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Definition of parameters of strength reliability of details of aircraft engines at a design stage
- Authors: 1 11, 1 11
-
Affiliations:
- Samara State Aerospace University
- Issue: Vol 5, No 2-1 (2006): Special Issue
- Pages: 296-301
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/347
- DOI: https://doi.org/10.18287/2541-7533-2006-0-2-1(10)-296-301
- ID: 347
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Abstract
The technique of definition of parameters of no-failure operation of aircraft engines details is in-process observed. For this purpose the dispersion of stresses in a detail by a method of a linearization and the Monte-Carlo method offered by authors in a packet of certainly-element analysis ANSYS is considered.
About the authors
1 1
Samara State Aerospace University
Author for correspondence.
Email: sadohina@ssau.ru
Russian Federation
1 1
Samara State Aerospace University
Email: sadohina@ssau.ru
Russian Federation
References
- Белоусов А. И., Биргер И. А. Прочностная надежность деталей турбомашин: Учебное пособие. – Куйбышев: КуАИ, 1983. – 75с.
- Расчет надежности деталей авиационных газотурбинных двигателей: Учеб. Пособие / А. С. Москаленко, - Харьков: Харьк. авиац. Ин-т, 1985. – 107с.
- Кузнецов Н. Д., Цейтлин В. И. Эквивалентные испытания газотурбинных двигателей. – М.: Машиностроение, 1976. – 216с.
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