From: Nonlinear Vibration of Gears With Tooth Surface Modifications

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From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Dimensional gear mesh stiffness at 50 Nm (dashed-dotted line), 150 Nm (dashed line), and 250 Nm (solid line) using finite element analysis. (a) Unmodified spur gear pair from [36] (ICR = 1.37). (b) Modified spur gear pair from [5] (tip relief starts at 22.2 deg).

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Dimensional mean-removed excitation levels from the gears in Fig. 1 at 50 Nm (dashed-dotted line), 150 Nm (dashed line), and 250 Nm (solid line) using finite element analysis. (a) Unmodified spur gear pair. (b) Modified spur gear pair.

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: The first harmonic of nondimensional excitation from the unmodified and modified gears with varying applied torque. The gears are the same as in Fig. 1.

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Dynamic response of equation of motion (Eqs. (11)–(12)) using second order perturbation and numerical integration. Parameters are: α0,1 = 2/75, α0,0 = 2/3, α2,0 = 1/4, α3,0 = -1/24, e1 = 0.1, ψ1 = 0, α2,1 = 0, μ = 0.0082. Important regions of solutions are marked with (1) through (4). (Stable perturbation solution: solid line, unstable perturbation solution: dashed line, numerical integration: circles, linear solution: dashed-dotted line.)

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Force-deflection function f(x,t) of a helical gear pair obtained by the method of Ref. [9]. Tooth surface modifications are: quadratic profile tip and root crown of 10μm and lead crown of 10μm on the gear.

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Primary resonance of a helical gear pair at 200 Nm using second order perturbation, numerical integration, and the linearized model. The numerical integration results are obtained using the method of Ref. [9] (stable perturbation solution: solid line, computational data by numerical integration: circles, linear solution: dashed-dotted line).

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Perturbation solution when α2,0, α3,0, α2,1, and φ2,1 are set to zero one at a time are shown. The nonzero parameters are the same as in Fig. 6. The circles denote numerical integration with no nonzero parameters.

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Force-deflection function f(x,t) obtained by finite element analysis of a spur gear pair with increasing applied torque. Gear data from Ref. [5], linear tip relief of 10μm starts at 20.9 deg.

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Primary resonance of a spur gear pair (tip relief start at 20.9 deg) at 85 Nm using second order perturbation and linearized model. Experimental data are from Fig. 3(c) of Ref. [5] (stable second order perturbation: solid line, unstable second order perturbation solution: dashed line, experimental measurement: circles, linear solution: dashed-dotted line).

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Primary resonance of a spur gear pair (tip relief start at 20.9 deg) at 170 Nm using second order perturbation and linearized model. Experimental data are from Fig. 3(b) of Ref. [5] (stable second order perturbation: solid line, unstable second order perturbation solution: dashed line, experimental measurement: circles, linear solution: dashed-dotted line).

From: Nonlinear Vibration of Gears With Tooth Surface Modifications Date of download: 10/7/2017 Copyright © ASME. All rights reserved. From: Nonlinear Vibration of Gears With Tooth Surface Modifications J. Vib. Acoust. 2013;135(5):051005-051005-11. doi:10.1115/1.4023913 Figure Legend: Primary resonance of a spur gear pair (tip relief start at 23.6 deg) at 170 Nm using second order perturbation and linearized model. Experimental data are from Fig. 3(b) of Ref. [5] (stable perturbation solution: solid line, unstable perturbation solution: dashed line, experimental measurement: circles, linear solution: dashed-dotted line).