Torsion dynamics of aviation micro cylinder sine oscillating tooth system

Xiang Yang Jin; Guang Bin Yu; Xiang Yi Guan

Torsion dynamics of aviation micro cylinder sine oscillating tooth system

Xiang Yang Jin^*
, Guang Bin Yu
, Xiang Yi Guan

^*Corresponding author for this work

School of Mechatronics Engineering

Harbin University of Commerce
Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

3 Scopus citations

Abstract

The mathematic model of torsion of aviation micro cylinder sine oscillating tooth reducer system was built with Lagrange equation. Dynamical characteristic parameters of natural frequency, principal shape, module admittance and potential distribution was obtained. In order to improve the structure and to give more theory support of dynamical characteristics, the weakness part was pointed out, which will affect the dynamical characteristics.

Original language	English
Pages (from-to)	299-303
Number of pages	5
Journal	Zhongbei Daxue Xuebao (Ziran Kexue Ban)/Journal of North University of China (Natural Science Edition)
Volume	28
Issue number	4
State	Published - Aug 2007

Keywords

Dynamical characteristics
Reducer
Sine oscillating tooth

Cite this

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title = "Torsion dynamics of aviation micro cylinder sine oscillating tooth system",

abstract = "The mathematic model of torsion of aviation micro cylinder sine oscillating tooth reducer system was built with Lagrange equation. Dynamical characteristic parameters of natural frequency, principal shape, module admittance and potential distribution was obtained. In order to improve the structure and to give more theory support of dynamical characteristics, the weakness part was pointed out, which will affect the dynamical characteristics.",

keywords = "Dynamical characteristics, Reducer, Sine oscillating tooth",

author = "Jin, \{Xiang Yang\} and Yu, \{Guang Bin\} and Guan, \{Xiang Yi\}",

year = "2007",

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language = "英语",

volume = "28",

pages = "299--303",

journal = "Zhongbei Daxue Xuebao (Ziran Kexue Ban)/Journal of North University of China (Natural Science Edition)",

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publisher = "North China Institute of Technology",

number = "4",

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T1 - Torsion dynamics of aviation micro cylinder sine oscillating tooth system

AU - Jin, Xiang Yang

AU - Yu, Guang Bin

AU - Guan, Xiang Yi

PY - 2007/8

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N2 - The mathematic model of torsion of aviation micro cylinder sine oscillating tooth reducer system was built with Lagrange equation. Dynamical characteristic parameters of natural frequency, principal shape, module admittance and potential distribution was obtained. In order to improve the structure and to give more theory support of dynamical characteristics, the weakness part was pointed out, which will affect the dynamical characteristics.

AB - The mathematic model of torsion of aviation micro cylinder sine oscillating tooth reducer system was built with Lagrange equation. Dynamical characteristic parameters of natural frequency, principal shape, module admittance and potential distribution was obtained. In order to improve the structure and to give more theory support of dynamical characteristics, the weakness part was pointed out, which will affect the dynamical characteristics.

KW - Dynamical characteristics

KW - Reducer

KW - Sine oscillating tooth

UR - https://www.scopus.com/pages/publications/34648831979

M3 - 文章

AN - SCOPUS:34648831979

SN - 1673-3193

VL - 28

SP - 299

EP - 303

JO - Zhongbei Daxue Xuebao (Ziran Kexue Ban)/Journal of North University of China (Natural Science Edition)

JF - Zhongbei Daxue Xuebao (Ziran Kexue Ban)/Journal of North University of China (Natural Science Edition)

IS - 4

ER -

Torsion dynamics of aviation micro cylinder sine oscillating tooth system

Abstract

Keywords

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