Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling
Near- α titanium alloys have extensive applications in high temperature structural components of aircrafts. To manufacture complex-shaped titanium alloy panel parts with desired microstructure and good properties, an innovative low-cost hot stamping process for titanium alloy was stud...
| Main Authors: | , , , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2019-01-01
|
| Series: | Materials |
| Subjects: | |
| Online Access: | http://www.mdpi.com/1996-1944/12/2/223 |
| _version_ | 1811289663389827072 |
|---|---|
| author | Zhiqiang Li Haitao Qu Fulong Chen Yaoqi Wang Zinong Tan Mateusz Kopec Kehuan Wang Kailun Zheng |
| author_facet | Zhiqiang Li Haitao Qu Fulong Chen Yaoqi Wang Zinong Tan Mateusz Kopec Kehuan Wang Kailun Zheng |
| author_sort | Zhiqiang Li |
| collection | DOAJ |
| description | Near- α titanium alloys have extensive applications in high temperature structural components of aircrafts. To manufacture complex-shaped titanium alloy panel parts with desired microstructure and good properties, an innovative low-cost hot stamping process for titanium alloy was studied in this paper. Firstly, a series of hot tensile tests and Scanning Electron Microscope (SEM) observations were performed to investigate hot deformation characteristics and identify typical microstructural evolutions. The optimal forming temperature range is determined to be from 750 °C to 900 °C for hot stamping of TA15. In addition, a unified mechanisms-based material model for TA15 titanium alloy based on the softening mechanisms of recrystallization and damage was established, which enables to precisely predict stress-strain behaviors and potentially to be implemented into Finite Element (FE) simulations for designing the reasonable processing window of structural parts for the aerospace industry. |
| first_indexed | 2024-04-13T03:59:34Z |
| format | Article |
| id | doaj.art-1ad6294968b04e058d5cd7a42ade0b8c |
| institution | Directory Open Access Journal |
| issn | 1996-1944 |
| language | English |
| last_indexed | 2024-04-13T03:59:34Z |
| publishDate | 2019-01-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Materials |
| spelling | doaj.art-1ad6294968b04e058d5cd7a42ade0b8c2022-12-22T03:03:31ZengMDPI AGMaterials1996-19442019-01-0112222310.3390/ma12020223ma12020223Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and ModellingZhiqiang Li0Haitao Qu1Fulong Chen2Yaoqi Wang3Zinong Tan4Mateusz Kopec5Kehuan Wang6Kailun Zheng7Metal Forming Technology Department, AVIC Manufacturing Technology Institute, Beijing 100024, ChinaMetal Forming Technology Department, AVIC Manufacturing Technology Institute, Beijing 100024, ChinaMetal Forming Technology Department, AVIC Manufacturing Technology Institute, Beijing 100024, ChinaMetal Forming Technology Department, AVIC Manufacturing Technology Institute, Beijing 100024, ChinaDepartment of Mechanical Engineering, Imperial College London, London SW7 2AZ, UKDepartment of Mechanical Engineering, Imperial College London, London SW7 2AZ, UKDepartment of Mechanical Engineering, Imperial College London, London SW7 2AZ, UKDepartment of Mechanical Engineering, Imperial College London, London SW7 2AZ, UKNear- α titanium alloys have extensive applications in high temperature structural components of aircrafts. To manufacture complex-shaped titanium alloy panel parts with desired microstructure and good properties, an innovative low-cost hot stamping process for titanium alloy was studied in this paper. Firstly, a series of hot tensile tests and Scanning Electron Microscope (SEM) observations were performed to investigate hot deformation characteristics and identify typical microstructural evolutions. The optimal forming temperature range is determined to be from 750 °C to 900 °C for hot stamping of TA15. In addition, a unified mechanisms-based material model for TA15 titanium alloy based on the softening mechanisms of recrystallization and damage was established, which enables to precisely predict stress-strain behaviors and potentially to be implemented into Finite Element (FE) simulations for designing the reasonable processing window of structural parts for the aerospace industry.http://www.mdpi.com/1996-1944/12/2/223TA15hot stampingphase evolutiondeformationmodelling |
| spellingShingle | Zhiqiang Li Haitao Qu Fulong Chen Yaoqi Wang Zinong Tan Mateusz Kopec Kehuan Wang Kailun Zheng Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling Materials TA15 hot stamping phase evolution deformation modelling |
| title | Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling |
| title_full | Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling |
| title_fullStr | Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling |
| title_full_unstemmed | Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling |
| title_short | Deformation Behavior and Microstructural Evolution during Hot Stamping of TA15 Sheets: Experimentation and Modelling |
| title_sort | deformation behavior and microstructural evolution during hot stamping of ta15 sheets experimentation and modelling |
| topic | TA15 hot stamping phase evolution deformation modelling |
| url | http://www.mdpi.com/1996-1944/12/2/223 |
| work_keys_str_mv | AT zhiqiangli deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT haitaoqu deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT fulongchen deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT yaoqiwang deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT zinongtan deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT mateuszkopec deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT kehuanwang deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling AT kailunzheng deformationbehaviorandmicrostructuralevolutionduringhotstampingofta15sheetsexperimentationandmodelling |