EP1631753A2 - A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same - Google Patents

A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same

Info

Publication number
EP1631753A2
EP1631753A2 EP04754966A EP04754966A EP1631753A2 EP 1631753 A2 EP1631753 A2 EP 1631753A2 EP 04754966 A EP04754966 A EP 04754966A EP 04754966 A EP04754966 A EP 04754966A EP 1631753 A2 EP1631753 A2 EP 1631753A2
Authority
EP
European Patent Office
Prior art keywords
component
isolator
shaft assembly
housing
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP04754966A
Other languages
German (de)
French (fr)
Other versions
EP1631753A4 (en
Inventor
Douglas Power
Bernie Rice
Robert Paladichuck
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cooper Standard Automotive Inc
Original Assignee
Cooper Standard Automotive Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US10/458,514 external-priority patent/US7204479B2/en
Application filed by Cooper Standard Automotive Inc filed Critical Cooper Standard Automotive Inc
Publication of EP1631753A2 publication Critical patent/EP1631753A2/en
Publication of EP1631753A4 publication Critical patent/EP1631753A4/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/387Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type comprising means for modifying the rigidity in particular directions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F13/00Units comprising springs of the non-fluid type as well as vibration-dampers, shock-absorbers, or fluid springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00Springs
    • F16F1/36Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F16F1/3842Method of assembly, production or treatment; Mounting thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F5/00Liquid springs in which the liquid works as a spring by compression, e.g. combined with throttling action; Combinations of devices including liquid springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F7/00Vibration-dampers; Shock-absorbers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M1/00Frames or casings of engines, machines or apparatus; Frames serving as machinery beds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F2228/00Functional characteristics, e.g. variability, frequency-dependence
    • F16F2228/08Functional characteristics, e.g. variability, frequency-dependence pre-stressed

Definitions

  • This invention relates to a vibration isolator assembly that generically refers to a device that absorbs vibrations and dampens relative movement between two structures, such as an isolator mount, bushing assembly, cradle mount assembly, etc.
  • a typical vibration isolator includes an external housing and an internal mounting shaft joined by an isolator such as a molded elastomer (e.g., rubber).
  • the elastomer provides isolation between the housing and the mounting shaft.
  • the elastomer is molded to the housing shaft in a high-temperature molding operation. This provides a desirable bond between the elastomer and the housing, as well as between the elastomer and the mounting shaft.
  • the elastomer experiences shrinkage as the part cools. Depending on the design, an undesirable effect of this shrinkage is to impart tensile stress to the elastomer. In such cases, fatigue performance of the vibration isolator assembly is generally improved by relieving the stress.
  • the present invention discloses a vibration isolator assembly having a housing and a shaft assembly interconnected by an isolator.
  • the shaft assembly includes first and second mating components, the first component of which is connected to the elastomer.
  • the first shaft component forms a cavity of a first dimension to receive the second component having a second dimension slightly greater than the first dimension for altering stress characteristics of the vibration isolator assembly.
  • the isolator is an elastomer, and the housing may be either metal or non-metal.
  • the second mention of the second component of the shaft assembly is pre-selected to relieve molded in tensile stress, or impart compressive stress to the isolator.
  • the first component of the shaft assembly is a split member and the second component is received along the split plane.
  • the first and second components of the shaft assembly have a keyed contour relationship to selectively alter spring rate build-up characteristics
  • the first component of the shaft assembly is comprised of first and second mirror portions and the second component is received between the portions.
  • a thin layer of elastomer is interposed between the first and second components of the shaft assembly.
  • the first and second components of the shaft assembly have an "I" contour relationship to selectively alter spring rate build-up characteristics.
  • a primary benefit of the invention resides in the ability to relieve molded in tensile stress and, if desired, impart compressive stress without affecting the housing or bonded layer between the housing and the elastomer material.
  • Another benefit of the invention resides in the ability to manipulate spring rate magnitude, rate ratios, rate build-up, and component fatigue characteristics of the vibration isolator assembly.
  • Still another benefit resides in reduced tooling costs and reduced lead times associated with different designs so that more options can be made available within the constraints of a fixed or predetermined development budget.
  • Still another benefit resides in the ability to manufacture the first components more economically at a lower tolerance of form by employing the layer of elastomer which is produced at precision tolerance through mold design to account for variation and permit easy assembly of the shaft assembly.
  • Yet another benefit is the ability to make changes to a design and tuning specifications without impacting a launch schedule of the product.
  • Figure 1 is a cross-sectional view illustrating a conventional vibration isolator assembly or suspension bushing.
  • Figure 2 is an elevational view of an embodiment of the present invention.
  • Figure 3 is a cross-sectional view taken generally along the lines 3-3 of
  • Figure 4 is a perspective view of a second component of the shaft assembly separated from the remainder of the vibration isolator assembly.
  • Figure 5 illustrates a separation of a first component of the shaft assembly along a split plane for receipt of the second component.
  • Figure 6 illustrates partial insertion of the second component into the remainder of the vibration isolator assembly.
  • Figure 7 is a perspective view of the final assembly.
  • Figure 8 is an elevational view of another embodiment of the present invention, namely, a cradle mount assembly.
  • Figure 9 is a cross-sectional view taken generally along the lines 9-9 of
  • Figure 10 is an exploded perspective view of individual components of the assembly.
  • Figure 11 illustrates a further step in the assembly of the vibration isolator assembly or cradle mount.
  • Figure 12 shows enlarging the cavity of a first component of the shaft assembly.
  • Figure 13 illustrates partial insertion of the second component of the shaft assembly.
  • Figure 14 illustrates the completed assembly of the second embodiment.
  • Figure 15 is a perspective view of the completed assembly of individual components of a third embodiment.
  • Figure 16 is a perspective view of another embodiment of the housing, isolator and first component of a shaft assembly.
  • Figure 17 is a perspective view of a second component of the shaft assembly of the third embodiment.
  • Figure 18 is a perspective view of a fourth embodiment of the housing, isolator and a first component of the shaft assembly.
  • Figure 19 is a perspective view of the first component of the shaft assembly.
  • Figure 20 is a perspective view of the second component of the shaft assembly.
  • the assembly includes a housing A and a shaft B that are interconnected by an isolator such as elastomer C.
  • the elastomer is typically mold bonded to the shaft and the housing and provides the vibration damping between the shaft secured to a first structure or component that moves relative to the housing which is secured to a second structure or component.
  • Vibration isolator assembly 20 includes a housing 22.
  • the housing is a metal structure, although as will be appreciated in accordance with the present invention, alternative materials including non-metallic materials such as nylon can be used to form the housing.
  • the housing when used as a mount bushing, the housing typically adopts a generally cylindrical conformation, i.e., circular in cross section.
  • an isolator 30 Secured to an inner surface 24 of the housing is an isolator 30.
  • the isolator is often an elastomer or rubber construction because of the ability to isolate and reduce noise and vibration from being transmitted therethrough because of the elastic nature of the material. Rubber is generally an incompressible material that is displaced during loading and exhibits the desirable property that the more the rubber is compressed, the higher the stiffness.
  • the elastomer is preferably mold bonded to the inner surface 24, although it will be appreciated that other bonding arrangements such as an adhesive bond, can be used without departing from the scope and intent of the present invention.
  • an inner diameter portion 34 of the isolator is secured to a shaft assembly 40, which is preferably comprised of first and second components 42, 44.
  • the isolator is secured to a first or outer surface 46 of the first component and again is illustrated as being mold bonded thereto.
  • the first component 42 in this embodiment is defined by first and second portions 42a, 42b that are separated and have outer surfaces 46a, 46b that are bonded to the isolator, respectively.
  • Inner, facing surfaces 48a, 48b of the first component are separated along a split plane and slidably engage the second component 44 of the shaft assembly.
  • the first and second components 42, 44 of the shaft assembly have mating, keyed configurations that provide for slidable insertion of the second component into a cavity defined along the split plane between the first and second portions 42a, 42b of the first component, and likewise resist relative movement between the first and second components in other directions.
  • This mating, keyed configuration provides an interlocking feature that allows the separate components (here, three separate pieces) to merge and function as a single component.
  • the first and second portions 42a, 42b of the first component have dovetailed keyways 60 formed on opposite axial sides of central axis 62.
  • the keyways are dimensioned to receive mating, dovetailed keys or projections 64 that extend outwardly from the second component 44 of the shaft assembly.
  • the first component 42 includes first and second mirror-image portions 42a, 42b having a central rounded portion 66 that merges into generally planar, outer radial portions 68.
  • the first and second portions 42a, 42b are separable or split along the plane 70 that passes through the longitudinal axis 62.
  • the second component is similarly contoured, having a central rounded portion 76 that merges into generally planar, outer radial portions 78 disposed on diametrically opposite sides of the rounded portion.
  • This contour has met with success, still other variations or contours may be used without departing from the scope and intent of the present invention.
  • the mirror image portions 42a, 42b of the first component of the shaft assembly are integrally bonded to the isolator.
  • the portions are separable along the facing, mating surfaces along split plane 70.
  • the facing dovetailed key ways 60 define an outer radial cavity portion and the rounded portions 66a, 66b define a central cavity portion 80.
  • the cavities 80 defined by the keyways present a first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating contour of the second component.
  • the first and second portions 42a, 42b of the first component of the shaft assembly are spread apart or separated along the split plane 70 to enlarge the cavity or opening 80 and allow selective sliding receipt of the second component 44 of the shaft assembly therein.
  • This sliding receipt is represented in Figure 6, where the second component is partially received into the first component of the shaft assembly.
  • complete insertion of the second component into the first component is achieved and is represented in Figure 7.
  • the isolator is typically an elastomer molded between the housing and shaft, here between the housing and the first component 42 of the shaft assembly. When it cures, the elastomer ends up with residual tensile stress.
  • the prior art has addressed this in a different manner.
  • using a two-part shaft assembly alters the stress characteristics of the vibration isolator assembly.
  • the residual tensile stress in the elastomer is removed upon complete insertion of the second component into the first component. If the second component is made even larger, then a predetermined compressive stress is formed in the isolator/elastomer. All of this is achieved without affecting or adversely impacting on the bond between the housing and elastomer, and likewise between the elastomer and shaft assembly.
  • variable compressive stresses can be introduced into the elastomer.
  • the first effect is associated with spring rate.
  • the compressive rate characteristics of the main elastomer elements will increase in magnitude, roughly in proportion to the degree of precompression, while the shear rate characteristics of the same elastomer elements will remain relatively unaffected. This results in a change in the compressive-to-shear rate ratio of the final assembly.
  • the second effect deals with fatigue life.
  • an elastomer or rubber can tolerate increasing levels of compressive stress under cyclic loading much better than it tolerates smaller amounts of tensile stress.
  • fatigue life of the assembly can be enhanced.
  • the forced separation of the molded split shaft assembly relieves the tensile stress resulting from part shrinkage, and imparts or introduces a desired compressive stress to the molded rubber, if desired.
  • the elastomer is radially continuous between the housing and the shaft assembly in one diametrical dimension (e.g., in the vertical direction as shown) and is discontinuous in another diametrical direction (e.g., in the horizontal direction as shown) through the inclusion of openings 90, 92.
  • the openings 90, 92 are generally symmetrical in the vertical and horizontal directions, but need not necessarily be symmetrical or similarly shaped.
  • boundary rubber 94, 96 ( Figure 2) define snubbing rubber extending inwardly from the housing in the horizontal direction.
  • the gap between the shaft assembly and the boundary rubber is selectively altered.
  • the width dimension of the second component of the shaft assembly i.e., by extending the planar portions 78 radially outward
  • the gap between the shaft assembly and the boundary rubber is selectively altered.
  • the amount of travel that the shaft assembly proceeds through before contacting the boundary rubber on the housing will decrease. This transfers loading and stress more rapidly from the main central rubber elements to the exterior boundary or snubbing elements, and effectively alters the spring rate build-up characteristics. This has the effect of providing additional tuning options and improved fatigue durability.
  • the present invention is also useful in other vibration isolator assemblies such as the cradle mount shown in Figures 8-14. Since much of the structure and function is substantially identical, reference numerals with a primed suffix refer to like components (e.g., housing is referred to by reference numeral 22"), and new numerals identify new components.
  • the primary distinction relates to the frame 100 of the vehicle in which the housing 22' of the cradle mount assembly 20" is also molded to the first component portions 42a', 42b' of the shaft assembly.
  • the subassembly, i.e., housing 22" is initially inserted into the frame 100, namely opening 102.
  • the housing 22' is preferably metal, but is should be noted that other composite or hard materials may be used.
  • the outer dimension of the housing can relate to any shape such as rectangular, square, circular, triangular, or any other shape or surface depending on the size and requirements needed for the end use.
  • the shaft assembly is shown as being located at or near the center point of the housing, although that could be varied.
  • other materials e.g., cast, extruded, powdered metal, forgings, cold headed steel, or still other materials of construction may be used without departing from the scope and intent of the invention.
  • the number and/or shape of the openings can also be varied, and the elastomer isolator that is bonded to the housing components may be secured thereto with any other type of bonding.
  • the first and second components 42", 44" of the shaft assembly have mating, keyed configurations that provide for slidable insertion of the second component into a cavity defined by the first component.
  • This mating, keyed configuration provides an interlocking feature that allows the separate components to merge and function as a single component.
  • the first component has enlarged dove-tailed keyways 60" formed on opposite axial sides of the central longitudinal axis 62". The keyways are dimensioned to receive mating, dove-tailed keys or projections 64" that extend outwardly from the second component 44" of the shaft assembly.
  • the first component 42" has a central, rounded (although no circular) portion 66" that merges into generally planar, outer portions 68".
  • the second component is similarly contoured, having a central portion 76" that merges into generally planar, outer portions 78" disposed on diametrically opposite sides of the central portion.
  • the facing dovetailed key ways 60" define an outer cavity portion and the non-rounded portions 66" define a central cavity portion 80".
  • the cavities present a first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating contour of the second component and allow selective sliding receipt of the second component 44" of the shaft assembly therein. Accordingly, as it relates to the first embodiment and specifically when compared with the enlarged dove-tailed projections 64" and keyways 60", this configuration reduces tolerance requirements for the dove-tail locking feature and simplifies assembly of the shaft assembly into the cavity portion.
  • the first component 42'" in this embodiment is defined by first and second mirror portions 110a, 110b that are separated and have outer surfaces 114a, 114b that are bonded to the isolator 30'", respectively. Inner facing surfaces 116a, 116b of the first component are separated by the isolator and slidably engage the second component 44"" of the shaft assembly.
  • the first and second components 42'", 44"' have mating configurations that provide for slidable insertion of the second component into a cavity 80'" defined between the first and second portions 110a, 110b of the first component and the isolator 30'", and likewise resist relative movement between the first and second components in other directions. This mating configuration provides an interlocking feature that allows the separate components to merge and function as a single component.
  • the second component 44'" of the shaft assembly (sometimes referred to as the spreader component) has a general "I" or I-beam contour with keyed portions 118a, 118b extending from a central portion 119.
  • the first and second portions 110a, 110b of the first component have curved end portions 120a, 120b ( Figure 19) dimensioned to receive the "I" contour of the second component.
  • the inner facing surfaces 116a, 116b of the first and second portions 110a, 110b of the first component 42"' have a thin layer or skin 122 of elastomer bonded thereto ( Figure 18).
  • the elastomer 122 bonded to the inner facing surfaces 116a, 116b of the first component permits the first component (sometimes referred to as a capture plate of half-shaft) to be manufactured more economically at a lower tolerance of form.
  • the elastomer layer is produced at precision tolerances through mold design thereby taking up any variation in the dimensions of the first component and allowing consistent assembly of the first component and second component.
  • alternate materials can be used to form the elastomer layer or skin.
  • the first and second portions 110a, 110b of the first component of the shaft assembly are integrally bonded to and separated by the isolator and define a central cavity portion 80'".
  • This cavity defines the first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating "I" contour of the second component.
  • the first and second portions 110a, 110b of the first component 42'" allow sliding receipt of the second component 44'" of the shaft assembly therein.
  • Figures 15-20 use first and second components that are preferably extruded designs because of the ease of manufacture and assembly. The ability to use other shapes, designs, or contours that are not extruded or conducive to extruding should be recognized as being within the scope and intent of the present invention.
  • the manipulation of spring rate magnitude, rate ratios, rate build-up, and component fatigue characteristics is accomplished using a common molded isolator or elastomer and interchangeable shaft assemblies of different designs. This is important since higher tooling costs and longer lead times are typically associated with the isolator/elastomer, while the inserted shaft can be modified quickly and economically.
  • the economical aspect of the vibration isolator assembly means that more options can also be made available within the constraints of a development budget.

Abstract

A vibration isolator assembly, such as an isolator bushing or cradle mount, includes a housing and an isolator connected to the housing. A shaft assembly includes first and second mating components, the first component being connected to the elastomer and having a cavity of a first dimension for receiving the second component having a different, second dimension therein. The differing dimensions alter the stress characteristics of the vibration isolator assembly. In the preferred arrangement, the shaft assembly includes a first component comprising first and second portions, a thin layer of elastomer interposed between the first and second components and a second component which is inserted between the portions to relieve tensile stress in the isolator and, if desired, to impart a compressive stress in the isolator. The thin layer of elastomer permits the first components to be made more economically. The first component of the shaft assembly is made at a lower dimensional tolerance and subsequently produced to a higher dimensional tolerance by molding the thin layer of elastomer to a precision tolerance.

Description

A VIBRATION ISOLATOR ASSEMBLY HAVING ALTERED STRESS CHARACTERISTICS AND METHOD OF ALTERING STRESS CHARACTERISTICS OF SAME
Background of the Invention
[0001] This invention relates to a vibration isolator assembly that generically refers to a device that absorbs vibrations and dampens relative movement between two structures, such as an isolator mount, bushing assembly, cradle mount assembly, etc.
[0002] A typical vibration isolator includes an external housing and an internal mounting shaft joined by an isolator such as a molded elastomer (e.g., rubber). The elastomer provides isolation between the housing and the mounting shaft. Typically, the elastomer is molded to the housing shaft in a high-temperature molding operation. This provides a desirable bond between the elastomer and the housing, as well as between the elastomer and the mounting shaft. After the molding operation, the elastomer experiences shrinkage as the part cools. Depending on the design, an undesirable effect of this shrinkage is to impart tensile stress to the elastomer. In such cases, fatigue performance of the vibration isolator assembly is generally improved by relieving the stress. One common way of relieving the stress is to pass the external housing through a funnel or reduced diameter opening to permanently reduce the diameter of the assembly. Such an arrangement is shown and described in the prior art representation of Figures 11-13 of US Patent No. 6,094,818, and is also well known to one skilled in the art.
[0003] Also, due to general poor fatigue performance of an elastomer under tensile loading, further enhancements to fatigue life may be realized by going beyond the simple relief of imparted tensile stresses and imparting compressive stress to the elastomer. Unfortunately, conventional methods for reducing the outer diameter of the isolator are limited in their effectiveness when there is a desire to impart compressive stress to the elastomer. This is due, for example, to negative effects on the bonding between the isolator and housing materials, i.e., the adhesive layer bonding between the isolator and housing, and isolator and the mounting shaft. There are also limits on the extent of deformation that the housing material can undergo. [0004] It will also be appreciated that a substantial amount of time and money are required to design, redesign, tool, and retool a product. The development cycle requires significant design and engineering time to be sure that the final product meets the final product specifications. If the specifications are altered during the development process, a need exists to remove, modify, and reinstall the assembly in a short time frame. With regard to producing manufactured mounting and vibration isolators for power trains, i.e., engines/transmissions in various consumer and commercial vehicles, as well as a development tool for engineering purposes that allows optimization and tuning of a power train mounting system for improved isolation and performance, a need exists to address tuning and durability issues. If such issues surface late in a program cycle, it is necessary to implement changes without a major redesign or a long retooling time, even though the basic characteristics of the isolator are being modified.
[0005] Thus a need exists to enhance the durability and tuning ability of a vibration isolator assembly. Means to relieve residual tensile stress, as well as vary the level of precompression of the elastomer portion, are desired. A need also exists to vary the travel limits of the elastomer portion. Lastly, there is a need to overcome these problems without major reworking of prototype or production tooling.
Summary of the Invention
[0006] The present invention discloses a vibration isolator assembly having a housing and a shaft assembly interconnected by an isolator. The shaft assembly includes first and second mating components, the first component of which is connected to the elastomer. The first shaft component forms a cavity of a first dimension to receive the second component having a second dimension slightly greater than the first dimension for altering stress characteristics of the vibration isolator assembly.
[0007] In a preferred embodiment of the invention, the isolator is an elastomer, and the housing may be either metal or non-metal. [0008] The second mention of the second component of the shaft assembly is pre-selected to relieve molded in tensile stress, or impart compressive stress to the isolator. [0009] In one embodiment, the first component of the shaft assembly is a split member and the second component is received along the split plane.
[0010] The first and second components of the shaft assembly have a keyed contour relationship to selectively alter spring rate build-up characteristics
[0011] In one embodiment, the first component of the shaft assembly is comprised of first and second mirror portions and the second component is received between the portions.
[0012] A thin layer of elastomer is interposed between the first and second components of the shaft assembly.
[0013] The first and second components of the shaft assembly have an "I" contour relationship to selectively alter spring rate build-up characteristics.
[0014] A primary benefit of the invention resides in the ability to relieve molded in tensile stress and, if desired, impart compressive stress without affecting the housing or bonded layer between the housing and the elastomer material.
[0015] Another benefit of the invention resides in the ability to manipulate spring rate magnitude, rate ratios, rate build-up, and component fatigue characteristics of the vibration isolator assembly.
[0016] Still another benefit resides in reduced tooling costs and reduced lead times associated with different designs so that more options can be made available within the constraints of a fixed or predetermined development budget.
[0017] Still another benefit resides in the ability to manufacture the first components more economically at a lower tolerance of form by employing the layer of elastomer which is produced at precision tolerance through mold design to account for variation and permit easy assembly of the shaft assembly.
[0018] Yet another benefit is the ability to make changes to a design and tuning specifications without impacting a launch schedule of the product.
[0019] Still other benefits and advantages of the invention will become apparent to those skilled in the art upon reading and understanding the following detailed description. Brief Description of the Drawings
[0020] A more complete appreciation of the present invention and many of its advantages may be obtained by referring to the following detailed description in conjunction with the accompanying drawings.
[0021] Figure 1 is a cross-sectional view illustrating a conventional vibration isolator assembly or suspension bushing.
[0022] Figure 2 is an elevational view of an embodiment of the present invention.
[0023] Figure 3 is a cross-sectional view taken generally along the lines 3-3 of
Figure 2.
[0024] Figure 4 is a perspective view of a second component of the shaft assembly separated from the remainder of the vibration isolator assembly.
[0025] Figure 5 illustrates a separation of a first component of the shaft assembly along a split plane for receipt of the second component.
[0026] Figure 6 illustrates partial insertion of the second component into the remainder of the vibration isolator assembly.
[0027] Figure 7 is a perspective view of the final assembly.
[0028] Figure 8 is an elevational view of another embodiment of the present invention, namely, a cradle mount assembly.
[0029] Figure 9 is a cross-sectional view taken generally along the lines 9-9 of
Figure 8.
[0030] Figure 10 is an exploded perspective view of individual components of the assembly.
[0031] Figure 11 illustrates a further step in the assembly of the vibration isolator assembly or cradle mount.
[0032] Figure 12 shows enlarging the cavity of a first component of the shaft assembly.
[0033] Figure 13 illustrates partial insertion of the second component of the shaft assembly.
[0034] Figure 14 illustrates the completed assembly of the second embodiment.
[0035] Figure 15 is a perspective view of the completed assembly of individual components of a third embodiment. [0036] Figure 16 is a perspective view of another embodiment of the housing, isolator and first component of a shaft assembly.
[0037] Figure 17 is a perspective view of a second component of the shaft assembly of the third embodiment.
[0038] Figure 18 is a perspective view of a fourth embodiment of the housing, isolator and a first component of the shaft assembly.
[0039] Figure 19 is a perspective view of the first component of the shaft assembly.
[0040] Figure 20 is a perspective view of the second component of the shaft assembly.
Detailed Description of the Invention
[0041] By way of brief description, a conventional vibration isolator assembly
A is shown in Figure 1. The assembly includes a housing A and a shaft B that are interconnected by an isolator such as elastomer C. As noted above, the elastomer is typically mold bonded to the shaft and the housing and provides the vibration damping between the shaft secured to a first structure or component that moves relative to the housing which is secured to a second structure or component. [0042] A first embodiment of the present invention is shown in Figures 2-7.
Vibration isolator assembly 20 includes a housing 22. Typically, the housing is a metal structure, although as will be appreciated in accordance with the present invention, alternative materials including non-metallic materials such as nylon can be used to form the housing. As illustrated in Figures 2 and 3, when used as a mount bushing, the housing typically adopts a generally cylindrical conformation, i.e., circular in cross section. Secured to an inner surface 24 of the housing is an isolator 30. The isolator is often an elastomer or rubber construction because of the ability to isolate and reduce noise and vibration from being transmitted therethrough because of the elastic nature of the material. Rubber is generally an incompressible material that is displaced during loading and exhibits the desirable property that the more the rubber is compressed, the higher the stiffness. This rate build-up controls noise, vibration, and harshness associated with, for example, the vehicle environment. The elastomer is preferably mold bonded to the inner surface 24, although it will be appreciated that other bonding arrangements such as an adhesive bond, can be used without departing from the scope and intent of the present invention. Likewise, an inner diameter portion 34 of the isolator is secured to a shaft assembly 40, which is preferably comprised of first and second components 42, 44. The isolator is secured to a first or outer surface 46 of the first component and again is illustrated as being mold bonded thereto. As will become more apparent below, the first component 42 in this embodiment is defined by first and second portions 42a, 42b that are separated and have outer surfaces 46a, 46b that are bonded to the isolator, respectively. Inner, facing surfaces 48a, 48b of the first component are separated along a split plane and slidably engage the second component 44 of the shaft assembly. As perhaps best illustrated in Figure 2, and Figures 4-7, the first and second components 42, 44 of the shaft assembly have mating, keyed configurations that provide for slidable insertion of the second component into a cavity defined along the split plane between the first and second portions 42a, 42b of the first component, and likewise resist relative movement between the first and second components in other directions. This mating, keyed configuration provides an interlocking feature that allows the separate components (here, three separate pieces) to merge and function as a single component. For example, as illustrated in Figure 2, the first and second portions 42a, 42b of the first component have dovetailed keyways 60 formed on opposite axial sides of central axis 62. The keyways are dimensioned to receive mating, dovetailed keys or projections 64 that extend outwardly from the second component 44 of the shaft assembly. Thus, with continued reference to Figure 2, and additional reference to Figures 4 and 5, it is seen that the first component 42 includes first and second mirror-image portions 42a, 42b having a central rounded portion 66 that merges into generally planar, outer radial portions 68. The first and second portions 42a, 42b are separable or split along the plane 70 that passes through the longitudinal axis 62. The second component is similarly contoured, having a central rounded portion 76 that merges into generally planar, outer radial portions 78 disposed on diametrically opposite sides of the rounded portion. As will be appreciated, although this contour has met with success, still other variations or contours may be used without departing from the scope and intent of the present invention.
[0043] As represented in Figure 4, the mirror image portions 42a, 42b of the first component of the shaft assembly are integrally bonded to the isolator. The portions are separable along the facing, mating surfaces along split plane 70. Thus, as shown in Figure 4, the facing dovetailed key ways 60 define an outer radial cavity portion and the rounded portions 66a, 66b define a central cavity portion 80. When the portions 42a, 42b are disposed in abutting relation as shown in Figure 4, the cavities 80 defined by the keyways present a first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating contour of the second component. Thus, and as will be appreciated from a comparison of Figures 4 and 5, the first and second portions 42a, 42b of the first component of the shaft assembly are spread apart or separated along the split plane 70 to enlarge the cavity or opening 80 and allow selective sliding receipt of the second component 44 of the shaft assembly therein. This sliding receipt is represented in Figure 6, where the second component is partially received into the first component of the shaft assembly. Ultimately, complete insertion of the second component into the first component is achieved and is represented in Figure 7.
[0044] As noted in the Background discussion above, the isolator is typically an elastomer molded between the housing and shaft, here between the housing and the first component 42 of the shaft assembly. When it cures, the elastomer ends up with residual tensile stress. As noted, the prior art has addressed this in a different manner. Here, using a two-part shaft assembly alters the stress characteristics of the vibration isolator assembly. At a predetermined dimension of the second component 44, the residual tensile stress in the elastomer is removed upon complete insertion of the second component into the first component. If the second component is made even larger, then a predetermined compressive stress is formed in the isolator/elastomer. All of this is achieved without affecting or adversely impacting on the bond between the housing and elastomer, and likewise between the elastomer and shaft assembly.
[0045] By varying the thickness of the second component, variable compressive stresses can be introduced into the elastomer. This has two basic effects. The first effect is associated with spring rate. The compressive rate characteristics of the main elastomer elements will increase in magnitude, roughly in proportion to the degree of precompression, while the shear rate characteristics of the same elastomer elements will remain relatively unaffected. This results in a change in the compressive-to-shear rate ratio of the final assembly. [0046] The second effect deals with fatigue life. In general, an elastomer or rubber can tolerate increasing levels of compressive stress under cyclic loading much better than it tolerates smaller amounts of tensile stress. Thus, by introducing compressive stress via this method, fatigue life of the assembly can be enhanced. The forced separation of the molded split shaft assembly relieves the tensile stress resulting from part shrinkage, and imparts or introduces a desired compressive stress to the molded rubber, if desired.
[0047] It is also known in these isolation mount assemblies or bushing assemblies to incorporate one or more openings in the elastomer. Thus, as shown in Figures 2-7, the elastomer is radially continuous between the housing and the shaft assembly in one diametrical dimension (e.g., in the vertical direction as shown) and is discontinuous in another diametrical direction (e.g., in the horizontal direction as shown) through the inclusion of openings 90, 92. Here, the openings 90, 92 are generally symmetrical in the vertical and horizontal directions, but need not necessarily be symmetrical or similarly shaped. Likewise, boundary rubber 94, 96 (Figure 2) define snubbing rubber extending inwardly from the housing in the horizontal direction. By selectively altering the width dimension of the second component of the shaft assembly, i.e., by extending the planar portions 78 radially outward, the gap between the shaft assembly and the boundary rubber is selectively altered. As the shaft assembly width is increased, the amount of travel that the shaft assembly proceeds through before contacting the boundary rubber on the housing will decrease. This transfers loading and stress more rapidly from the main central rubber elements to the exterior boundary or snubbing elements, and effectively alters the spring rate build-up characteristics. This has the effect of providing additional tuning options and improved fatigue durability.
[0048] The present invention is also useful in other vibration isolator assemblies such as the cradle mount shown in Figures 8-14. Since much of the structure and function is substantially identical, reference numerals with a primed suffix refer to like components (e.g., housing is referred to by reference numeral 22"), and new numerals identify new components. The primary distinction relates to the frame 100 of the vehicle in which the housing 22' of the cradle mount assembly 20" is also molded to the first component portions 42a', 42b' of the shaft assembly. The subassembly, i.e., housing 22", is initially inserted into the frame 100, namely opening 102. Rather than encountering high insertion forces as is typical with conventional structures, smaller friction forces can be provided during insertion of the housing into the frame in accordance with the present invention. Thereafter, the first component portions of the shaft assembly are spread apart (Figure 12) to accommodate the second component 44'. The second component is slidably received therein (Figure 13), thus altering the stress characteristics of the isolator/elastomer, and also enhancing the abutting engagement force between the housing 22' and the frame 100.
[0049] The housing 22' is preferably metal, but is should be noted that other composite or hard materials may be used. Likewise, the outer dimension of the housing can relate to any shape such as rectangular, square, circular, triangular, or any other shape or surface depending on the size and requirements needed for the end use. Similarly, the shaft assembly is shown as being located at or near the center point of the housing, although that could be varied. Likewise, although it is preferred to extrude the shaft assembly components from aluminum, occasionally other materials, e.g., cast, extruded, powdered metal, forgings, cold headed steel, or still other materials of construction may be used without departing from the scope and intent of the invention. The number and/or shape of the openings can also be varied, and the elastomer isolator that is bonded to the housing components may be secured thereto with any other type of bonding.
[0050] Similar to the aforementioned embodiments, two additional embodiments are shown in Figures 15-20. Since most of the structure and function is substantially identical, reference numerals with a double primed suffix (") refer to like components (e.g., housing is referred to by reference numeral 22"), and new numerals identify new components in the additional embodiment of Figures 15-17. Likewise, reference numerals with a triple primed ("') suffix refer to like components (e.g., housing is identified by reference numeral 22'") in the still additional embodiment of Figures 18-20, and new numerals identify new components. The primary distinctions relate to the first component and second component of the shaft assembly. [0051] As shown in Figures 15-17, the first and second components 42", 44" of the shaft assembly have mating, keyed configurations that provide for slidable insertion of the second component into a cavity defined by the first component. This mating, keyed configuration provides an interlocking feature that allows the separate components to merge and function as a single component. Preferably, the first component has enlarged dove-tailed keyways 60" formed on opposite axial sides of the central longitudinal axis 62". The keyways are dimensioned to receive mating, dove-tailed keys or projections 64" that extend outwardly from the second component 44" of the shaft assembly. Thus, with continued reference to Figures 15- 17, it is seen that the first component 42" has a central, rounded (although no circular) portion 66" that merges into generally planar, outer portions 68". The second component is similarly contoured, having a central portion 76" that merges into generally planar, outer portions 78" disposed on diametrically opposite sides of the central portion.
[0052] The facing dovetailed key ways 60" define an outer cavity portion and the non-rounded portions 66" define a central cavity portion 80". The cavities present a first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating contour of the second component and allow selective sliding receipt of the second component 44" of the shaft assembly therein. Accordingly, as it relates to the first embodiment and specifically when compared with the enlarged dove-tailed projections 64" and keyways 60", this configuration reduces tolerance requirements for the dove-tail locking feature and simplifies assembly of the shaft assembly into the cavity portion. [0053] As shown in Figures 18-20 and as will become more apparent below, the first component 42'" in this embodiment is defined by first and second mirror portions 110a, 110b that are separated and have outer surfaces 114a, 114b that are bonded to the isolator 30'", respectively. Inner facing surfaces 116a, 116b of the first component are separated by the isolator and slidably engage the second component 44"" of the shaft assembly. The first and second components 42'", 44"' have mating configurations that provide for slidable insertion of the second component into a cavity 80'" defined between the first and second portions 110a, 110b of the first component and the isolator 30'", and likewise resist relative movement between the first and second components in other directions. This mating configuration provides an interlocking feature that allows the separate components to merge and function as a single component.
[0054] With reference to Figure 20, it is seen that the second component 44'" of the shaft assembly (sometimes referred to as the spreader component) has a general "I" or I-beam contour with keyed portions 118a, 118b extending from a central portion 119. The first and second portions 110a, 110b of the first component have curved end portions 120a, 120b (Figure 19) dimensioned to receive the "I" contour of the second component. The inner facing surfaces 116a, 116b of the first and second portions 110a, 110b of the first component 42"'have a thin layer or skin 122 of elastomer bonded thereto (Figure 18). The elastomer 122 bonded to the inner facing surfaces 116a, 116b of the first component permits the first component (sometimes referred to as a capture plate of half-shaft) to be manufactured more economically at a lower tolerance of form. The elastomer layer is produced at precision tolerances through mold design thereby taking up any variation in the dimensions of the first component and allowing consistent assembly of the first component and second component. As will be appreciated in accordance with the present embodiment, alternate materials can be used to form the elastomer layer or skin.
[0055] As represented in Figure 20, the first and second portions 110a, 110b of the first component of the shaft assembly are integrally bonded to and separated by the isolator and define a central cavity portion 80'". This cavity defines the first dimension of the first component of the shaft assembly that is smaller than a second dimension provided by the preselected, mating "I" contour of the second component. Thus, the first and second portions 110a, 110b of the first component 42'" allow sliding receipt of the second component 44'" of the shaft assembly therein. [0056] Again, it will be appreciated that the third and fourth embodiments of
Figures 15-20 use first and second components that are preferably extruded designs because of the ease of manufacture and assembly. The ability to use other shapes, designs, or contours that are not extruded or conducive to extruding should be recognized as being within the scope and intent of the present invention. [0057] In summary, the manipulation of spring rate magnitude, rate ratios, rate build-up, and component fatigue characteristics is accomplished using a common molded isolator or elastomer and interchangeable shaft assemblies of different designs. This is important since higher tooling costs and longer lead times are typically associated with the isolator/elastomer, while the inserted shaft can be modified quickly and economically. The economical aspect of the vibration isolator assembly means that more options can also be made available within the constraints of a development budget. This highlights yet another feature of the invention wherein the ability to make changes to design and tuning specifications later in the program can be achieved without impacting the launch schedule of the product. [0058] The invention has been described with reference to the different embodiments. Modifications and alterations will occur to others upon reading and understanding this specification. For example, various other manufacturing steps may be employed or in a different sequence. Likewise, different materials may be used or alternative processes without departing from the present invention. It is intended to include all such modifications and alterations in so far as they come within the scope of the appended claims or the equivalents thereof.

Claims

Having thus described the invention, it is now claimed:
1. A vibration isolator assembly comprising: a housing; an isolator connected to the housing for limiting the transmission of vibrations thereto; and a shaft assembly that is adapted for exposure to vibration forces, the shaft assembly including first and second mating components, the first component connected to the isolator and having a cavity of a first dimension for receiving the second component having a second dimension slightly greater than the first dimension for altering stress characteristics of the vibration isolator assembly.
2. The invention of claim 1 wherein the isolator is an elastomer.
3. The invention of claim 1 wherein the housing is metal.
4. The invention of claim 1 wherein the housing is a non-metallic material.
5. The invention of claim 4 wherein the housing is a nylon material.
6. The invention of claim 1 wherein the isolator is an elastomer that is molded to the housing and the first component of the shaft assembly.
7. The invention of claim 1 wherein the first component is contoured for slidable receipt of the second component of the shaft assembly.
8. The invention of claim 1 wherein the second dimension of the second component is preselected to relieve molded in tensile stress in the isolator.
9. The invention of claim 1 wherein the second dimension of the second component is preselected to impart compressive stress to the isolator.
10. The invention of claim 1 wherein the first component of the shaft assembly is a split member having first and second surfaces disposed in facing relation.
11. The invention of claim 10 wherein the second component is contoured for receipt in the cavity of the first component along the split, first and second surfaces of the first component.
12. The invention of claim 10 wherein the first and second components of the shaft assembly include keyed contours for limiting relative movement of the first and second components of the shaft assembly in directions other than a direction of the split between the first and second components.
13. The invention of claim 1 wherein the isolator includes at least one opening formed therein whereby the shaft assembly is spaced from the isolator by the at least one opening, and a dimension of the second component in the direction of the at least opening is preselected to selectively alter spring rate build-up characteristics in said direction.
14. The invention of claim 1 further comprising a thin layer of material interposed between the first and second components of the shaft assembly.
15. The invention of claim 14 wherein the thin layer of material is an elastomer provided on one of the first and second components of the shaft assembly.
16. The invention of claim 15 wherein the thin layer of elastomer is provided on the first component of the shaft assembly.
17. The invention of claim 16 wherein the thin layer of elastomer is provided on an inner surface of the first component.
18. A method of altering spring rate characteristics in a vibration isolator assembly having a housing, shaft, and isolator interconnecting the housing and shaft to limit transfer of vibration therebetween, the method comprising the steps of: forming a cavity in the shaft; and varying a dimension of the shaft to alter the spring rate characteristics of the vibration isolator assembly.
19. The method of claim 18 wherein the varying step includes the step of inserting a component of the shaft into the cavity.
20. The method of claim 18 wherein the varying step includes forming a shaft assembly from a split, first component and inserting a second component of the shaft assembly between split portions of the first component.
21. The method of claim 20 wherein the varying step includes dimensioning the second component to relieve tensile stress in the isolator.
22. The method of claim 20 wherein the varying step includes dimensioning the second component to impart a compressive stress in the isolator.
23. The method of claim 20 wherein the varying step includes enlarging a dimension of the shaft assembly without effecting a bond formed between the isolator and the housing, and between the isolator and shaft assembly.
24. The method of claim 20 comprising the first step of coating a surface of each split component with a material to form a close dimensional tolerance of the split components.
25. The method of claim 20 wherein the isolator has at least one opening therethrough, and the varying step further includes the step of varying a dimension of the shaft in a direction of the at least one opening in the isolator to alter spring rate characteristics thereof.
EP04754966A 2003-06-10 2004-06-10 A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same Withdrawn EP1631753A4 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/458,514 US7204479B2 (en) 2003-06-10 2003-06-10 Vibration isolator assembly having altered stress characteristics, and method of altering stress characteristics of same
US10/828,574 US7063310B2 (en) 2003-06-10 2004-04-21 Vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same
PCT/US2004/018540 WO2005001305A2 (en) 2003-06-10 2004-06-10 A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same

Publications (2)

Publication Number Publication Date
EP1631753A2 true EP1631753A2 (en) 2006-03-08
EP1631753A4 EP1631753A4 (en) 2007-05-30

Family

ID=33555087

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04754966A Withdrawn EP1631753A4 (en) 2003-06-10 2004-06-10 A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same

Country Status (7)

Country Link
EP (1) EP1631753A4 (en)
JP (1) JP2007500332A (en)
KR (1) KR20060036902A (en)
BR (1) BRPI0406220A (en)
CA (1) CA2520739A1 (en)
MX (1) MXPA05004532A (en)
WO (1) WO2005001305A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2381646T3 (en) 2006-10-10 2012-05-30 Trelleborg Automotive Germany Gmbh Procedure for calibrating an elastomer spring of a support
JP2010101385A (en) * 2008-10-22 2010-05-06 Molten Corp Bush
DE102017201903B4 (en) 2017-02-07 2019-06-19 Ford Global Technologies, Llc storage unit

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3881711A (en) * 1973-01-12 1975-05-06 Paulstra Sa Elastic supports
FR2333163A1 (en) * 1975-11-25 1977-06-24 Kleber Colombes Suspension spring for railway carriage bogie - has concentric rubber layers precompressed by bush before installation between rings
GB2010438A (en) * 1977-12-10 1979-06-27 Metzeler Kautschuk Prestressable Resilient Mounting
JPH02113137A (en) * 1988-10-21 1990-04-25 Bridgestone Corp Vibration-proof device
US5024425A (en) * 1989-02-24 1991-06-18 Firma Carl Freudenberg Elastomeric sleeve spring
EP0499996A1 (en) * 1991-02-19 1992-08-26 Bridgestone Corporation Vibration isolation apparatus
FR2739153A1 (en) * 1995-09-27 1997-03-28 Peugeot Elastic pivot joint for suspension of motor vehicle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0435009A (en) * 1990-05-31 1992-02-05 Taiyo Yuden Co Ltd Rectangular-shaped ferrite core
JPH04210134A (en) * 1990-11-30 1992-07-31 Bridgestone Corp Vibration isolating device
JPH04321823A (en) * 1991-04-17 1992-11-11 Toyoda Gosei Co Ltd Cylindrical vibration-isolating bush
JPH04337129A (en) * 1991-05-11 1992-11-25 Kurashiki Kako Co Ltd Bush assembly body
JP3193253B2 (en) * 1995-01-17 2001-07-30 東海ゴム工業株式会社 Fluid-filled anti-vibration bush
US5657510A (en) * 1995-06-14 1997-08-19 Yamashita Rubber Kabushiki Kaisha Fluid-filled insulating bushing
JPH11125290A (en) * 1997-10-22 1999-05-11 Tokai Rubber Ind Ltd Cylindrical vibration isolating device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3881711A (en) * 1973-01-12 1975-05-06 Paulstra Sa Elastic supports
FR2333163A1 (en) * 1975-11-25 1977-06-24 Kleber Colombes Suspension spring for railway carriage bogie - has concentric rubber layers precompressed by bush before installation between rings
GB2010438A (en) * 1977-12-10 1979-06-27 Metzeler Kautschuk Prestressable Resilient Mounting
JPH02113137A (en) * 1988-10-21 1990-04-25 Bridgestone Corp Vibration-proof device
US5024425A (en) * 1989-02-24 1991-06-18 Firma Carl Freudenberg Elastomeric sleeve spring
EP0499996A1 (en) * 1991-02-19 1992-08-26 Bridgestone Corporation Vibration isolation apparatus
FR2739153A1 (en) * 1995-09-27 1997-03-28 Peugeot Elastic pivot joint for suspension of motor vehicle

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2005001305A2 *

Also Published As

Publication number Publication date
JP2007500332A (en) 2007-01-11
CA2520739A1 (en) 2005-01-06
KR20060036902A (en) 2006-05-02
WO2005001305A2 (en) 2005-01-06
BRPI0406220A (en) 2005-08-09
WO2005001305A3 (en) 2005-05-26
EP1631753A4 (en) 2007-05-30
MXPA05004532A (en) 2005-11-23

Similar Documents

Publication Publication Date Title
US7063310B2 (en) Vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same
KR101730686B1 (en) Knuckle and bushing assembly
AU724888B2 (en) Composite elastomeric spring
CN101240827B (en) Cylindrical vibration isolating device
JP6190638B2 (en) Anti-vibration bush and method for manufacturing anti-vibration bush
US20050254888A1 (en) Torque rod and method of producing the same
JP2002295560A (en) Cylindrical rubber mount
JP2007105789A (en) Method for manufacturing supporting structure for vehicle
WO2010147213A1 (en) Vibration damping device
DE102014012748A1 (en) Piston structure for engine and piston pin
EP1138973A2 (en) Dynamic damper having generally cylindrical shape and method of producing the same
WO2005001305A2 (en) A vibration isolator assembly having altered stress characteristics and method of altering stress characteristics of same
JP2013204801A (en) Cylindrical antivibration device, and method for manufacturing the same
JP6257389B2 (en) Cylindrical vibration isolator and manufacturing method thereof
JP2007064301A (en) Rubber vibration isolator member
JP2008057792A (en) Cylindrical dynamic damper and its manufacturing process
JP4766372B2 (en) Pulley with damper and manufacturing method thereof
CN108412957B (en) Spacer pin and vibration damping device
JP4669329B2 (en) Dynamic damper
JP2001198645A (en) Manufacturing method for cam lobe used for assembly type cam shaft
JPS58132363A (en) Cylindrical spacer and its production
KR101673629B1 (en) Apparatus for engine mount of vehicle
JP6974989B2 (en) Manufacturing method of anti-vibration device
JP2009085305A (en) Cylindrical vibration isolator and its manufacturing method
JPH08152035A (en) Cylindrical mount and manufacture thereof

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20050427

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR

DAX Request for extension of the european patent (deleted)
RIN1 Information on inventor provided before grant (corrected)

Inventor name: PALADICHUCK, ROBERTCOOPER-STANDARD AUTOMOTIVE INC

Inventor name: RICE, BERNIE

Inventor name: POWER, DOUGLAS

A4 Supplementary search report drawn up and despatched

Effective date: 20070503

RIC1 Information provided on ipc code assigned before grant

Ipc: F16F 1/38 20060101AFI20070425BHEP

17Q First examination report despatched

Effective date: 20080305

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20080916