introduction to designing elastomeric vibration isolators.pptx

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    Introduction

    Why elastomers?

    Key design parameters

    Loading

    Configuration

    Spring rates

    Design considerations

    Steps to designing a simple isolator

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    Elastomers

    An eastomer is any elastic polymer

    Silicone Rubber

    Butyl Rubber

    Fluorosilicone Rubber

    Material selection dependent on application

    Ulitimate Loading

    Sensitivity to Environment

    Internal Properties

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    Elastomeric Isolators

    Engineered properties can meet specificapplications

    Modulus of elasticity

    Internal dampening

    Homogeneous nature allows for compactforms

    Easily manufactured Molded

    Formed in place

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    Key Isolator Design Parameters

    Configuration

    Loading

    Spring rate

    Shear, Bulk, and Youngs modulus

    Geometry

    Ultimate strength

    Internal dampening

    Maximum displacement

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    Simple Isolator Configurations

    Planer Sandwich Form

    Laminate

    Cylindrical

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    Spring Rates

    Isolator spring rate sets system resonantfrequency

    Ratio of resonant frequency to input frequency

    plus dampening control amount of isolation For an elastomer, spring rate is determined by

    Shape factor

    Loading: shear, compression, tension

    Material Properties: bulk, shear, and youngsmodulus

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    Transmissibility

    0.1

    1

    10

    0 0.5 1 1.5 2 2.5 3

    Transmissibility

    fr/f

    Transmissibility vs. Frequency Ratio

    = 0.01

    = 0.05

    = 0.1

    = 0.5

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    Shape Factor

    Ratio of load area to bulge area

    Easy to calculate for simple shapes simply loaded

    Planer sandwich forms are simple

    Tube form bearings are more difficult, but can beapproximated as a planer form

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    Shear Spring Rate

    Design isolator to attenuate in shear if possible

    Dependent on load area, thickness, and shearmodulus

    Shear modulus is linear up to 75%-100% strain

    Shear modulus for large shape factors is alsoeffected by high compressive loads

    When aspect ratio exceeds 0.25 a correctionfactor is added to account for bending

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    Compression Spring Rate

    Designed properly, compression canprovide high stiffness

    Depends on load area, effectivecompression modulus, and thickness

    Effective compression modulus Linear up to 30% strain

    Can be tricky to compute

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    Finding Modulus

    Many elastomers are listed with only with Durometer Shore hardness

    Ultimate strength (MPa or psi)

    Contacting manufacturer may be useful

    Perform tests Shear stress is 1/3 Youngs modulus as poissonsratio

    approaches 0.5

    Use Gents relation between Shore A hardness and Youngsmodulus (if you gotta have it now)

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    Computing Ec

    Gent provides a reference graph

    Hatheway found empirically that the

    transition zone is (Ec

    /E)(t/D)1.583=0.3660

    Can calculate Ecor the simple case of a circular

    load area of diameter D and thickness t

    Find the break points

    First break point: (t/D)1.583= 0.366(E/EB)

    Second break point: (t/D)1.583= 0.366

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    Compression Modulus vs. Shape

    Factor [Gent]

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    Laminate Isolator

    Shear modulus is not effected byshape factor (if aspect ratio is

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    Design Considerations

    What is being Isolated?

    What are the inputs?

    Are there static loads? What are the environmental conditions?

    What is the allowable system response?

    What is the service life?

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    Example Design Process for a Simple

    Isolator

    Single excitation frequency

    Circular cross section, planar geometery

    All other components infinitely rigid Low dampening

    Attenuation provided in shear

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    Design Process

    Specifications

    Mass, input vibration, required attenuation, max

    displacement

    Use transmissibility to determine resonance

    frequency and spring rate

    Find isolator minimum area (A)

    Total number of isolators and max allowable stress

    Select modulus (G)

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    Design Process (cont)

    Knowing area (A), modulus (G), and springrate (ks), calculate thickness (t)

    Calculate radius, verify aspect ratio < 0.25 to avoid

    bending effect Find static deflection

    Is static plus dynamic deflection < max allowabledeflection?

    Find static shear strain

    Low strain reduces fatigue (

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    Conclusion

    Careful selection of parameters necessary to usemethods presented. Can get complicated quick Low strains

    Low loads

    Try to stay clear of the transition zone betweenYoungs and the bulk modulus

    For multiple input frequencies, need to considerif dampening () is necessary

    May need to include considerations other thanjust isolation Stresses due to CTE mismatch

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    References

    P. M. Sheridan, F. O. James, and T. S. Miller, Design ofcomponents, in Engineering with Rubber (A. N. Gent,ed.), pp. 209{Munich:Hanser, 1992)

    A. E. Hatheway, Designing Elastomeric MirrorMountings,Proc. of SPIE Vol. 6665 (2007)

    Daniel Vukobratovich and Suzanne M. VukobratovichIntroduction to Optomechanical design

    A. N. Gent, On The Relation Between IndentationHardness and Youngs Modulus, IRI Trans. Vol. 34,pg.46-57 (1958)

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    Questions?