Structural Characteristics of Rotate Vector Reducer Free Vibration

For RV reducer widely used in robots, vibration significantly affects its performance. A lumped parameter model is developed to investigate free vibration characteristics without and with gyroscopic effects. The dynamic model considers key factors affecting vibration such as involute and cycloid gea...

Full description

Bibliographic Details
Main Authors: Chuan Chen, Yuhu Yang
Format: Article
Language:English
Published: Hindawi Limited 2017-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2017/4214370
id doaj-d7774c9920394739a03749f2bd745356
record_format Article
spelling doaj-d7774c9920394739a03749f2bd7453562020-11-24T23:57:31ZengHindawi LimitedShock and Vibration1070-96221875-92032017-01-01201710.1155/2017/42143704214370Structural Characteristics of Rotate Vector Reducer Free VibrationChuan Chen0Yuhu Yang1School of Mechanical Engineering, Tianjin University, Tianjin 300072, ChinaSchool of Mechanical Engineering, Tianjin University, Tianjin 300072, ChinaFor RV reducer widely used in robots, vibration significantly affects its performance. A lumped parameter model is developed to investigate free vibration characteristics without and with gyroscopic effects. The dynamic model considers key factors affecting vibration such as involute and cycloid gear mesh stiffness, crankshaft bending stiffness, and bearing stiffness. For both nongyroscopic and gyroscopic systems, free vibrations are examined and compared with each other. Results reveal the specific structure of vibration modes for both systems, which results from symmetry structure of RV reducer. According to vibration of the central components, vibration modes of two systems can be classified into three types, rotational, translational, and planetary component modes. Different from nongyroscopic system, the eigenvalues with gyroscopic effects are complex-valued and speed-dependent. The eigenvalue for a range of carrier speeds is obtained by numerical simulation. Divergence and flutter instability is observed at speeds adjacent to critical speeds. Furthermore, the work studies effects of key factors, which include crankshaft eccentricity and the number of pins, on eigenvalues. Finally, experiment is performed to verify the effectiveness of the dynamic model. The research of this paper is helpful for the analysis on free vibration and dynamic design of RV reducer.http://dx.doi.org/10.1155/2017/4214370
collection DOAJ
language English
format Article
sources DOAJ
author Chuan Chen
Yuhu Yang
spellingShingle Chuan Chen
Yuhu Yang
Structural Characteristics of Rotate Vector Reducer Free Vibration
Shock and Vibration
author_facet Chuan Chen
Yuhu Yang
author_sort Chuan Chen
title Structural Characteristics of Rotate Vector Reducer Free Vibration
title_short Structural Characteristics of Rotate Vector Reducer Free Vibration
title_full Structural Characteristics of Rotate Vector Reducer Free Vibration
title_fullStr Structural Characteristics of Rotate Vector Reducer Free Vibration
title_full_unstemmed Structural Characteristics of Rotate Vector Reducer Free Vibration
title_sort structural characteristics of rotate vector reducer free vibration
publisher Hindawi Limited
series Shock and Vibration
issn 1070-9622
1875-9203
publishDate 2017-01-01
description For RV reducer widely used in robots, vibration significantly affects its performance. A lumped parameter model is developed to investigate free vibration characteristics without and with gyroscopic effects. The dynamic model considers key factors affecting vibration such as involute and cycloid gear mesh stiffness, crankshaft bending stiffness, and bearing stiffness. For both nongyroscopic and gyroscopic systems, free vibrations are examined and compared with each other. Results reveal the specific structure of vibration modes for both systems, which results from symmetry structure of RV reducer. According to vibration of the central components, vibration modes of two systems can be classified into three types, rotational, translational, and planetary component modes. Different from nongyroscopic system, the eigenvalues with gyroscopic effects are complex-valued and speed-dependent. The eigenvalue for a range of carrier speeds is obtained by numerical simulation. Divergence and flutter instability is observed at speeds adjacent to critical speeds. Furthermore, the work studies effects of key factors, which include crankshaft eccentricity and the number of pins, on eigenvalues. Finally, experiment is performed to verify the effectiveness of the dynamic model. The research of this paper is helpful for the analysis on free vibration and dynamic design of RV reducer.
url http://dx.doi.org/10.1155/2017/4214370
work_keys_str_mv AT chuanchen structuralcharacteristicsofrotatevectorreducerfreevibration
AT yuhuyang structuralcharacteristicsofrotatevectorreducerfreevibration
_version_ 1725453534950850560