This invention relates to a resilient joint bushing for use in joining two structural members.
Typically, a bushing is used to connect two structural members that move relative to one anther. Normally, bushings include an inner sleeve of a predetermined diameter secured to one of the structural members and an outer sleeve having a diameter larger then the inner sleeve. In one type of bushing, the inner sleeve is suspended within the outer sleeve in a concentric manner by a resilient and deformable material. The deformable material is typically bonded to both the inner and outer sleeves. The deformable material disposed between the inner and outer sleeves allows a discrete amount of movement. The movement between inner and outer sleeves may be longitudinal or rotational. Such bushings dampen the transmission of vibrations from one structural member to another reducing noise created by such vibrations. This type of bushing does not direct motion between the structural parts.
One other type of bushing is a laminated bushing. Sheets of metal and deformable material are layered to form this type of bushing. The laminated bushing can have greater strength and durability properties than the above-mentioned bushing. Further, laminated bushings may be constructed in a manner that can aid in the direction of movement between structural members. This is accomplished by layering the alternating metal sheets to provide for shear in only desired directions. Laminated bushings however are costly in comparison to typical bushings.
For these reasons, it is desirable to develop a low cost laminated bushing to provide additional strength and durability while providing a cost efficient alternative to conventional bushings.
One disclosed embodiment of this invention is a laminated bushing formed by spirally winding a metal sheet with a resilient material to provide a range of motion proportional to an applied force.
The laminated bushing includes a metal sheet spirally wound about a first longitudinal axis forming a spirally shaped cavity. A deformable resilient material such as rubber is disposed on one side of the metal sheet and within the cavity. The metal sheet forming the spiral shaped cavity may mechanically compress the resilient material disposed within the cavities. Alternatively, the resilient material can be vulcanized once within the laminated bushing is formed. The spirally wound laminated bushing includes inner and outer sleeves concentric about the longitudinal axis and that move relative to one another in direct proportion to the material deformation properties of the resilient material disposed between the metal sheet. However, because the resilient material is alternatively layered with the metal sheet the direction of movement between the inner sleeve and the outer sleeve is controlled by the specific configuration of the laminated bushing.
The configuration of the laminated bushing can be adapted to provide various directions of movement between two fastened structural members. In one embodiment, the inner sleeve is concentric with the outer sleeve. The outer sleeve forms a continuous cylinder and movement of the inner sleeve relative to the outer sleeves can occur in many planes.
In another embodiment, the laminated bushing includes a plurality of grooves disposed annularly about the longitudinal axis. Movement of the resilient material is resisted at a greater rate in a direction across or perpendicular to the grooves. In this way the grooves can be configured to direct motion between the two structural members by increasing resistance to movement across the grooves. Further embodiments include grooves that are disposed along the longitudinal axis, and grooves that are spirally wound about longitudinal axis.
The invention includes the method of constructing a spirally wound bushing including the steps of bonding a resilient deformable material to a least one side of a metal sheet, then rolling the metal sheet over itself about a longitudinal axis such that a plurality of spirally wound cavities are formed. The method further includes forming the spirally wound cavities such that the resilient deformable material is compressed within the spiral cavities.
The laminated bushing of the subject invention provide the benefits of increased strength and durability along with providing a means of directionally controlling movement of a structural member.
The various features and advantages of this invention will become apparent to those skilled in the art from the following detailed description of the currently preferred embodiment. The drawings that accompany the detailed description can be briefly described as follows:
Referring to the FIGS., wherein like numerals indicate like or corresponding parts throughout the several views and embodiments, a laminated bushing generally indicated at 10 is shown in FIG. 1. The laminated bushing 10 includes a metal sheet 12 spirally wound about a longitudinal axis 14 to form a spirally shaped cavity 20. A resilient material 16 such as rubber is disposed between the metal sheet 12 and within the spiral shaped cavity 20. Preferably, the resilient material 16 is mechanically compressed between the metal sheets 12. Alternatively, the resilient material 16 can be rubber that is vulcanized after formation of the luminated bushing 10. It should be understood that the resilient material 16 could be of any type known in the art. Preferably, the inner sleeve 22 is rotatable relative to an outer sleeve 18 in a proportional manner related to the specific material properties of the resilient material 16. The spirally wound metal sheet 12 is inserted into the outer sleeve 18. The inner sleeve 22 is formed concentric with the outer sleeve 18 about the longitudinal axis 14. The inner sleeve 22 is movable along the longitudinal axis 14 relative to the outer sleeve 18 in a proportional manner dependent on the specific properties of the resilient material 16.
Referring to
Referring to
Referring to
The laminated bushings 10 enable control of the direction of motion by using alternating layers of metal sheet 12 and resilient material 16 with or without the formed geometry. The embodiments of the laminated bushing described and shown in
Referring to
Referring to
Referring to
Referring to
Referring to
The resilient material 16 is mechanically compressed within the spirally shaped cavity 20 during the winding step to form alternating layers of metal sheet 12 and resilient material 16. Alternatively, the resilient material 16 is composed of rubber and adhered to the metal sheet 12 by a vulcanization process as is known in the art. The vulcanized resilient material 16 adheres to the metal sheet 12 of the laminated bushing 10.
The method also includes the step of mechanically forming a plurality of grooves within the metal sheet. As discussed hereinabove, the grooves 24 may be of any configuration and extend in any direction. The resilient material is then adhered to the metal sheet 12 and wound to form the spirally shaped cavity 20.
Referring to
The foregoing description is exemplary and not just a material specification. The invention has been described in an illustrative manner, and should be understood that the terminology used is intended to be in the nature of words of description rather than of limitation. Many modifications and variations of the present invention are possible in light of the above teachings. The preferred embodiments of this invention have been disclosed, however, one of ordinary skill in the art would recognize that certain modifications are within the scope of this invention. It is understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. For that reason, the following claims should be studied to determine the true scope and content of this invention.
Number | Name | Date | Kind |
---|---|---|---|
1541276 | Powell | Jun 1925 | A |
1729328 | Chilton | Sep 1929 | A |
2001257 | Lecler | May 1935 | A |
2073419 | Houdaille et al. | Mar 1937 | A |
2176971 | Klotsch | Oct 1939 | A |
2346574 | Guy | Apr 1944 | A |
2358518 | Kraft | Sep 1944 | A |
2900182 | Hinks | Aug 1959 | A |
3071422 | Hinks | Jan 1963 | A |
3235941 | Krotz | Feb 1966 | A |
3690639 | Brandon et al. | Sep 1972 | A |
3750249 | Brandon et al. | Aug 1973 | A |
3869113 | Dudek | Mar 1975 | A |
3998503 | Van Wyk | Dec 1976 | A |
4108508 | Clinard, Jr. | Aug 1978 | A |
4349184 | Peterson et al. | Sep 1982 | A |
4687223 | Miyoshi et al. | Aug 1987 | A |
4819385 | Baumann et al. | Apr 1989 | A |
5062193 | Thompson | Nov 1991 | A |
5332255 | Velazquez | Jul 1994 | A |
5413374 | Pierce | May 1995 | A |
5609353 | Watson | Mar 1997 | A |
6425576 | Choi | Jul 2002 | B1 |
Number | Date | Country | |
---|---|---|---|
20030121122 A1 | Jul 2003 | US |