Evidence map›Paper›PMID 40429012›Full record

ArticleMaterials (Basel, Switzerland)2025

Research on Creep Deformation of Dissimilar FSWed T-Joints Under Different Ultrasonic Vibration Modes: Experiment, Constitutive Model, and Simulation Verification.

Ti Ye, Yanjie Han, Duquan Zuo, Haoran Fu, Shilin Feng, Chong Gao, Wenya Li

Abstract read
In one paragraph

Article in Materials (Basel, Switzerland), 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 1 paper.

0numbers the graph read from it
0cells of the map it votes in
1citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

1 citing paper in PubMed.

  1. Article
4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

7 authors.

Ti YeCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.
Yanjie HanCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.
Duquan ZuoCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.ORCID 0000-0002-5053-0400
Haoran FuCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.
Shilin FengCollege of Aviation Engineering, Civil Aviation Flight University of China, 46, Nanchang Road, Guanghan 618307, China.
Chong GaoSchool of Engineering, University of Tokyo, 7-3-1 Hongo, Bunkyo, Tokyo 113-8656, Japan.ORCID 0000-0001-9764-853X
Wenya LiSchool of Materials Science and Engineering, Northwestern Polytechnical University, 127 West Youyi Road, Xi'an 710072, China.ORCID 0000-0002-5067-843X

Funding

China Postdoctoral Science Foundation NO. 2022M722592Fundamental Research Funds for the Central Universities NO. 24CAFUC07002Sichuan Province Engineering Technology Research Center of General Aircraft Maintenance NO. GAMRC2023ZD03
6 · The paper itself

Abstract

This article presents experimental and numerical studies on the creep deformation of 7055-T6 Al and 2197-T8 Al-Li T-joints. Firstly, the optimal process parameters for creep tensile tests (CATs) are determined to be 155 °C, 130 MPa, and 8 h. Based on this, different modes of ultrasonic vibration are introduced. It is found that under the same amplitude, the creep limit of intermittent vibration is 64.7‱ to 97.2‱ higher than that of continuous vibration, and the tensile strength of the former specimens is significantly better than that of the latter. Further analysis reveals that during long-duration or high-amplitude vibrations, the joint material exhibits hardening effects, while short-duration, low-amplitude intermittent vibrations result in softening effects. When the amplitude is 12.53 μm, the material exhibits optimal comprehensive mechanical properties, with yield strengths, tensile strengths, and elongations of 402.1 MPa, 429.3 MPa, and 7.9%, respectively. Additionally, based on the mechanisms of superposition and acoustic softening effects, an improved creep aging constitutive model is established, which incorporates the creep process, stress superposition, and ultrasonic softening changes and is applied in ABAQUS. It is found that at an amplitude of 12.53 μm, the residual stress in the joint is more thoroughly eliminated and distributed more evenly, measuring 97.35 MPa. Moreover, the creep strain calculated using the above model in a finite element analysis shows a high degree of agreement with the experimental results, indicating that the proposed model can more accurately predict the creep deformation behavior of FSWed T-joints during the CAT process.

Indexed as

constitutive modelcreep deformationFSWT-jointsultrasonic vibration

Identifiers

PMID40429012
PMCPMC12112799

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