIG. The bottom portion 64 is formed by being closed, and the inward bent portion 65 is formed at the lower end of the cylindrical portion 63 and is opened. The bottom part 64 is formed in a spherical shape. When the cylindrical portion 63 of the needle bearing 6 is press-fitted into the bearing hole 41, the seal 52 comes into light contact with the lower end surface of the inward bent portion 65, and dust is prevented from entering the needle bearing 6 from the outside.

  A plurality of needles 62 are arranged on the inner rolling surface 631 of the cylindrical portion 63 so as to be able to roll. Further, the inner periphery of the needle 62 and the outer peripheral surface 511 of the shaft portion 51 of the cross shaft 5 are formed in a dimensional relationship that fits with an appropriate gap. The fitting between the inner circumferential surface of the needle 62 and the outer circumferential surface 511 of the shaft portion 51 of the cross shaft 5 may be an interference fit fitting.

  A bottomed axial hole 53 is formed in the shaft core of the shaft portion 51, and a thrust piece 7 composed of a low-rigidity thrust piece 71 and a high-rigidity thrust piece 72 is inserted into the axial hole 53. . The axial hole 53 is formed by drilling, and the bottom 531 of the axial hole 53 is formed in a conical shape.

  As a material of the low-rigidity thrust piece 71, an elastic member such as rubber, elastomer, or synthetic resin is preferable. As a material of the high-rigidity thrust piece 72, an elastomer, a synthetic resin, a metal, or the like having higher rigidity than the low-rigidity thrust piece 71 is preferable.

  As shown in FIGS. 3 to 4, the low-rigidity thrust piece 71 is formed in a cylindrical shape as a whole. From the lower end side of FIG. 4, a truncated cone portion (conical portion with a truncated head) 711 and a large-diameter shaft portion 712 are formed. The small-diameter shaft portion 713, the large-diameter shaft portion 714, and the truncated cone portion 715 are formed in this order.

  The diameters of the large-diameter shaft portions 712 and 714 are formed slightly smaller than the inner diameter of the axial hole 53, and four rectangular cross-section ridges 716 are formed at intervals of 90 degrees on the outer peripheral surface of the large-diameter shaft portions 712 and 714. , 717 are formed. The diameter of the outer periphery of the protrusions 716 and 717 is formed to be slightly larger than the inner diameter of the axial hole 53.

  The lower end of the protrusion 716 is formed by being slightly retracted (from the small diameter shaft portion 713 side) from the connecting edge between the large diameter shaft portion 712 and the truncated cone portion 711. Similarly, the upper end of the ridge 717 is formed by being retracted slightly downward (smaller diameter shaft portion 713 side) from the connecting edge between the larger diameter shaft portion 714 and the truncated cone portion 715.

  The upper end of the protrusion 716 extends in the radial direction along the axially inner step surface of the large-diameter shaft portion 712 to the outer peripheral surface of the small-diameter shaft portion 713, thereby reinforcing the protrusion 716. Similarly, the lower end of the protrusion 717 extends in the radial direction along the axially inner step surface of the large diameter shaft portion 714 to the outer peripheral surface of the small diameter shaft portion 713, thereby reinforcing the protrusion 717.

  A through-hole 718 is formed in the shaft center of the low-rigidity thrust piece 71, and a high-rigidity thrust piece 72, which is a small-diameter rod-like body, is fitted in the through-hole 718. The diameter of the high-rigidity thrust piece 72 is slightly smaller than the inner diameter of the through hole 718. The axial length L2 of the high-rigidity thrust piece 72 is slightly shorter than the axial length L1 of the low-rigidity thrust piece 71.

  The high-rigidity thrust piece 72 is inserted into the through-hole 718 of the low-rigidity thrust piece 71, and the low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are integrated. In an integrated state, between the upper end surface 715A of the low rigidity thrust piece 71 and the upper end surface 721 of the high rigidity thrust piece 72, and the lower end surface 711A of the low rigidity thrust piece 71 and the lower end surface 722 of the high rigidity thrust piece 72. Between the two, gaps L3 and L4 are formed. The diameter of the high-rigidity thrust piece 72 may be slightly larger than the inner diameter of the through-hole 718, and the high-rigidity thrust piece 72 may be press-fitted into the through-hole 718 of the low-rigidity thrust piece 71.

  The integrated thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51. A truncated conical portion 711 at the lower end of the low-rigidity thrust piece 71 contacts the bottom portion 531 of the axial hole 53. In this state, the upper end surface 715 </ b> A of the low-rigidity thrust piece 71 slightly protrudes from the distal end surface 512 of the shaft portion 51.

  In the first embodiment of the present invention, if the low-rigidity thrust piece 71 is formed in a vertically symmetrical shape and the gaps L3 and L4 are set to have the same size, the axial hole is formed from either the upper end surface 715A or the lower end surface 711A of the thrust piece 7. Since it may be inserted into 53, assembly work becomes easy. Further, the protrusion 716 is formed by retracting toward the small diameter shaft portion 713 from the lower end surface 711A, and the protrusion 717 is formed by retracting from the upper end surface 715A toward the small diameter shaft portion 713. Therefore, it is easy to insert the thrust piece 7 into the axial hole 53. Even if there is some variation in the inner diameter of the axial hole 53, since the protrusions 716 and 717 are present, the pressure input of the thrust piece 7 is small and the change of the pressure input is small, so that the press-fitting operation becomes easy. .

  After the thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51, the cylindrical portion 63 of the needle bearing 6 is press-fitted into the bearing hole 41. Then, the center portion of the bottom inner surface 641 of the needle bearing 6 comes into contact with the upper end surface 715A of the low-rigidity thrust piece 71 and compresses the low-rigidity thrust piece 71 in the axial direction. Since there is a gap L3 between the upper end surface 721 of the high rigidity thrust piece 72 and the upper end surface 715A of the low rigidity thrust piece 71, the high rigidity thrust piece 72 is not compressed. The small-diameter shaft portion 713 of the low-rigidity thrust piece 71 is formed to have a smaller diameter than other portions of the low-rigidity thrust piece 71. Accordingly, when the low-rigidity thrust piece 71 is pushed into the bottom inner surface 641 of the needle bearing 6, the small-diameter shaft portion 713 is compressed and elastically deformed, and an appropriate preload in the thrust direction is applied between the needle bearing 6 and the shaft portion 51. Is done.

  When the steering assist torque of the assist device (steering assisting portion) 20 acts and a large torque acts on the cross shaft universal joint 15, a large thrust load acts on the shaft portion 51. Then, the low-rigidity thrust piece 71 is further compressed from the state shown in FIG. 3 to the state shown in FIG. That is, as shown in FIG. 5, the center portion of the bottom inner surface 641 of the needle bearing 6 contacts the upper end surface 721 of the high-rigidity thrust piece 72 and pushes down the high-rigidity thrust piece 72 in the axial direction.

When the lower end surface 722 of the high-rigidity thrust piece 72 comes into contact with the bottom 531 of the axial hole 53,
The high-rigidity thrust piece 72 is compressed in the axial direction to support a large thrust load, and a steering feeling with a feeling of rigidity is obtained. The low-rigidity thrust piece 71 is axially compressed together with the high-rigidity thrust piece 72 to support the thrust load. Therefore, even if a large thrust load is applied, the amount of compressive deformation of the low-rigidity thrust piece 71 does not increase, so that plastic deformation and creep of the low-rigidity thrust piece 71 can be suppressed, and the durability of the cross joint universal joint 15 is improved. To do.

  In Embodiment 1 of the present invention, a cylindrical low-rigidity thrust piece 71 and a high-rigidity thrust piece 72 are accommodated in an axial hole 53 formed in the shaft core of the shaft portion 51, and the thrust load is compressed by compressing in the axial direction. To support. Therefore, it is easy to ensure the amount of compressive deformation of the low-rigidity thrust piece 71 and a space for arranging the high-rigidity thrust piece is also ensured, so that a large thrust load can be supported.

  Next, a second embodiment of the present invention will be described. FIG. 6 is an enlarged cross-sectional view showing a cross section of a part of the shaft portion of the cross joint according to the second embodiment of the present invention. 7 (a) is a front view showing a thrust piece of Example 2 of the present invention, FIG. 7 (b) is a front view showing a low-rigidity thrust piece of FIG. 7 (a), and FIG. 7 (c) is FIG. It is a front view which shows the highly rigid thrust piece of a). In the following description, only structural portions and operations different from the above embodiment will be described, and redundant description will be omitted.

  The second embodiment is an example in which the shapes of the low rigidity thrust piece 71 and the high rigidity thrust piece 72 are changed. That is, as shown in FIGS. 6 and 7, a bottomed axial hole 53 is formed in the shaft core of the shaft portion 51, and a low-rigidity thrust piece 71 and a high-rigidity thrust piece 72 are formed in the axial hole 53. A thrust piece 7 is inserted. The low-rigidity thrust piece 71 is formed in a columnar shape as a whole, and is formed in the order of a small-diameter shaft portion 713, a large-diameter shaft portion 714, and a truncated cone portion 715 from the lower end side in FIG.

  The diameter of the large-diameter shaft portion 714 is formed to be slightly smaller than the inner diameter of the axial hole 53, and four rectangular cross-section ridges 717 are formed on the outer peripheral surface of the large-diameter shaft portion 714 at intervals of 90 degrees. Yes. The diameter of the outer periphery of the protrusion 717 is formed to be slightly larger than the inner diameter of the axial hole 53.

  The upper end of the ridge 717 is formed by being retracted slightly downward (to the small diameter shaft portion 713 side) from the connecting edge between the large diameter shaft portion 714 and the truncated cone portion 715. Further, the lower end of the protrusion 717 extends in the radial direction along the axially inner step surface of the large diameter shaft portion 714 to the outer peripheral surface of the small diameter shaft portion 713, thereby reinforcing the protrusion 717. A through hole 718 is formed in the axial center of the low-rigidity thrust piece 71 over the entire axial length thereof.

  As shown in FIG. 7 (c), the high-rigidity thrust piece 72 is formed in a columnar shape as a whole. From the lower end side of FIG. 7 (c), a truncated cone portion (conical portion with a cut head) 723, a large diameter The shaft portion 724, the small diameter shaft portion 725, and the small diameter rod-shaped body 726 are formed in this order.

  The diameter of the large-diameter shaft portion 724 is slightly smaller than the inner diameter of the axial hole 53, and four rectangular cross-section ridges 727 are formed on the outer peripheral surface of the large-diameter shaft portion 724 at intervals of 90 degrees. Yes. The diameter of the outer periphery of the protrusion 727 is formed to be slightly larger than the inner diameter of the axial hole 53.

  The lower end of the protrusion 727 is formed by being slightly retracted (from the small diameter shaft portion 725 side) from the connecting edge between the large diameter shaft portion 724 and the truncated cone portion 723. The upper end of the protrusion 727 extends in the radial direction along the axially inner step surface of the large-diameter shaft portion 724 to the outer peripheral surface of the small-diameter shaft portion 725, thereby reinforcing the protrusion 727.

  A small-diameter rod-like body 726 of the highly rigid thrust piece 72 is fitted in the through hole 718. The diameter of the small diameter rod-like body 726 is slightly smaller than the inner diameter of the through hole 718. Further, the axial length L6 of the small-diameter rod-like body 726 is slightly shorter than the axial length L5 of the low-rigidity thrust piece 71.

  The small-diameter rod-like body 726 of the high-rigidity thrust piece 72 is inserted into the through hole 718 of the low-rigidity thrust piece 71 so that the low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are integrated. When integrated, a gap L7 is formed between the upper end surface 715A of the low-rigidity thrust piece 71 and the upper end surface 721 of the small-diameter rod-like body 726 of the high-rigidity thrust piece 72. The diameter of the small-diameter rod-shaped body 726 of the high-rigidity thrust piece 72 is slightly larger than the inner diameter of the through-hole 718, and the small-diameter rod-shaped body 726 of the high-rigidity thrust piece 72 is inserted into the through-hole 718 of the low-rigidity thrust piece 71. You may press fit.

  The integrated thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51. The truncated conical portion 723 at the lower end of the high-rigidity thrust piece 72 abuts on the bottom portion 531 of the axial hole 53. In this state, the upper end surface 715 </ b> A of the low-rigidity thrust piece 71 slightly protrudes from the distal end surface 512 of the shaft portion 51.

  In the second embodiment of the present invention, the protrusion 727 is formed by retracting toward the small diameter shaft portion 725 from the lower end surface 723A, and the protrusion 717 is formed by retracting toward the small diameter shaft portion 713 from the upper end surface 715A. Therefore, it is easy to insert the thrust piece 7 into the axial hole 53. Even if there is some variation in the inner diameter of the axial hole 53, since the protrusions 727 and 717 are present, the pressure input of the thrust piece 7 is small and the change of the pressure input is small, so that the press-fitting operation becomes easy. .

  After the thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51, the cylindrical portion 63 of the needle bearing 6 is press-fitted into the bearing hole 41. Then, the center portion of the bottom inner surface 641 of the needle bearing 6 comes into contact with the upper end surface 715A of the low-rigidity thrust piece 71 and compresses the low-rigidity thrust piece 71 in the axial direction. Since there is a gap L7 between the upper end surface 721 of the small-diameter rod-like body 726 of the high rigidity thrust piece 72 and the upper end face 715A of the low rigidity thrust piece 71, the high rigidity thrust piece 72 is not compressed.

  The small-diameter shaft portion 713 of the low-rigidity thrust piece 71 is formed to have a smaller diameter than other portions of the low-rigidity thrust piece 71. Accordingly, when the low-rigidity thrust piece 71 is pushed into the bottom inner surface 641 of the needle bearing 6, the small-diameter shaft portion 713 is compressed and elastically deformed, and an appropriate preload in the thrust direction is applied between the needle bearing 6 and the shaft portion 51. Is done.

  When the steering assist torque of the assist device (steering assisting portion) 20 acts and a large torque acts on the cross shaft universal joint 15, a large thrust load acts on the shaft portion 51. Then, the low-rigidity thrust piece 71 is further compressed from the state shown in FIG. 6, and the center portion of the bottom inner surface 641 of the needle bearing 6 comes into contact with the upper end surface 721 of the small-diameter rod-like body 726 of the high-rigidity thrust piece 72. The thrust piece 72 is compressed in the axial direction.

  The high-rigidity thrust piece 72 is compressed in the axial direction to support a large thrust load, and a steering feeling with a feeling of rigidity is obtained. The low-rigidity thrust piece 71 is axially compressed together with the high-rigidity thrust piece 72 to support the thrust load. Therefore, even if a large thrust load is applied, the amount of compressive deformation of the low-rigidity thrust piece 71 does not increase, so that plastic deformation and creep of the low-rigidity thrust piece 71 can be suppressed, and the durability of the cross joint universal joint 15 is improved. To do.

  In Embodiment 2 of the present invention, a cylindrical low-rigidity thrust piece 71 and a high-rigidity thrust piece 72 are accommodated in an axial hole 53 formed in the shaft core of the shaft portion 51, and the thrust load is compressed by compressing in the axial direction. To support. Therefore, it is easy to ensure the amount of compressive deformation of the low-rigidity thrust piece 71 and a space for arranging the high-rigidity thrust piece is also ensured, so that a large thrust load can be supported.

  Next, a third embodiment of the present invention will be described. FIG. 8 is an enlarged cross-sectional view of a part of the shaft portion of the cross joint according to the third embodiment of the present invention. 9A is a front view showing a thrust piece according to the third embodiment of the present invention, FIG. 9B is a front view showing the low-rigidity thrust piece of FIG. 9A, and FIG. 9C is FIG. It is a front view which shows the highly rigid thrust piece of a). In the following description, only structural portions and operations different from the above embodiment will be described, and redundant description will be omitted.

  The third embodiment is a modification of the second embodiment, in which the low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are reliably integrated. That is, as shown in FIGS. 8 and 9, a bottomed axial hole 53 is formed in the shaft core of the shaft portion 51, and a low-rigidity thrust piece 71 and a high-rigidity thrust piece 72 are formed in the axial hole 53. A thrust piece 7 is inserted. The low-rigidity thrust piece 71 is formed in a columnar shape as a whole, and is formed in the order of a small-diameter shaft portion 713, a large-diameter shaft portion 714, and a truncated cone portion 715 from the lower end side in FIG.

  The diameter of the large-diameter shaft portion 714 is formed to be slightly smaller than the inner diameter of the axial hole 53, and four rectangular cross-section ridges 717 are formed on the outer peripheral surface of the large-diameter shaft portion 714 at intervals of 90 degrees. Yes. The diameter of the outer periphery of the protrusion 717 is formed to be slightly larger than the inner diameter of the axial hole 53.

  The upper end of the ridge 717 is formed by being retracted slightly downward (to the small diameter shaft portion 713 side) from the connecting edge between the large diameter shaft portion 714 and the truncated cone portion 715. Further, the lower end of the protrusion 717 extends in the radial direction along the axially inner step surface of the large diameter shaft portion 714 to the outer peripheral surface of the small diameter shaft portion 713, thereby reinforcing the protrusion 717. A through hole 718 is formed in the axial center of the low-rigidity thrust piece 71 over the entire axial length thereof.

  As shown in FIG. 9 (c), the high-rigidity thrust piece 72 is formed in a columnar shape as a whole. From the lower end side of FIG. 9 (c), a truncated cone portion (conical portion with a cut head) 723, a large diameter The shaft portion 724, the small diameter shaft portion 725, and the small diameter rod-shaped body 726 are formed in this order.

  The diameter of the large-diameter shaft portion 724 is slightly smaller than the inner diameter of the axial hole 53, and four rectangular cross-section ridges 727 are formed on the outer peripheral surface of the large-diameter shaft portion 724 at intervals of 90 degrees. Yes. The diameter of the outer periphery of the protrusion 727 is formed to be slightly larger than the inner diameter of the axial hole 53.

  The lower end of the protrusion 727 is formed by being slightly retracted (from the small diameter shaft portion 725 side) from the connecting edge between the large diameter shaft portion 724 and the truncated cone portion 723. The upper end of the protrusion 727 extends in the radial direction along the axially inner step surface of the large-diameter shaft portion 724 to the outer peripheral surface of the small-diameter shaft portion 725, thereby reinforcing the protrusion 727.

  A small-diameter rod-like body 726 of the highly rigid thrust piece 72 is fitted in the through hole 718. The diameter of the small diameter rod-like body 726 is slightly smaller than the inner diameter of the through hole 718. Further, the axial length L6 of the small-diameter rod-like body 726 is slightly shorter than the axial length L5 of the low-rigidity thrust piece 71.

  The upper end surface 721 of the small diameter rod-like body 726 is formed into a spherical surface. Further, an engagement claw 721A is formed slightly below the upper end surface 721 of the small diameter rod-like body 726, and the engagement claw 721A protrudes radially outward from the outer peripheral surface of the small diameter rod-like body 726. An engagement hole 718A having a slightly larger diameter than the inner diameter of the through hole 718 is formed at the upper end of the through hole 718 of the low rigidity thrust piece 71.

  The small-diameter rod-like body 726 of the high-rigidity thrust piece 72 is inserted into the through hole 718 of the low-rigidity thrust piece 71. The engaging claw 721A is inserted along the through-hole 718 while reducing the diameter, and when the engaging claw 721A reaches the engaging hole 718A, the engaging claw 721A increases in diameter. Then, the engaging claw 721A engages with the step surfaces of the engaging hole 718A and the through hole 718, and the low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are integrated. The piece 72 is securely retained. When the low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are integrated, a gap L7 is formed between the upper end surface 715A of the low-rigidity thrust piece 71 and the upper end surface 721 of the small-diameter rod-like body 726 of the high-rigidity thrust piece 72. The

  The integrated thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51. The truncated conical portion 723 at the lower end of the high-rigidity thrust piece 72 abuts on the bottom portion 531 of the axial hole 53. In this state, the upper end surface 715 </ b> A of the low-rigidity thrust piece 71 slightly protrudes from the distal end surface 512 of the shaft portion 51.

  In Embodiment 3 of the present invention, the protrusion 727 is formed by retracting toward the small diameter shaft portion 725 from the lower end surface 723A, and the protrusion 717 is formed by retracting toward the small diameter shaft portion 713 from the upper end surface 715A. Therefore, it is easy to insert the thrust piece 7 into the axial hole 53. Even if there is some variation in the inner diameter of the axial hole 53, since the protrusions 727 and 717 are present, the pressure input of the thrust piece 7 is small and the change of the pressure input is small, so that the press-fitting operation becomes easy. .

  After the thrust piece 7 is inserted into the axial hole 53 of the shaft portion 51, when the cylindrical portion 63 of the needle bearing 6 is press-fitted into the bearing hole 41, the center portion of the bottom inner surface 641 of the needle bearing 6 is reduced in the low rigidity thrust piece 71. The lower rigidity thrust piece 71 is compressed in the axial direction. Since there is a gap L7 between the upper end surface 721 of the small-diameter rod-like body 726 of the high rigidity thrust piece 72 and the upper end face 715A of the low rigidity thrust piece 71, the high rigidity thrust piece 72 is not compressed.

  The small-diameter shaft portion 713 of the low-rigidity thrust piece 71 is formed to have a smaller diameter than other portions of the low-rigidity thrust piece 71. Accordingly, when the low-rigidity thrust piece 71 is pushed into the bottom inner surface 641 of the needle bearing 6, the small-diameter shaft portion 713 is compressed and elastically deformed, and an appropriate preload in the thrust direction is applied between the needle bearing 6 and the shaft portion 51. Is done.

  When the steering assist torque of the assist device (steering assisting portion) 20 acts and a large torque acts on the cross shaft universal joint 15, a large thrust load acts on the shaft portion 51. Then, the low-rigidity thrust piece 71 is further compressed from the state shown in FIG. 8, and the center portion of the bottom inner surface 641 of the needle bearing 6 comes into contact with the upper end surface 721 of the small-diameter rod-like body 726 of the high-rigidity thrust piece 72. The thrust piece 72 is compressed in the axial direction.

  The high-rigidity thrust piece 72 is compressed in the axial direction to support a large thrust load, and a steering feeling with a feeling of rigidity is obtained. The low-rigidity thrust piece 71 is axially compressed together with the high-rigidity thrust piece 72 to support the thrust load. Therefore, even if a large thrust load is applied, the amount of compressive deformation of the low-rigidity thrust piece 71 does not increase, so that plastic deformation and creep of the low-rigidity thrust piece 71 can be suppressed, so that the durability of the cross joint 15 is improved. To do.

  In Embodiment 3 of the present invention, the upper end surface 721 of the small-diameter rod-like body 726 of the high-rigidity thrust piece 72 is formed into a spherical surface. Therefore, since the frictional resistance when the shaft portion 51 rotates while a large thrust load is applied can be reduced, the steering feeling is improved and the durability of the cross joint universal joint 15 is improved.

  In the third embodiment of the present invention, the cylindrical low-rigidity thrust piece 71 and the high-rigidity thrust piece 72 are accommodated in the axial hole 53 formed in the shaft core of the shaft portion 51, and thrust is compressed in the axial direction. Support the load. Therefore, it is easy to ensure the amount of compressive deformation of the low-rigidity thrust piece 71 and a space for arranging the high-rigidity thrust piece is also ensured, so that a large thrust load can be supported.

  In the above-described embodiment, an example in which the present invention is applied to a cross shaft universal joint used in a vehicle steering apparatus has been described. However, the present invention may be applied to a cross shaft universal joint used in a power transmission shaft. In the above embodiment, an example in which the present invention is applied to a cross joint that is used in a vehicle steering apparatus having the assist device 20 has been described. However, the present invention may be applied to a vehicle steering apparatus without the assist device 20. Good.

DESCRIPTION OF SYMBOLS 11 Steering wheel 12 Steering shaft 12A Female steering shaft 12B Male steering shaft 13 Steering column 13A Outer column 13B Inner column 14 Support bracket 15 Cross shaft universal joint 16 Intermediate shaft 16A Male intermediate shaft 16B Female intermediate shaft 18 Car body 20 Assist device 21 Gear housing DESCRIPTION OF SYMBOLS 23 Output shaft 26 Electric motor 261 Case 30 Steering gear 31 Input shaft 32 Tie rod 4 Yoke 41 Bearing hole 5 Cross shaft 51 Shaft part 511 Outer surface 512 Front end surface 52 Seal 53 Axial hole 531 Bottom part 6 Needle bearing 61 Outer ring 62 Needle 63 Cylinder 631 Inner rolling surface 64 Bottom 641 Bottom inner surface 65 Inwardly bent portion 7 Thrust piece 71 Low rigidity thrust piece DESCRIPTION OF SYMBOLS 11 Cone cone part 711A Lower end surface 712 Large diameter shaft part 713 Small diameter shaft part 714 Large diameter shaft part 715 Cone cone part 715A Upper end surface 716,717 Projection 718 Through hole 718A Engagement hole 72 High rigidity thrust piece 721 Upper end surface 721A engaging claw 722 lower end surface 723 truncated cone portion 723A lower end surface 724 large diameter shaft portion 725 small diameter shaft portion 726 small diameter rod-shaped body 727 protrusion

Claims (6)

Bearing holes formed in the yoke,
A bearing having a bottomed cylindrical outer ring fitted into the bearing hole;
A cross shaft having a cross-shaped shaft portion fitted into the bearing;
A bottomed axial hole formed in the axial center of the shaft portion of the cross shaft,
A low-rigidity thrust piece that fits into the bottomed axial hole, abuts against the bottom inner surface of the bearing outer ring, and is axially compressed to support a thrust load;
It is fitted in a through-hole formed in the shaft center of the low-rigidity thrust piece, and after the low-rigidity thrust piece is compressed in the axial direction, it comes into contact with the bottom inner surface of the bearing outer ring, and the shaft together with the low-rigidity thrust piece A cross shaft universal joint comprising a highly rigid thrust piece that is compressed in a direction to support a thrust load. In the cross joint according to claim 1,
The high rigidity thrust piece is
A cross shaft universal joint characterized by being a small-diameter rod-like body fitted into the through hole. In the cross joint according to claim 1,
The high rigidity thrust piece is
A small-diameter rod-like body fitted into the through hole;
A cross-joint universal joint characterized in that a large-diameter shaft portion that is fitted in the axial hole and abuts against a bottom portion of the axial hole is integrally formed. In the cross joint according to claim 3,
The small diameter rod-shaped body is
A cross joint with a universal joint, characterized in that a surface that contacts the inner surface of the bottom of the outer ring of the bearing is formed into a spherical surface. In the cross joint according to claim 3,
In the small diameter rod-shaped body,
A cross shaft universal joint characterized in that an engaging claw for engaging the low rigidity thrust piece and coupling the high rigidity thrust piece to the low rigidity thrust piece is formed. In the cross joint according to claim 1,
The low rigidity thrust piece and the high rigidity thrust piece are
A cross shaft universal joint characterized in that the shape of the bottom side of the axial hole and the shape of the bottom inner surface of the bearing outer ring are symmetrical to each other.

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