Asymmetric Gears: Parameter Selection Approach
p.70
p.70
Failures in the Development and Service of the Helicopter Transmission System
p.74
p.74
Modification Analysis of the New Axis-Fixed Cycloid Drive
p.82
p.82
Research on the Dynamic Response of a Combining Gear Drive System
p.86
p.86
Study on General Principle for Structure Fatigue Substantiation of Helicopter Transmission Systems
p.90
p.90
Thermal Effects Analysis on DCT Driven Plate in Vehicle Initial Condition
p.96
p.96
Simulation of Finite Element Analysis for Cutting Force of High-Speed Dry Gear Milling by Flying Cutter
p.100
p.100
Optimum Design of the 3Z-II Planet Drive Based on Matlab
p.104
p.104
The Influence Analysis of Fatigue Limit for Mechanical Components Based on Standard Deviation of Full Scale Sub-Sample
p.108
p.108
Study on General Principle for Structure Fatigue Substantiation of Helicopter Transmission Systems
Abstract:
On the base of reading up the latest overseas certification specifications and integrating the experience of engineering practice, the requirement for structure fatigue substantiation of helicopter transmission system was expounded, and the related key concepts were explained in detail. Furthermore, the general method for structure fatigue substantiation was presented. Thus, the frame of general principle for structure fatigue substantiation of helicopter transmission systems was basically founded.
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Info:
Periodical:
Applied Mechanics and Materials (Volume 86)
Pages:
90-95
Citation:
Online since:
August 2011
Authors:
Price:
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