Bearing structure

Abstract

An outer-ring-equivalent component having an annular raceway surface on which rolling elements roll is disposed on an outer circumference of a bearing. The bearing is, for example, a retainer-equipped roller. Between the bearing and a fixed member located apart from the bearing in an axial direction, a thrust washer is interposed so as to be movable in the axial direction. A gap forming device is provided which constantly forms a gap between the thrust washer and the outer-ring-equivalent component. For example, as the gap forming device, an axial width of the bearing is made larger than an axial width of the outer-ring-equivalent component.

Claims

1. A bearing structure comprising: a single-row or multiple-row bearing composed of a plurality of rolling elements arranged in a circumferential direction, and an annular retainer that retains the plurality of rolling elements; an outer-ring-equivalent component disposed on an outer circumference of the bearing, and having an annular raceway surface on which the rolling elements roll; and a thrust washer interposed between the bearing and a fixed member spaced apart from the bearing in an axial direction, the thrust washer being movable in the axial direction, wherein an axial width of the bearing is larger than an axial width of the outer-ring-equivalent component to constantly form a gap between the thrust washer and the outer-ring-equivalent component.

2. The bearing structure as claimed in claim 1, wherein the bearing is a retainer-equipped roller.

3. A bearing structure comprising: a single-row or multiple-row bearing composed of a plurality of rolling elements arranged in a circumferential direction, and an annular retainer that retains the plurality of rolling elements; an outer-ring-equivalent component disposed on an outer circumference of the bearing, and having an annular raceway surface on which the rolling elements roll; a thrust washer interposed between the bearing and a fixed member spaced apart from the bearing in an axial direction, the thrust washer being movable in the axial direction; and a spacer interposed between the bearing and the thrust washer to constantly form a gap between the thrust washer and the outer-ring-equivalent component.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) In any event, the present invention will become more clearly understood from the following description of preferred embodiments thereof, when taken in conjunction with the accompanying drawings. However, the embodiments and the drawings are given only for the purpose of illustration and explanation, and are not to be taken as limiting the scope of the present invention in any way whatsoever, which scope is to be determined by the appended claims. In the accompanying drawings, like reference numerals are used to denote like parts throughout the several views, and:

(2) FIG. 1A is a cross-sectional view conceptually showing a state of a bearing structure according to a first embodiment of the present invention;

(3) FIG. 1B is a cross-sectional view conceptually showing the bearing structure, in a state different from the state shown in FIG. 1A, according to the first embodiment of the present invention;

(4) FIG. 2A is a cross-sectional view of a bearing structure in which a retainer is guided-by-rolling-element;

(5) FIG. 2B is a partially enlarged view of FIG. 2A;

(6) FIG. 3A is a cross-sectional view of a bearing structure in which a retainer is guided-at-outer-diameter-surface;

(7) FIG. 3B is a partially enlarged view of FIG. 3A;

(8) FIG. 4 is a cross-sectional view conceptually showing a bearing structure using multiple rows of bearings;

(9) FIG. 5 is a cross-sectional view conceptually showing a roller bearing structure according to a second embodiment of the present invention;

(10) FIG. 6 is a cross-sectional view conceptually showing a roller bearing structure according to a third embodiment of the present invention;

(11) FIG. 7 is a cross-sectional view conceptually showing a roller bearing structure according to a fourth embodiment of the present invention;

(12) FIG. 8A is a cross-sectional view conceptually showing a state of a conventional bearing structure; and

(13) FIG. 8B is a cross-sectional view conceptually showing the conventional bearing structure in a state different from the state shown in FIG. 8A.

DESCRIPTION OF EMBODIMENTS

(14) Embodiments of the present invention will be described with reference to the drawings.

(15) FIGS. 1A and 1B show a first embodiment of the present invention. A bearing structure according to the first embodiment is used for rotatably supporting an outer-ring-equivalent component 2 composed of a planetary gear with respect to a horizontally oriented shaft 1, in a planetary reduction gear of a hydraulically operated shovel, for example. The bearing structure is composed of a bearing 3, and thrust washers 4 disposed at both axial sides of the bearing 3.

(16) The bearing 3 is composed of a plurality of rolling elements 5 arranged in a circumferential direction thereof, and an annular retainer 6 that retains the plurality of rolling elements 5 in a pocket 6a. In this example, each rolling element 5 is a cylindrical roller, and the bearing 3 is a retainer-equipped cylindrical roller. Each rolling element 5 has a rolling surface 5a on its outer circumference, and rolls on a raceway surface 1a formed as an outer peripheral surface of the shaft 1, and a raceway surface 2a formed as an inner peripheral surface of the outer-ring-equivalent component 2. In this example, the retainer is guided-by-rolling-element. However, the retainer 6 may be guided-at-inner-diameter-surface (not shown), or may be guided-at-outer-diameter-surface as shown in FIGS. 3A and 3B. The term guided-by-rolling-element means that an inner diameter surface of the retainer 6 is not in contact with the shaft 1, an outer diameter surface of the retainer 6 is not in contact with the outer-ring-equivalent component 2, and rotation of the retainer 6 is guided by only the rolling elements 5. The term guided-at-inner-diameter-surface means that the inner diameter surface of the retainer 6 is in contact with the shaft 1, whereby rotation of the retainer 6 is guided by the shaft 1. The term guided-at-outer-diameter-surface means that the outer diameter surface of the retainer 6 is in contact with the outer-ring-equivalent component 2, whereby rotation of the retainer 6 is guided by the outer-ring-equivalent component 2.

(17) Each thrust washer 4 is a ring-shaped member, both end surfaces of which are smoothly formed. Each thrust washer 4 is movable in the axial direction between the bearing 3 and a fixed member 7. The fixed member 7 is fixed in position, and supports the shaft 1. The fixed member 7 is a carrier of a planetary reduction gear, for example. At a bottom portion of the fixed member 7 composed of the carrier, oil for lubrication is stored to a depth at which the outer-ring-equivalent component 2 or the bearing 3 is immersed in the oil. With rotation of the outer-ring-equivalent component 2 or the bearing 3, the components arranged in the circumferential direction are immersed in the stored oil, whereby the oil for lubrication is supplied to the bearing 3. Therefore, the bearing 3 is not forcibly lubricated. An oil hole for lubrication is not provided in the shaft 1.

(18) The bearing structure is provided with gap forming device 10 that constantly forms a gap between the thrust washer 4 and the outer-ring-equivalent component 2. In the case of the bearing structure shown in FIGS. 1A and 1B, as the gap forming device 10, an axial width J of the bearing 3 is set to be larger than an axial width G of the outer-ring-equivalent component 2.

(19) When the axial widths J and G of the bearing 3 and the outer-ring-equivalent component 2 are set as described above, even if the thrust washer 4 is completely in close contact with or almost comes into close contact with one of end faces of the outer-ring-equivalent component 2 due to surface tension of the oil as shown in FIG. 1B, the thrust washer 4 does not come into close contact with the other end face of the outer-ring-equivalent component 2 because the bearing 3 hinders the contact. Therefore, a gap 11 is constantly formed between at least one of the thrust washers 4 and the outer-ring-equivalent component 2, and foreign matter such as wear debris contained in the oil for lubrication is not likely to stay in the bearing 3, specifically, in the pocket 6a of the retainer 6, between the rolling element 5 and the shaft 1, and between the rolling element 5 and the outer-ring-equivalent component 2. Thus, it is possible to avoid the situation that the foreign matter is jammed between the shaft 1 and the rolling element 5 and thereby surface portions of the shaft 1, the outer-ring-equivalent component 2, the rolling element 5 and the like are peeled off.

(20) When the two thrust washers 4 are provided at the both sides of the bearing 3 as described above, it can be said that the gap forming device 10 is a device to form the gap 11 between at least one of the two thrust washers 4 and the outer-ring-equivalent component 2.

(21) FIGS. 1A and 1B are cross-sectional views conceptually showing the bearing structure. However, in an actual bearing structure, as shown in cross-sectional views of FIGS. 2A and 2B and FIGS. 3A and 3B, chamfered portions 2b are formed at both ends of the raceway surface 2a of the outer-ring-equivalent component 2, and chamfered portions 5b are formed at both ends of the rolling surface 5a of the rolling element 5 composed of a cylindrical roller. Therefore, in the case where the axial width J of the bearing 3 is set to be larger than the axial width G of the outer-ring-equivalent component 2, in order to make the entire area of the rolling surface 5a of the rolling element 5 in the axial direction constantly in contact with the raceway surface 2a of the outer-ring-equivalent component 2, the dimensions of the components of the bearing structure need to be set as follows.

(22) That is, in the case of the bearing structure (FIGS. 2A and 2B) in which the retainer 6 is guided-by-rolling-element or guided-at-inner-diameter-surface, a relationship of a+c<b+d is satisfied, in which a represents a maximum guide gap, in the axial direction, of the outer-ring-equivalent component 2, b represents a minimum guide width from an end surface of the retainer 6 to the pocket 6a, c represents a maximum chamfering amount of the raceway surface 2a of the outer-ring-equivalent component 2, and d represents a minimum chamfering amount of the rolling surface 5a of the rolling element 5, as shown in FIG. 2B. In the case of the bearing structure (FIGS. 3A and 3B) in which the retainer 6 is guided-at-outer-diameter-surface, a relationship of a+c<b is satisfied as shown in FIG. 3B. The maximum guide gap a, in the axial direction, of the outer-ring-equivalent component 2 is a maximum guide gap in the axial direction, which is formed between the thrust washer 4 and the outer-ring-equivalent component 2 in the state where the thrust washers 4 at the both ends are in contact with the fixed member 7 (FIGS. 1A and 1B) as a carrier.

(23) In FIGS. 2A and 2B and FIGS. 3A and 3B, a gap is formed between the rolling surface 5a of the rolling element 5 and the raceway surface 1a of the shaft 1 and between the rolling surface 5a of the rolling element 5 and the raceway surface 2a of the outer-ring-equivalent component 2. However, actually, the rolling surface 5a of the rolling element 5 is in contact with the raceway surface 1a of the shaft 1, and the rolling surface 5a of the rolling element 5 is in contact with the raceway surface 2a of the outer-ring-equivalent component 2.

(24) While the single-row bearing 3 is described as an example in the above embodiment, a multiple-row bearing 3 may be provided as shown in FIG. 4. That is, a plurality of single-row bearing portions 3A may be arranged in the axial direction to provide the multiple-row bearing 3. In this case, the following relationship is satisfied: (axial width J of single-row bearing portion 3A)(number of single-row bearing portions 3A)>(axial width G of outer-ring-equivalent component 2).

(25) FIG. 5 shows a second embodiment. In a bearing structure according to the second embodiment, a projecting portion 12 that projects toward the bearing 3 is provided, as the gap forming device 10, on a radial portion of each thrust washer 4 opposed to the bearing 3. The projecting portion 12 may be continuously provided over the entire circumference, or projecting portions 12 may be partially provided at a plurality of positions in the circumferential direction. A projecting amount e of the projecting portion 12 is set so that a dimension value (J+2e) obtained by adding a sum of projecting amounts e of the projecting portions 12 of the both thrust washers 4 to the axial width J of the bearing 3 is larger than the dimension value of the axial width G of the outer-ring-equivalent component 2. According to this configuration, even if the axial width J of the bearing 3 is smaller than the axial width G of the outer-ring-equivalent component 2, it is possible to achieve the same effect as that obtained when the axial width J of the bearing 3 is larger than the axial width G of the outer-ring-equivalent component 2 as shown in FIGS. 1A and 1B. Thus, the gap 11 is constantly formed between the thrust washer 4 and the outer-ring-equivalent component 2.

(26) FIG. 6 shows a third embodiment. In a bearing structure according to the third embodiment, an annular spacer 13 is interposed, as the gap forming device 10, between the bearing 3 and each thrust washer 4. An axial width f of the spacer 13 is set so that a dimension value (J+2f) obtained by adding a sum of the axial widths f of the both spacers 13 to the axial width J of the bearing 3 is larger than the dimension value of the axial width G of the outer-ring-equivalent component 2. According to this configuration, even if the axial width J of the bearing 3 is smaller than the axial width G of the outer-ring-equivalent component 2, it is possible to achieve the same effect as that obtained when the axial width J of the bearing 3 is larger than the axial width G of the outer-ring-equivalent component 2 as shown in FIGS. 1A and 1B. Thus, the gap 11 is constantly formed between the thrust washer 4 and the outer-ring-equivalent component 2.

(27) FIG. 7 shows a fourth embodiment. In a bearing structure according to the fourth embodiment, as the gap forming device 10, one of thrust washers 4A is arched so that, in the cross-sectional view, an axial distance from the outer-ring-equivalent component 2 is increased toward the outer diameter side thereof. According to this configuration, even if the axial width J of the bearing 3 is smaller than the axial width G of the outer-ring-equivalent component 2, the thrust washer 4A is prevented from coming into close contact with the outer-ring-equivalent component 2. Thus, the gap 11 is constantly formed between the thrust washer 4A and the outer-ring-equivalent component 2.

(28) Although the preferred embodiments have been described with reference to the drawings, those skilled in the art will readily conceive various changes and modifications within the framework of obviousness upon the reading of the specification herein presented of the present invention. Accordingly, such changes and modifications are to be construed as included in the scope of the present invention as delivered from the claims annexed hereto.

REFERENCE NUMERALS

(29) 1 . . . shaft 2 . . . outer-ring-equivalent component 2a . . . raceway surface 3 . . . bearing 4, 4A . . . thrust washer 5 . . . rolling element 6 . . . retainer 7 . . . fixed member 10 . . . gap forming device 11 . . . gap 12 . . . projecting portion 13 . . . spacer