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pro vyhledávání: '"E. E. Kocherova"'
Autor:
E. E. Kocherova
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 17, Iss 1, Pp 61-71 (2018)
This article presents an example of calculating the durability of a real part of a gas turbine engine. The part under examination had problems in its operation due to origination of cracks, exhaustion of load bearing capacity and non-localized fractu
Externí odkaz:
https://doaj.org/article/348c2625707144079cb13264118e61dd
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 16, Iss 1, Pp 129-136 (2017)
To calculate the durability of gas turbine engine parts damaged by low-cycle fatigue (LCF), according to the Structural codes of turbine engine strength it is necessary to test specimens cut from respective parts (or test coupons) under hard loading.
Externí odkaz:
https://doaj.org/article/7bcf040373e2420e808abab44d438353