Handbook of Case Histories in Failure Analysis
Stress-Rupture Characterization in Nickel-Based Superalloy Gas Turbine Engine Components
-
Published:2019
Abstract
This article describes the visual, fractographic, and metallographic evidence typically encountered when analyzing stress rupture of turbine airfoils. Stress-rupture fractures are generally heavily oxidized, tend to be rough in texture, and are primarily intergranular and/or interdendritic in appearance compared to smoother, transgranular fatigue type fractures. Often, gross plastic yielding is visible on a macroscopic scale. Commonly observed microstructural characteristics include creep voiding along grain boundaries and/or interdendritic regions. Internal voids can also nucleate at carbides and other microconstituents, especially in single crystal castings that do not possess grain boundaries.
Wesley D. Pridemore, Stress-Rupture Characterization in Nickel-Based Superalloy Gas Turbine Engine Components, Handbook of Case Histories in Failure Analysis, Vol 3, Edited By Larry Berardinis, ASM International, 2019, p 43–50, https://doi.org/10.31399/asm.fach.v03.c9001758
Download citation file:
Data Ecosystem
The ASM Data Ecosystem is a new and innovative product line that arms ASM Members and the scientific community with the tools and data required to exponentially expand the boundaries of materials science to meet the needs of Industry 4.0.