Analysis on natural characteristics of four-stage main transmission system in three-engine helicopter
Analysis on natural characteristics of four-stage main transmission system in three-engine helicopter
The vibration model of four-stage main transmission system in helicopter was established through lumped mass method. In the model, many factors, including time-varying meshing stiffness and torsional stiffness of gear shaft were considered. The differential equation of the system was solved via Fourier method, and the influence of the torsional stiffness of shafts on the first five orders of the system’s natural frequency was studied. Some theoretical results were summarized as guidelines for further research and design of four-stage deceleration helicopter at last.
helicopter transmission system, four-stage reducer, natural characteristics, torsional stiffness, nonlinear dynamics
19
Chen, Yuan
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Zhu, Ru-peng
cab2bd69-3e29-4459-a1ed-e8c5e5876d36
Xiong, Yeping
51be8714-186e-4d2f-8e03-f44c428a4a49
Jin, Guang-hu
71a612f4-09c0-40a4-80d4-6616f1fc8610
29 June 2017
Chen, Yuan
05bcc581-b03f-44a8-b0e0-f27f889ec994
Zhu, Ru-peng
cab2bd69-3e29-4459-a1ed-e8c5e5876d36
Xiong, Yeping
51be8714-186e-4d2f-8e03-f44c428a4a49
Jin, Guang-hu
71a612f4-09c0-40a4-80d4-6616f1fc8610
Chen, Yuan, Zhu, Ru-peng, Xiong, Yeping and Jin, Guang-hu
(2017)
Analysis on natural characteristics of four-stage main transmission system in three-engine helicopter.
In Vibroengineering PROCEDIA.
.
(doi:10.21595/vp.2017.18558).
Record type:
Conference or Workshop Item
(Paper)
Abstract
The vibration model of four-stage main transmission system in helicopter was established through lumped mass method. In the model, many factors, including time-varying meshing stiffness and torsional stiffness of gear shaft were considered. The differential equation of the system was solved via Fourier method, and the influence of the torsional stiffness of shafts on the first five orders of the system’s natural frequency was studied. Some theoretical results were summarized as guidelines for further research and design of four-stage deceleration helicopter at last.
Text
Vibroengineering Procedia_final manucsript
- Accepted Manuscript
More information
Accepted/In Press date: 29 April 2017
Published date: 29 June 2017
Venue - Dates:
International Conference on VIBROENGINEERING: Theme: Nonlinear Dynamics and Chaos in Engineering Applications, Saint Petersburg Electrotechnical University, St. Petersburg, Russian Federation, 2017-06-29 - 2017-06-30
Keywords:
helicopter transmission system, four-stage reducer, natural characteristics, torsional stiffness, nonlinear dynamics
Identifiers
Local EPrints ID: 413507
URI: http://eprints.soton.ac.uk/id/eprint/413507
ISSN: 2345-0533
PURE UUID: e8c230b3-b069-45ed-b8c4-f1c10841be2e
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Date deposited: 25 Aug 2017 16:31
Last modified: 16 Mar 2024 03:17
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Contributors
Author:
Yuan Chen
Author:
Ru-peng Zhu
Author:
Guang-hu Jin
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