BEARING ARRANGEMENT FOR A MUTUALLY TURNABLE UNIT WORKING UNDER HIGH PRESSURE

Abstract

A bearing arrangement for a unit that is mutually turnable around a centre of rotation (R) comprising an external part (1) and an internal part (7), which, with the aid of high hydraulically acting pressure, is arranged to achieve a reciprocating rotary motion, or that is arranged to achieve a high hydraulic pressure from an applied torque from a reciprocating motion, whereby the external part (1) is provided with side walls arranged to axially surround at least a part of the internal part (7), and whereby the external part (1) comprises a radially inwardly arranged and essentially surrounding cavity (11, 12, 13, 14) in which the internal part (7) is arranged such that it can be rotated, which cavity (11, 12, 13, 14) is limited in the circumferential direction by at least one wing (3, 4) that protrudes inwards from the external part (1) and also limited by at least one wing (9, 10) that protrudes radially outwards from the internal part (7), which wings (3, 4, 9, 10) limit at least two chambers or compartments (11, 12, 13, 14) between the external part (1) and the internal part (7). At least one of the side walls of the external part is fixed connected with the, at least one, wing (3, 4) that protrudes radially inwards towards the internal part (7), which wing demonstrates a surface that faces radially inwards and that has a circular concave curvature for connection with an outwardly facing circular convex contact surface (8) at the internal part (7).

Claims

1. A bearing arrangement for a unit that is mutually turnable around a centre of rotation, comprising an external part and an internal part, which, with the aid of high hydraulically acting pressure, is arranged to achieve a reciprocating rotary motion, or that is arranged to achieve a high hydraulic pressure from an applied torque from a reciprocating motion, whereby the external part is provided with side walls arranged to axially surround at least a part of the internal part, and whereby the external part comprises a radially inwardly arranged and essentially surrounding cavity in which the internal part is arranged such that it can be rotated, which cavity is limited in the circumferential direction by at least one wing that protrudes inwards from the external part and also limited by at least one wing that protrudes radially outwards from the internal part, which wings limit at least two compartments or chambers between the external part and the internal part, wherein at least one of the side walls of the external part is fixed connected with the, at least one, wing that protrudes radially inwards towards the internal part, which wing demonstrates a surface that faces radially inwards and that has a circular concave curvature for connection with an outwardly facing circular convex contact surface at the internal part.

2. The bearing arrangement according to claim 1, wherein the side walls of the external part are bolted fixed to each other, whereby one of the side walls is bolted fixed also at the, at least one, wing that protrudes radially inwards towards the internal part.

3. The bearing arrangement according to claim 1, wherein one of the side walls is designed integrated with the, at least one, wing that protrudes radially inwards towards the internal part.

4. The bearing arrangement according to claim 1, wherein the two side walls of the external part are designed as one piece and the, at least one, wing that protrudes radially inwards towards the internal part is designed by the milling of a groove that passes round the circumference and that connects to the, at least one, wing.

5. The bearing arrangement according to claim 1 wherein the external part comprises two wings that protrude radially inwards towards the internal part, and that the internal part comprises two wings that protrude radially outwards towards the external part, whereby the wings limit four compartments or chambers between the external part and the internal part.

6. The bearing arrangement according to claim 5, wherein two diametrically located compartments or chambers are pairwise connected with each other through pressure-equalisation passages that pass through the internal part.

7. The bearing arrangement according to claim 1 wherein the external part and the internal part are arranged surrounding a shaft, whereby either the external part or the internal part is connected to the shaft in a manner that does not allow rotation.

Description

[0017] The invention will now be described in more detail in the form of a non-limiting embodiment as an example, shown with a design that is in particular suitable to achieve a reciprocating rotary motion for a saw blade in a forestry machine. The drawings show as follows:

[0018] FIG. 1 shows a schematic cross-section through a turnable unit in which the bearing arrangement according to the invention is applied, FIG. 1a shows one half of an axial section through the turnable unit along the line A-A shown in FIG. 1, FIG. 1b shows one half of an axial section through the turnable unit along the line B-B shown in FIG. 1, FIG. 1c shows one half of an axial section through the turnable unit along the line C-C shown in FIG. 1,

[0019] FIG. 2 shows a longitudinal section through the turnable unit shown in FIG. 1, FIG. 2a shows an end view of the turnable unit shown in FIG. 2 where the dot-dash line A-A shows the location of the section shown in FIG. 2,

[0020] FIG. 3 shows a cross-section through the turnable unit shown in FIG. 1 at another axial position,

[0021] FIG. 4 shows a longitudinal section through the turnable unit shown in FIG. 1 at a position other than that shown in FIG. 2, FIG. 4a shows an end view of the turnable unit shown in FIG. 4 where the dot-dash line A-A shows the location of the section shown in FIG. 4,

[0022] FIG. 5 shows a perspective view of a side part of the turnable unit according to the invention in another embodiment, FIG. 5a shows a frontal view of the side part shown in FIG. 5, and FIG. 5b shows a cross-section through the side part shown in FIG. 5a along the dot-dash line C-C.

[0023] Thus, FIG. 1 shows a turnable unit comprising an external principally ring-shaped part 1 and an internal principally ring-shaped part 7, where the external part 1 forms a housing that surrounds the internal part 7 in the radial direction and where it also at least partially surrounds the internal part 7 in the axial direction. The external ring-shaped part 1 comprises an internal contact surface 2, which also is principally ring-shaped, and two wings 3 and 4 that are diametrically located and protrude radially inwards. The external ring-shaped part comprises also two side walls 5 and 6 that protrude downwards and radially inwards outside of the wings 3 and 4 and that surround these wings (as is shown most clearly in FIG. 1a- FIG. 1c). The internal principally ring-shaped part 7 demonstrates a contact surface 8 that faces radially outwards, and two wings 9 and 10 that are diametrically located and protrude radially outwards from this. The external part 1 and the internal part 7 are mutually turnable around a centre of rotation R. The wings 3 and 4 of the external part 1 protrude radially inwards such that the surfaces of the wings 3, 4 that face radially inwards are in close connection with the contact surface 8 of the internal part 7 that faces outwards, and in a corresponding manner the wings 9 and 10 of the internal part 7 protrude radially outwards such that their surfaces that face outwards are in close connection with the contact surface 2 of the external part 1 that faces inwards. The surfaces of the wings 3, 4 of the external part that face inwards have a circular concave curvature, with a radius of curvature that corresponds to the radius of curvature of the outwardly facing circular convex contact surface 8 of the internal part. In a corresponding manner, the surfaces of the wings 9, 10 of the internal part that face outwards have a circular convex curvature, with a radius of curvature that corresponds to the radius of curvature of the inwardly facing contact surface 2 of the external part. It is appropriate that the play between the wings 9, 10 of the internal part and the inwardly facing contact surface 2 of the external part, as also the play between the wings 3, 4 of the external part and the outwardly facing contact surface 8 of the internal part, have a magnitude of the order of 0.01-0.04 mm. The wings 3, 4 and the wings 9, 10 have their principal extension in the circumferential direction.

[0024] As is made clear by FIG. 1, compartments or chambers 11, 12, 13, 14 are formed between the external part 1 with its wings 3, 4 and the internal part 7 with its wings 9, 10, which chambers are limited by the internal contact surface 2, the inwardly facing sides of the side walls 5, 6, the outwardly facing contact surface 8 and the sides of the wings 3, 4 and 9, 10. The heights of the wings 3, 4 and of the wings 9, 10 in the radial direction thus correspond to the heights of the compartments or chambers 11, 12, 13, 14 in the radial direction, which height is a fraction of the radial dimension of the external part 1. An oil passage 15, 16 is connected to two of the chambers 12, 13 for the supply of hydraulic oil and for its removal, respectively, or vice versa. If oil is supplied to the chamber 12 through the oil passage 15, the pressure in this chamber will increase, which, if the internal part is fixed connected to a fitting, leads to the external part starting to turn in a clockwise direction through the volume of the chamber 12 increasing, while oil at the same time flows out of the chamber 13 through the oil passage 16 through the volume in this chamber 13 decreasing due to the rotation. Corresponding processes occur also in the chambers 14 and 11. Corresponding oil passages may be connected also to these chambers from an external supply, or through an internal system of passages as will be described in association with FIG. 3.

[0025] Thus, FIG. 1a shows the right half of a section along the line A-A in FIG. 1, and it is there made clear not only that the side walls 5, 6 of the external part 1 surround the internal part 7, but also that the inwardly facing surface of the wing 4 is in contact with the outwardly facing contact surface of the internal part 7.

[0026] FIG. 1b shows the upper half of a section along the line B-B in FIG. 1, and in this case the wing 10 of the internal part is in contact with the inwardly facing contact surface 2 of the external part.

[0027] FIG. 1c shows the upper half of a section along the line C-C, and in this case the section does not pass through any of the wings, but what is seen is instead the section through the chamber 12, with the inwardly facing 2 and outwardly facing 8 contact surfaces of the external part and the internal part.

[0028] FIG. 2 shows a longitudinal cross-section through a turnable unit with a bearing arrangement according to the invention, taken along the section line A-A in FIG. 2a. The external part is here shown as a two-part ring, consisting of a side ring 17 and an external ring 18, where it is the external ring 18 that supports the wings 3, 4 that are shown in FIG. 1. Furthermore, the external ring 18 radially surrounds the internal ring-shaped part 7, which is in turn connected at its second side with a flange 19, by it being bolted to this with a bolt 20. The side ring 17 is bolted to the external ring 18 by means of bolts 21, arranged in a circle of bolts adjacent to the complete circumference of the two rings 17, 18. The side ring 17 is, furthermore, also bolted to the wings 3, 4 of the external ring by means of bolts 22 in order to increase the rigidity of the connection with these wings.

[0029] FIG. 2a shows an end view of the bearing arrangement shown in FIG. 2 as would be seen from the left of this drawing. Thus, it is the front surface of the side ring 17 that is seen, and the bolts 22 that connect the side ring 17 with the wings of the external ring are located on this circle of bolts with the bolts 21, and inside of this circle at the locations of the wings 3, 4. Also the position of the section, as it is shown in FIG. 2, is shown in the drawing by the dot-dash line A-A.

[0030] Also FIG. 3 shows a cross-section through the turnable unit, to be more precise a cross-section through the external ring 18 and the internal part 7. Thus, the drawing shows the two inwardly directed wings 3, 4 of the external ring 18, and the holes 21 for the bolts of the circle of bolts and the holes 22 for the bolts that are to be connected to the wings. At the internal part 7, the drawing shows the two outwardly directed wings 9, 10 of this part. The drawing shows also the chambers 11, 12, 13, 14 that have been formed between the external ring, the internal part and the wings. The drawing, however, is intended to show in particular the internal system of passages that is preferably arranged for the supply of oil between the chambers. This system of passages comprises a first transverse passage 23 that joins the chamber 12 with the chamber 14, and a second transverse passage 24 that joins the chambers 11 and 13 to each other. The second transverse passage 24 is shown in the drawing by dashed lines since it is located in a deeper axial plane when the arrangement is viewed as in the drawing. When oil under pressure is supplied to the chamber 12 through the oil passage 15, this oil will flow from the chamber 12 through the transverse passage 23 and into the chamber 14, and, since the chambers 12 and 14 will in this case be enlarged in the circumferential direction, the chambers 11 and 13 will instead be reduced in volume, and oil will then flow from the chamber 11 through the second transverse passage 24 to the chamber 13 and through the oil passage 16 out of the chamber to a connected oil tank.

[0031] FIG. 4 shows a section similar that in FIG. 2, but in a different angular position as is made clear by the dot-dash line A-A in FIG. 4a. It is here made clear that the section passes through a part that includes the two wings 9, 10 of the internal part 7, where these are in contact with the inwardly facing contact surface 2 of the external part.

[0032] FIG. 5 shows an alternate design of the side ring 17 of the external part 1, and removable wings 25, 26 are arranged at the front surface on the inner surface of the side ring, i.e. on the surface that faces inwards into the turnable unit. The removable wings 25, 26 are connected with the side ring 17 through bolts inserted through the holes 22 and tightened in the removable wings. An external ring 18 can subsequently be mounted fixed at this side ring 17 with the aid of bolts inserted into the bolt holes 21 in the circle of bolts. Also an internal part 7 is mounted such that it is held fixed by the external ring 18, in order to form a unit that is in principle similar to that shown in the other drawings. Also the wings arranged at the internal part may be arranged in a corresponding manner as the wings 25, 26 at the side ring 17. A turnable unit of this type, however, may not be subject to the same high pressure as the embodiments shown in the other drawings.

[0033] As is made clear by several of the drawings, sealing rings 27 are arranged in grooves 28 in contact surfaces between the external part and the internal part, although these contact surfaces are not subject to the same pressure that causes wear that occurs between the other contact surfaces 2, 8 and the wings, and the play at the locations at which these seals 27 are arranged is greater than the play that can be accepted in order to achieve the hydrostatic pressure that seals against the wings.

[0034] It has been mentioned above that the embodiments of the invention shown here have been constructed for a reciprocating rotary motion of a saw blade. In such an application, thus, either one or the other of the external part and the internal part is connected to the saw blade. This can then, with the design shown here, be rotated with the saw blade in a reciprocating motion through an angle that is in practice not greater than approximately 60, with four wings arranged in the turnable unit. The second part is in this case fixed connected with a shaft, with a centre of rotation R as has been mentioned above, and in this application the shaft that is connected with the second part is a hollow shaft that can, in turn, surround a further shaft that can rotate within the hollow shaft and that is required to be arranged in order to drive the chain of the saw blade.

[0035] It is obvious for one skilled in the arts that a bearing arrangement of the type that has been described above can be used for many applications in which two parts are to be mutually rotated and that function at relatively high pressure in order to be able to handle heavy loads. It is obvious for one skilled in the arts also that the arrangement can comprise only one wing on each part, or more than two wings on each part. In general, the greater the number of wings that the unit comprises, the higher the torque that can be achieved, while, however, at the same time the angle of rotation that can be used in the unit is reduced by a corresponding degree.

[0036] If the bearing arrangement is used as a pump, an external torque is instead applied to the external or internal part in order to rotate it, while the other of the two parts is stationary, and in this case hydraulic oil can in a corresponding manner be pumped at high pressure through the chambers being alternately caused to expel oil at a high pressure.