Mg합금의 고온변형과 기계적 성질 및 감쇠능에 관한 연구
- Alternative Title
- A Study on the High Temperature Deformation, Mechanical Properties and Damping Capacity of Magnesium Alloys
- Abstract
- Magnesium is known to have a good damping capacity compared to other known metals and their alloys. Also, the damping properties of metals are generally recognized to be dependent on microstructural factors such as grain size and dislocation etc. However, there are only few studies about the damping capacity of magnesium alloys.
Therefore, in this study, effect of heat treatment on the microstructure, their mechanical properties and damping capacity of two kinds of specimens AZ31 (Mg-3Al-1Zn in mass%) and AZ61(Mg-6Al-1Zn in mass%) magnesium alloys ware investigated. The results obtained from the experiment are summarized as follows,
As a result of microstructure observation after hot-rolling, dendrite structure was formation and compounds was precipitated along the grain boundary in two kinds of specimens, and this precipitated compounds is found to be Mg17Al12. The Mg17Al12 compounds and dendrite ware decomposed and dissipated by annealing treatment. With increasing the annealing temperature and time, damping capacity was slowly increased by the growth of grain size and decreasing of defects.
Also, two kinds of magnesium alloys after annealing show no difference in damping capacity. After annealing of hot-rolled magnesium alloys, damping capacity rapidly decreased with an increase of strength. Strength and damping capacity show proportional relationship. From the microstructure observation, fine and coarse grains were existed together by occurrence of DRX (Dynamic recrystallization) during high-temperature. The lower strain rate and higher temperature lead grain size to increases.
At the beginning stage, after the maximum stress (work softening) appeared, true stress decrease with an increase of true strain in all specimens. The faster strain rate and lower temperature, work softening behaviors rapidly occur. In case of flow stress, faster strain rate and lower temperature, flow stress increases. However, there were no differences according to the direction of processing. The lower strain rate and higher temperature, strain rate sensitivity index decreases. The degree of spring back is higher with increasing the radious of curvature, and the higher temperature and lower strain rate, spring back slightly increases.
After hot working, the strength of AZ61 magnesium alloy is much higher than that of AZ31 magnesium alloy. However, the elongation of two kinds of magnesium alloy do not show a significant difference. In case of damping capacity, with an increase of strength and elongation, damping capacity rapidly decreases.
- Author(s)
- 이규현
- Issued Date
- 2015
- Awarded Date
- 2015. 2
- Type
- Dissertation
- Publisher
- 부경대학교 일반대학원
- URI
- https://repository.pknu.ac.kr:8443/handle/2021.oak/11889
http://pknu.dcollection.net/jsp/common/DcLoOrgPer.jsp?sItemId=000001967508
- Alternative Author(s)
- Lee Gyu Hyun
- Affiliation
- 부경대학교 일반대학원
- Department
- 대학원 금속공학과
- Advisor
- 강창룡
- Table Of Contents
- Abstract ⅳ
제 1 장 서 론 1
1.1 연구배경 2
제 2 장 이론적 배경 6
1.1 마그네슘 및 마그네슘합금의 일반적인 특징 7
1.1.1 경량성과 비강도 7
1.1.2 전자파 차폐성 8
1.1.3 진동감쇠능 9
1.1.4 치수 안정성 9
1.1.5 주조성 9
1.1.6 재활용성 11
1.1.7 절삭성 11
1.2 마그네슘 합금의 슬립변형 11
1.3 순 Mg과 Mg-Zr 합금의 진동 감쇠능 기구 14
1.3.1 Mg 합금의 연구동향 17
1.4 동적재결정 19
1.5 Mg-Al 합금의 상태도 20
제 3 장 열간가공한 Mg 합금의 감쇠능에 미치는 어닐링처리의 영향 25
1. 서 론 26
2. 실험방법 28
2.1 시료 28
2.2 열간압연 28
2.3 열처리 28
2.4 미세조직 관찰 29
2.5 감쇠능 측정 29
3. 실험결과 및 고찰 30
3.1 미세조직 관찰 30
3.2 미세조직 변화에 미치는 열처리의 영향 31
3.3 감쇠능에 미치는 열처리의 영향 35
4. 결 론 44
제 4 장 AZ31 마그네슘합금의 고온 변형, 인장 및 성형성에 대한 연구 45
1. 서 론 46
2. 실험방법 48
2.1 시료 48
2.2 미세조직 관찰 48
2.3 고온 인장 변형 시험 48
2.4 성형성 시험 49
3. 실험결과 및 고찰 52
3.1 미세조직 관찰 52
3.2 고온 인장 특성 변화 53
3.3 변형률 속도 민감지수 변화 58
3.4 성형성에 미치는 변형조건의 영향 60
4. 결 론 76
제 5 장 열간 압연후 어닐링처리한 Mg 합금의 인장성질과 감쇠능의 상호관계 77
1. 서 론 78
2. 실험방법 80
2.1 시료 80
2.2 열간압연 80
2.3 어닐링처리 80
2.4 미세조직 관찰 80
2.5 인장성질 측정 81
2.6 감쇠능 측정 81
3. 실험결과 및 고찰 82
3.1 미세조직 관찰 82
3.2 인장성질에 미치는 어닐링열처리의 영향 84
3.3 인장성질과 감쇠능과의 관계 92
4. 결 론 103
제 6 장 결 론 104
참고문헌 107
- Degree
- Doctor
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