Failure risk control for aeroengine turbine disks based on active thermal management

Author:

Wang Ziyao,Ding Shuiting,Li Guo

Funder

Academic Excellence Foundation of BUAA

Co-Innovation Center for Advanced Aeroengine of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference31 articles.

1. US Department of Transportation Federal Aviation Administration, Advisory Circular 33.75-1A: Guidance Material for 14 CFR 33.75 Safety Analysis, Washington DC, US, FA A, 2007.

2. US Department of Transportation Federal Aviation Administration, Advisory Circular 33.70-1: Guidance Material for Aircraft Engine-life-limited Parts Requirements, Washington DC, US, FAA, 2009.

3. Probabilistic analysis of aircraft gas turbine disk life and reliability;Melis;J. Propul. Power,1999

4. G.R. Leverant, D.L. Littlefield, R.C. McClung, H.R. Millwater, J.Y. Wu, A probabilistic approach to aircraft turbine rotor material design, ASME Paper, 1997-GT-22, 1997.

5. M.P. Enright, R.C. McClung, L. Huyse, A probabilistic framework for risk prediction of gas turbine engine components with inherent or induced material anomalies, ASME Paper, 2005-GT-68982, 2005.

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