Patent Application
20150048235
This disclosure relates to a dampening mechanism for coaxially aligned relatively translatable components. More particularly, it relates to such a mechanism comprising a resilient monolithic member interposed between the relatively translatable components that provides dampening through elastic tensile deformation.
Telescoping components are employed in a variety of applications. One important example is found in personal support devices such as crutches, canes, ski poles, trekking poles, and the like. Many forms of such personal support devices include a resilient connection between coaxially aligned, connected tubular support shafts to cushion impact loading. Known forms of these devices employ a compression coil spring between the coaxial, relatively movable shaft segments that compresses on application of load to absorb shock and cushion the impact associated with use. Such springs are susceptible to buckling or other undesired characteristics associated with deformation, which, over time, deteriorate the spring function and overall utility of the device.
The present disclosure is directed to an arrangement for a reciprocal connection between coaxial components of a support structure comprising an elastomeric element that absorbs load and develops a restoring force through tensile elongation.
The resilient element of the present disclosure is a molded member interposed between the relatively slidable ends of coaxially aligned telescoping support components. It provides resilient restoring force to the components through extension of the element in tension. It also provides a sleeve-like journal between the telescoping components to reduce frictional resistance and maintain coaxial alignment.
The dampening mechanism of the present disclosure is depicted in
The dampening mechanism comprises a pair of coaxially aligned, telescoping components and an interposed resilient elastomeric member 50. The telescoping components comprise an outer component 102 and an inner component 104 illustrated here as telescoping cylindrical shafts.
It should be appreciated that though the illustrated embodiment discloses cylindrical shafts, the dampening mechanism is suitable for use in any configuration where relatively reciprocating telescoping components are employed. These components may have any desired cross-section, such as oval, square, rectangular or other geometric shape. Moreover, though the outer component 102 must be hollow to receive the inner component 104 in telescoping relation, the components need not have the same cross section. For example, the inner component may be square, or “T” shaped or other suitable cross section.
Resilient elastomeric member 50 is intended to be interposed between two coaxially aligned relatively translatable components, intended for use in a generally vertical orientation. As illustrated in
Referring to
Referring to
As used herein the term axial means along the longitudinal axis of the shafts. Forward means in the direction of insertion of inner shaft element 104 into telescoping relation with outer shaft element 102. Rearward means in the opposite direction. The term radial means in a direction perpendicular to the longitudinal axis along which the telescoping elements are axially translatable. The terms radially inner or inward mean toward the longitudinal axis and radially outer or outward means in the opposite direction. As here illustrated, outer shaft element 102 is below and coaxial with inner shaft element 104. However, this configuration could be reversed with the inner shaft element 104 positioned below the outer shaft element 102.
As seen in
Shaft 104 includes a pair of engagement pins 110 spaced from the end 105. As seen in
The shaft elements 102 and 104 are assembled together to form the shaft assembly by insertion of end 105 of inner shaft 104 into end 103 of outer shaft 102. The spring loaded pins 110 are pushed radially into shaft element 104 to pass into end 103 of shaft element 102. Pins 110 engage within slots 106 and spring radially outward into the slots to connect the shafts 102 and 104 in a coaxial relation with axial translation permitted between the limits defined by the upper and lower terminus 107 and 109 of slots 106.
The resilient elastomeric member 50 of the assembly is shown in
Elastic energy absorbing resilient member 50 is molded from a polymeric material that provides the qualities of energy absorption on elongation and resiliency sufficient to restore it to its original shape after initial elongation. The element is designed via a proprietary ITW (Dahti) process that orients the crystalline structure of the device which increases tensile strength and adds the elasticity required to absorb energy. It is made available by ITW-Nexus, Des Plaines, IL.
The resilient member 50 may be molded from a variety of materials depending on the requirements of a specific application. It may, for example, be molded from a TPE (Thermoplastic Elastomer) material such as a COPE (Copolyester) material or a TPU (Thermoplastic Urethane) material. Suitable materials are available from Du Pont under the Hytrel® trademark or other commercially competitive materials.
After molding, the resilient member 50 is processed by elongation of portions of the structure beyond the yield point to align the crystalline lamellae in one direction. Such processing may proceed as disclosed in U.S. Patent Publication 2012/0153536, published Jun. 21, 2012, and entitled “Pre-deformed Thermoplastic Spring and Method of Manufacture,” the entire specification and drawings of which are hereby incorporated by reference herein as if fully set forth.
Referring to
Best seen in
Referring to
External surface 60 of support portion 56 is somewhat conical or curvilinear and defines a tapered centering node. It provides a forward guide surface to facilitate insertion of resilient elastomeric member 50 into the end of hollow tubular shaft component 102.
Cylindrical body portion 56 and webs 58 of resilient elastomeric member 50 are disposed between the inner surface of the end 103 of outer shaft element 102 and the outer surface of end 105 of inner shaft element 104. Pins 110 extend through aligned voids 59 into slots 106. Note that the spaced elongate webs 58 define voids 59 which can be aligned with slots 106 in outer shaft 102 to permit disposition of pins 110 within slots 106.
In
On loading of shaft elements 102 and 104, inner shaft element 104 is urged further into outer shaft element 102, causing elongation of resilient elastomeric member 50. Such elongation continues until pins 110 reach the limit of travel within slots 106 and engage lower terminus 109 of slots 106. Such movement and resultant elongation of resilient elastomeric member 50 cushion the impact of the applied load and, through tensioning elongation, develop a restoring force within resilient elastomeric member 50. On removal of the applied load, the restoring force urges the inner shaft 104 to return to its original position with pins 110 at upper terminus 107 of slots 106.
Notably, the cylindrical body 52 and webs 58 of resilient elastomeric member 50 are disposed between the relatively translatable shafts 102 and 104 and provide a journaling effect to reduce friction between the relatively translatable shafts and maintain coaxial alignment.
The number of webs 58 may be varied to alter the resilient and damping properties of the mechanism to correlate with the expected impact loading experienced during use of the coaxially aligned, translatable shafts. The properties of the dampening mechanism can, therefore, be tuned to the particular application involved. Because the damping mechanism is elastomeric, it is not susceptible to deterioration due to exposure to moisture or other environmental conditions.
Variations and modifications of the foregoing are within the scope of the present invention. It is understood that the invention disclosed and defined herein extends to all alternative combinations of two or more of the individual features mentioned or evident from the text and/or drawings. All of these different combinations constitute various alternative aspects of the present invention. The claims are to be construed to include alternative embodiments to the extent permitted by the prior art.
This application claims priority pursuant to Title 35 USC §119(e) to U.S. Provisional Application No. 61/616,725, filed Mar. 28, 2012 entitled “Dampening Mechanism for Coaxially Aligned Relatively Translatable Shafts”, the entire specification and drawings of which are hereby incorporated by reference herein as if fully set forth herein.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2013/033805 | 3/26/2013 | WO | 00 |
| Number | Date | Country | |
|---|---|---|---|
| 61616725 | Mar 2012 | US |
