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Fatigue Life Prediction of TC4 Titanium Alloy Bolted Structures in Thermal Environments Below 400 °C Using an
Hang Peng1, Bintuan Wang1, Jianbo Qin1
1AVIC The First Aircraft Institute, Xi'an 710089, China.
Materials (Basel, Switzerland)
|March 28, 2026
Summary
An enhanced fatigue prediction method accurately assesses TC4 titanium alloy bolted structures up to 400°C. This new detail fatigue rating (DFR) approach improves accuracy for aerospace applications in moderate thermal environments.
Area of Science:
- Materials Science
- Mechanical Engineering
- Aerospace Engineering
Background:
- TC4 titanium alloy bolted structures are critical in aerospace, especially in aircraft engines.
- Existing fatigue life prediction methods are insufficient for moderate elevated temperatures (up to 400°C).
Purpose of the Study:
- To develop an enhanced detail fatigue rating (DFR) method for TC4 titanium alloy bolted structures under thermal conditions up to 400°C.
- To improve the accuracy of fatigue life prediction in moderate temperature environments.
Main Methods:
- Acquired fatigue life data for TC4 titanium alloy at 20°C, 200°C, and 400°C.
- Developed an enhanced DFR method incorporating temperature-dependent thermal effects.
- Applied the enhanced DFR method to predict fatigue life of double-shear TC4 bolted structures.
Main Results:
- The enhanced DFR method demonstrated improved fatigue life estimation accuracy.
- Average fatigue life estimation accuracy increased by 9.29% compared to the conventional DFR method.
- The proposed method shows high promise for evaluating fatigue performance within the 20-400°C range.
Conclusions:
- The enhanced DFR method provides a more accurate tool for predicting the fatigue life of TC4 bolted structures at moderate elevated temperatures.
- This advancement is crucial for ensuring the safety and reliability of aerospace components operating in thermal environments up to 400°C.
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