1995
DOI: 10.1115/1.2826101
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Parametric Deflection Approximations for End-Loaded, Large-Deflection Beams in Compliant Mechanisms

Abstract: Geometric nonlinearities often complicate the analysis of systems containing large-deflection members. The time and resources required to develop closed-form or numerical solutions have inspired the development of a simple method of approximating the deflection path of end-loaded, large-deflection cantilever beams. The path coordinates are parameterized in a single parameter called the pseudo-rigid-body angle. The approximations are accurate to within 0.5 percent of the closed-form elliptic integral solutions.… Show more

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Cited by 299 publications
(110 citation statements)
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“…The compliance for torsional stiffness of link attached is represented by a torsional spring. The torsional spring constant K t for a cantilever beam with a force at the free end is given by [14].…”
Section: Bearing Stiffnessmentioning
confidence: 99%
“…The compliance for torsional stiffness of link attached is represented by a torsional spring. The torsional spring constant K t for a cantilever beam with a force at the free end is given by [14].…”
Section: Bearing Stiffnessmentioning
confidence: 99%
“…PSEUDO-RIGID-BODY MODEL APPLIED TO THE C-LEG. ADAPTED FROM [21] and [4] strength to withstand the demands of the intended environment which include stresses caused by changing payloads, speeds, irregular landings and collisions. Many composites, including the fiberglass composite chosen, are anisotropic and thus have properties that change depending on the orientation along which the property is measured [20].…”
Section: Materials Selectionmentioning
confidence: 99%
“…In the absence of the tip moment, this incremental approach is applied only for orthogonal inclination loading angle where the elastica of the beam does exceed the vertical axis. Similar procedure applying Jacobi elliptic integrals of first and second types by considering only end-load is used by Howell and Midha (Howell & Midha, 1995). Saxena and Kramer proposed a numerical integration scheme that requires special consideration for the occurrence of any inflection point within the beam for combined end loading (Saxena & Kramer, 1998).…”
Section: Introductionmentioning
confidence: 99%