scholarly journals Analysis of the algorithm for determining the meshing forces in a spline coupling with misalignment

2021 ◽  
Vol 1129 (1) ◽  
pp. 012026
Author(s):  
I V Nikolaev ◽  
M K Leontiev
Keyword(s):  
Wear ◽  
2007 ◽  
Vol 262 (9-10) ◽  
pp. 1205-1216 ◽  
Author(s):  
J. Ding ◽  
I.R. McColl ◽  
S.B. Leen

Author(s):  
A Barrot ◽  
M Paredes ◽  
M Sartor

In this paper, an analytical method is used to investigate the distortions of involute spline teeth. The following hypotheses are adopted: teeth geometry is in conformity with standardization, dimensions are nominal (no defect), there is no friction and the load is a pure torsional torque. Teeth distortions due to bending, shear, compression, and foundation rotation are analysed. As the load is distributed along the tooth height, the displacement calculation differs from the conventional approach used for gear teeth. Sliding over the contact surfaces is also considered as it emerged during the study that this phenomenon, that has not hitherto been taken into account, plays a significant role. A punch model is used to describe the radial distribution of the contact pressure. Ascribing an arbitrary value to the tilted angle between the two contacting flanks enables the pressure profile to be evaluated, from which calculation of teeth distortions can be arrived at so as finally to obtain a new estimation of the tilted angle. Thus, displacements and the contact load can be determined together by iterating the calculation procedure until convergence. Torsional stiffness, which is one of the main parameters required to predict the torque distribution along the spline coupling, is evaluated from the various displacement components. The results derived from the proposed analytical method are compared with finite-element results and show good correlation.


Author(s):  
S B Leen ◽  
I R McColl ◽  
C H H Ratsimba ◽  
E J Williams

Aeroengine spline couplings experience a wide range of loading conditions leading to contrasting service life limiting phenomena, including fatigue, fretting fatigue and fretting wear. Highly loaded couplings may employ incomplete contact axial profiles, while the contact geometry transverse to the spline axis is nominally complete with theoretical stress singularities at the contact edges. Life assessment of such components is consequently complex. The effect of torque overload conditions on the fatigue life of a barrelled, aeroengine type spline coupling is investigated experimentally. The experimental results are interpreted using three-dimensional finite element analyses, incorporating frictional contact and elastic-plastic material behaviour and the results of simple tension-tension fatigue tests. Torque-life and finite element predicted stress-life relationships are generated for spline life prediction purposes. Good correlation is obtained between the spline coupling and simple tension-tension fatigue test results, interpreted via the finite element predicted stress ranges.


2014 ◽  
Vol 74 ◽  
pp. 135-142 ◽  
Author(s):  
Vincenzo Cuffaro ◽  
Francesca Curà ◽  
Andrea Mura

Author(s):  
Giulio Barbato ◽  
Vincenzo Cuffaro ◽  
Francesca Curà ◽  
Gianfranco Genta ◽  
Andrea Mura

Spline couplings are mechanical elements used to transmit power by joining two coaxial rotating shafts. The main damaging phenomenon on these elements is fretting wear, which can occur on teeth surfaces when there is a relative movement. Therefore, specific design criteria to evaluate teeth damage of spline couplings subjected to fretting wear are needed. In this work, the criterion proposed by Ruiz is considered and criticalities of the first Ruiz parameter are analysed by performing an uncertainty evaluation. The specific working misaligned conditions of a dedicated test rig were considered in this analysis. An uncertainty table allows the comparison of main geometrical and mechanical factors, evidencing their relevant effects. It shows the need of a deeper analysis on the coefficient of friction between the contact surfaces of spline couplings working in misaligned conditions.


2017 ◽  
Vol 2017 ◽  
pp. 1-11 ◽  
Author(s):  
Xiangzhen Xue ◽  
Sanmin Wang ◽  
Jie Yu ◽  
Liyun Qin

In order to reduce wear and design high-performance spline coupling, the friction coefficient, wear coefficient, and wear depth of 14 groups of material specimens were tested using multifunctional friction and wear tester. The effect of materials, loads, rotation speed, and surface treatment on friction coefficient, wear coefficient, and wear depth was investigated. A method using an Archard’s equation based on the finite element method to calculate the wear depth of 14 groups of material specimens was proposed, and the results were consistent with the experimental results. Then, the wear of a floating involute spline coupling of aero-engine was predicted using this method. It can be concluded that carburizing and silvering can decrease the friction coefficient. The wear and wear coefficient decreased after carburizing. So, it is necessary to take 18CrNi4A with carburization and 32Cr3MoVA with nitridation as the material of the spline coupling in aero-engine to minimize wear. Furthermore, the method presented to predicate the wear of spline coupling in this work provided a good fundament for the fatigue prediction methodology of spline coupling.


2009 ◽  
Vol 16 (1) ◽  
pp. 200-211 ◽  
Author(s):  
Adrien Barrot ◽  
Manuel Paredes ◽  
Marc Sartor

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