New insights into thermomechanical fatigue behavior of AISI Type 316 LN SS weld joint

Author(s):  
Suresh Kumar Telagathoti ◽  
Nagesha Atikukke ◽  
Kannan Ramamurthy
2017 ◽  
Vol 47 (3) ◽  
pp. 1881-1895 ◽  
Author(s):  
Yong Zuo ◽  
Thomas R. Bieler ◽  
Quan Zhou ◽  
Limin Ma ◽  
Fu Guo

Author(s):  
T. Coppola ◽  
S. Riscifuli ◽  
O. Tassa ◽  
G. Pasquero

Highly cooled turbine blades undergo very high thermal gradients during rapid engine idle-max-idle cycling. Traditional isothermal fatigue data are often insufficient for predicting service lives. A complete set of high temperature tests, in the range of 750–1050°C, was performed on single crystal alloy CMSX-4. The test program comprised tensile, creep, low cycle fatigue, and thermomechanical fatigue (TMF) tests. In particular the cycle time for TMF was 3 min, aiming to simulate the real high-power transient conditions in aircraft engines. Clockwise and counterclockwise diamond cycle types were applied on bare and coated specimens to investigate their influence on the fatigue limit. The comparison of the results obtained with the available ones from open literature is discussed.


2020 ◽  
Vol 789 ◽  
pp. 139676 ◽  
Author(s):  
Bingbing Li ◽  
Yiming Zheng ◽  
Caiming Liu ◽  
Qite Li ◽  
Zhe Zhang ◽  
...  

2020 ◽  
Vol 2020 ◽  
pp. 1-11
Author(s):  
Wei Li ◽  
Huitao Chen ◽  
Lu Zuo ◽  
Jian Chen ◽  
Dongliang Xu ◽  
...  

The thermomechanical fatigue (TMF) behaviors of spray-deposited SiCp-reinforced Al-Si alloy were investigated in terms of the size of Si particles and the Si content. Thermomechanical fatigue experiments were conducted in the temperature range of 150-400°C. The cyclic response behavior indicated that the continuous cyclic softening was exhibited for all materials, and the increase in SiC particles size and Si content aggravated the softening degree, which was attributed to dislocation generation due to differential thermal contraction at the Al matrix/Si phase interface or Al matrix/SiC particle interface. Meanwhile, the TMF life and stress amplitude of SiCp/Al-7Si composites were greater than those of Al-7Si alloy, and increased with the increasing SiC particle size, which was associated with “load sharing” of the direct strengthening mechanism. The stress amplitude of 4.5μmSiCp/Al-Si composite increased as the Si content increased; however, the influence of Si content on the TMF life was not so significant. The TMF failure mechanism revealed that the crack mainly initiated at the agglomeration of small-particulate SiC and the breakage of large-particulate SiC, and the broken primary Si and the exfoliated eutectic Si accelerated the crack propagation.


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