GB2095347A

GB2095347A - Seals

Info

Publication number: GB2095347A
Application number: GB8109011A
Authority: GB
Original assignee: Komatsu Ltd
Current assignee: Komatsu Ltd
Priority date: 1981-03-23
Filing date: 1981-03-23
Publication date: 1982-09-29
Also published as: DE3111670A1; GB2095347B

Abstract

A seal for a joint subjected to oscillatory motion has a seal ring which is W-shaped in an unloaded condition and which encompasses a load ring 9. The W-shaped seal ring comprises a driving flange 10, a sealing flange 11 and a bight portion 12 inter-connecting the two flanges. The load ring 9 is fitted in the seal ring to force the driving flange into an interference fit with the counterbore walls so as to cause the driving torque to be applied through the seal ring. The thickness of the driving flange 10 and the bight portion 12 is made substantially the same so as to ensure enough rigidity in the radial direction while allowing the seal ring to deform readily in the axial direction. A clearance 14 is thus maintained between the seal ring and a thrust ring 7. <IMAGE>

Description

SPECIFICATION Seal assembly with load ring This invention relates to a seal adapted to be used for track link connections for construction vehicles such as bulldozers and the like.

One of the conventional seal rings which has been employed in the seals of the kind specified comprises, as disclosed in U.S. Patent No.3,841,718, a driving flange, a sealing flange and a bight portion of a thin wall thickness connecting the two flanges.

When this seal ring is set together with a load ring in a counterbore defined by a bushing and a link, because the thickness of the bight portion is thin, the bight portion tends to deform inwardly to a large extent and contact with a thrust ring so that the inclination of the load-deflection curve will change and therefore required stable load-deflection characteristics can not be obtained.

Further, because the seal ring of the abovementioned type has a small rigidity, when it is set in loaded position, the seal flange tends to be subjected to an abnormal deformation, thus causing earlier weardown of the sealing surface.

Another type of seal assembly is disclosed in U.S.

Patent No. 4,062,550, the assignee of which is the same as that of the present application. However, it revealed by the results of later experiments that the seal ring of this type could not exhibit such a durability as expected. The reason envisaged for it is that, because the sealing flange of the seal ring is kept into contact with the end face of the bushing in a wide sealing surface, there is a tendency of occurrence of oil leaks.

It is therefore an object of the present invention to provide a seal assembly with a backup load ring which can effectively overcome the above noted problems. Another object of the present invention is to provide a seal assembly comprising a seal ring and a backup load ring wherein the seal ring has a high rigidity against the deformation in the radial direction while allowing an easy deformation in the axial direction.

In accordance with an aspect of the present invention, there is provided a seal assembly comprising: first and second axially spaced members mounted for relative rotation about a common axis, said first member having a counterbore formed in one face thereof, said second member having an end face opposite the counterbore; a third member disposed between said first and second members; a seal ring of tough abrasion-resistant material having a W-shaped cross-section in an unloaded condition disposed within the counterbore with the W-shaped cross-section defining an annular groove facing the side wall of the counterbore, said seal ring including a driving flange engaged in non-rotative driving contact with the side wall and an end wall of the counterbore at the juncture of these walls, a sealing flange adapted to be engaged in annular lip sealing rotative contact with the end face of said second member and a bight portion interconnecting said driving and sealing flanges, the thickness of the driving flange and the bight portion being made substantially same and the thickness of the sealing flange being made thicker than that of the driving flange and the bight portion; and a load ring of elastomeric material having substantial spring response characteristics, said load ring being disposed within the annular groove of the W-shaped seal ring and engaging substantially the entire inner walk surface of the sealing flange and being axially compressed between the driving flange and the sealing flange, wherein said seal ring is compressed between said first and second members when loaded in place and the shape of cross-section is transformed from W-shape to C-shape having a substantially straight bight portion interconnecting the flanges with keeping a spacing between the bight portion of said seal ring and said third member.

The above and other objects, features and advantages of the present invention will be readily apparent from the following description taken in conjunction with the accompanying drawings.

Fig. lisa longitudinal sectional view of a seal assembly for linkage connectings of endless tracks according to the present invention; Fig. 2 is an enlarged view of Fig. 1 in which the seal in an unloaded free condition is shown by imaginary lines; Fig. 3 is a cross-sectional view of the seal which is unloaded free condition; Fig. 4 is a graph showing a relationship between a load imposed on the seal ring and a deflection thereof in the axial direction; and Fig. 5 is a comparative graph showing the service life of seal assemblies of the present invention and first and second prior art devices mentioned in the background of the invention, the first prior art being U.S. Patent No. 3,841,718 and second prior art being U.S. Patent No. 4,062,550.

The present invention will now be described below by way of example only with reference to the accompanying drawings.

In the drawings, reference numeral 1 denotes one of links which has a recess 2 formed therein and in which a pin 3 is forcibly fitted.

Another link 5 is fitted through a bushing 4 to the pin 3.

One end of the bushing 4 is inserted into the recess 2 to define a counterbore 20 therebetween.

Mounted in the counterbore 20 are a seal 6 and a thrust ring 7.

The seal 6 comprises a seal ring 8 and a load ring 9. The seal ring 8 has a generally W-shaped crosssection and comprises a driving flange 10, a sealing flange 11 having a lip-like sealing surface 13 and a bight portion 12 connecting the two flanges.

As shown in Figure 3, if the thickness of the driving flange 10 of the seal ring 8 is represented by to and those of the bight portion 12 at two places are indicated by t2 and t3, respectively, the following relationship exists.

The drawings originally filed were informal and the print here reproduced is taken from a later filed formal copy.

ti = t2 = t3 i . 1.0 If and when the ratr of deflection O' o'.t sus216, r = (B, - B2)/E, is set at about 17%, the sea riang 8 can possess a sufficient rigidity without inpaiting its inherent flexibility.

When the seal ring 8 is in free state, there is provided a difference H between the highest part of the bight portion 12 and the lowest part thereof. When the seal ring 8 is set into the counterbore 20, the difference H will become approximately zero thereby eliminating the interference between the seal ring 8 and the thrust ring 7.

When the above-mentioned seal 6 is set in the counterbore 20, the lip 13 of the sealing flange 11 is urged against the end face of the bushing 4, and a space 14 is formed between the seal ring 8 and the thrust ring 7.

Since the seal ring 8 has an approximately equal wall thickness except the sealing flange 11, it possesses a large rigidity. Further, because the seal ring 8 per se is not brought into contact with the thrust ring 7, the rate of fluctuation in the loading excerted on the lip sealing face 13 becomes low and stable. A load-deflection curve of the seal ring 8 is shown by reference numeral ll in Figure 4. In this graph, reference numeral I denotes a load-deflection curve of the seal assembly disclosed in U.S. Patent No.3,841,718.

Further, since the seal ring 8 according to the present invention has a generally W-shaped crosssection, the rigidity of the seal ring in the radial direction can be increased, whilst its rigidity in the axial direction can be reduced because of the presence of readily deformable W-shaped wavy portion. When the rigidity of the seal ring in the radial direction is large, the possible occurrence of abnormal deformation and bending of the seal ring when it is set in position in the counterbore can be prevented.

Further, when the rigidity in the axial direction is small, a seal assembly having stable load-deflection characteristics and a small spring constant can be obtained.

Figure 5 is a graph showing the relationship between the service time of seal assemblies and the rate of generation of seizure of bushings due to oil leaks wherein a comparison between the seal assembly of the present invention and the aforementioned two types of prior art seal assemblies are shown. As can be clearly seen from the graph, as compared to the prior art seal assemblies, in the case of the seal assembly of the present invention, there occurs almost no seizures of the bushing even if its service time is extended.

As described in detail hereinabove, the present invention is characterized by that the seal 6 adapted to be set in the counterbore 20 defined by the link 1 and the bushing 4 is comprised of a seal ring 8 having a generally W-shaped cross-section and having a generally equal wall thickness except sealing flange 11 and of a load ring 9 to be fitted into the seal ring 8, and a space or clearance 14 is formed between the seal ring 8 and the thrust ring 7.

Therefore, the seal ring 8 per se can possess an appropriate rigidity without impairing its inherent flexibility, and because the seal ring 8 is not brought into contact with the thrust ring 7, the rate of fluctua tion in the load exerted on the sealing face will become low and stable thereby elirninating a possible earth and sand intrusion and enhancing sealing effect.

It is to be understood that the foregoing description is merely illustrative of a preferred embodiment of the present invention, and that the scope of the invention is not to be limited thereto, but is to be determined by the scope of the appended claim.

Claims

1. Aseal assemblycomprising: first and second axialtyspaced members mounted for relative rotation about a common axis, said first member having a counterbore formed in one face thereof, said second member having an end face opposite the counterbore; a third member disposed between said first and second members;; a seal ring of tough abrasion-resistant material having a W-shaped cross-section in an unloaded condition disposed within the counterbore with tlhe W-shaped cross-section defining an annular groove facing the side wall of the counterbore, said seal ring including a driving flange engaged in non-rotative driving contact with the side wall and an end wall of the counterbore at the juncture of these walls, a sealing flange adapted to be engaged In annular lip sealing rotative contact with the end face of said second member and a bight portion interconnecting said driving and sealing flanges, the thickness of the driving flange and the bight portion being made substantially same and the thickness of the sealing flange being made thicker than that of the driving flange and the bight portion; and a load ring of elastomeric material having substantial spring response characteristics, said load ring being disposed within the annular groove of the W-shaped seal ring and engaging substantially the entire inner wall surface of the sealing flange and being axially compressed between the driving flange and the sealing flange; wherein said seal ring is compressed between said first and second members when loaded in place and the shape of cross-section is transformed from W-shape to C-shape having a substantially straight bight portion interconnecting the flanges with keeping a spacing between the bight portion of said seal ring and said third member

2. A seal assembly substantially as hereinbefore described with reference to the accompanying drawings.