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Structural optimization of uniaxial symmetry non-circular bolt clearance hole on turbine disk

  • Published:2014-10 Issue:5 Volume:27 Page:1142-1148
  • ISSN:1000-9361
  • Container-title:Chinese Journal of Aeronautics
  • language:en
  • Short-container-title:Chinese Journal of Aeronautics

Author:

Chen Qiuren,Guo Haiding,Zhang Chao,Liu Xiaogang

Funder

Aeronautical Science Foundation of China

Central Universities of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference20 articles.

1. Structure analysis and life evaluation of the pin holes in a turbine disk of a type of aero-engine;Li;J Aerosp Power,2009

2. New method for damage tolerance analysis of turbine disk and its application;Lu;J Aerosp Power,2002

3. Analysis on shear behavior of high-strength bolts connection;Shi;Int J Steel Struct,2011

4. Optimization of bolt thread stress concentrations;Pedersen;J Arch Appl Mech,2013

5. Reliability analysis of multi-axial low cycle fatigue life for turbine disk;Gao;Acta Aeronaut et Astronaut Sin,2009
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