트러스를 이용한 중력 보상기구의 합성방법
- Author(s)
- 김상형
- Issued Date
- 2016
- Keyword
- Associated linkage, Baranov truss, Deletion rules, Design equation, Gravity compensation, Static balancing, Space mapping
- Abstract
- This research presents a synthesis method by which a static balancer of a truss is transformed into static balancers of various mechanisms. For conventional design methods the kinematics and potential energy of every mechanism should be computed to design a static balancer. To overcome this limitation the concepts of kinematic syntheses (e.g., Baranov truss and associated linkage) are adopted to the design of a static balancer. The space mapping method is used to design a static balancer in this paper. A sliding mechanism can be derived from a Baranov truss combining two concepts of the Baranov truss and associated linkage. For example, elimination of a link at the 5-link Baranov truss results in a 4-bar linkage and a slider-crank mechanism can be derived from a 4-bar linkage when replacing a revolute joint by a prismatic joint. Variations of kinematic parameters and joint variables are investigated in the viewpoint of the static balancing during transforming a truss (or an associated linkage) to an associated linkage (or a sliding mechanism). The conversion rules are determined in which variations of kinematic parameters and joint variables are summarized in the viewpoint of the potential energy or gravitational torques. When applying the conversion rules to the design equation of the space mapping method, successive deletions of row and column vectors of the design equation occur. These deletion procedures are referred as the deletion rules in this paper. Static balancers of various mechanisms (four-bar linkage, Watt mechanism, Stephenson mechanism and sliding mechanisms) are derived from those of the five-link and seven-link Baranov trusses using the deletion rules. Thus, no computation of kinematics and potential energy is necessary to obtain static balancers of various mechanisms, once a static balancer of a truss has been designed. Simulations results showed that complete gravity compensation is achieved for all derived mechanisms from Baranov trusses. Experiments are conducted with the sliding mechanism derived from the seven-link Braranov truss and show that gravitational torques are effectively counterbalanced.
- Alternative Title
- Synthesis method of a static balancer using truss
- Alternative Author(s)
- Sanghyung Kim
- Affiliation
- 조선대학교 일반대학원
- Department
- 일반대학원 제어계측공학과
- Advisor
- 조창현
- Awarded Date
- 2017-02
- Table Of Contents
- ABSTRACT ix
제1장 서론 1
제1절 연구배경 1
제2절 연구목표 4
제2장 공간 사상 기법 9
제1절 공간 사상 9
제2절 두 공간에서의 포텐셜 에너지 10
제3절 설계 방정식 11
제4절 사상행렬의 결정 12
제3장 변환 설계방법 14
제1절 Baranov truss와 파생기구 사이의 관계 14
제2절 변형규칙 14
제3절 삭제규칙 16
제4장 Baranov truss의 중력보상기 설계 18
제1절 1에 대한 5-link Baranov truss 19
제2절 1의 대체 관절공간 22
제3절 2에 대한 7-link Baranov truss 24
제4절 3에 대한 7-link Baranov truss 27
제5절 Baranov truss의 중력보상기 31
제5장 설계 예 33
제1절 5-link Baranov truss에서 파생된 기구들 37
1. Case 1: Associated linkage 37
2. Case 2: Slider crank 39
3. Case 3: Swinging block linkage 40
4. Case 4: Turning block linkage 40
5. Case 5: Cardanic motion 41
6. 5-link Baranov truss에서 파생된 기구의 중력보상기 42
7. 미끄럼 관절의 고려 43
제2절 7-link Baranov truss에서 파생된 기구들 I 46
1. Case 1: Associated linkage 48
2. Case 2: Sliding mechanism 1 49
3. Case 3: Sliding mechanism 2 51
4. Case 4: Sliding mechanism 3 52
5. Case 5: Sliding mechanism 4 53
6. Case 6: Sliding mechanism 5 55
7. 7-link Baranov truss에서 파생된 기구의 중력보상기 I 57
제3절 7-link Baranov truss에서 파생된 기구들 II 59
1. Case 1: Associated linkage 61
2. Case 2: Sliding mechanism 1 62
3. Case 3: Sliding mechanism 2 63
4. Case 4: Sliding mechanism 3 65
5. Case 5: Sliding mechanism 4 67
6. 7-link Baranov truss에서 파생된 기구의 중력보상기 II 69
제4절 등가 중력보상기 71
제6장 모의실험 75
제7장 실험 84
제8장 토의 86
제9장 결론 90
참고문헌 92
CURRICULUM VITAE 96
- Degree
- Master
- Publisher
- 조선대학교 일반대학원
- Citation
- 김상형. (2016). 트러스를 이용한 중력 보상기구의 합성방법.
- Type
- Dissertation
- URI
- https://oak.chosun.ac.kr/handle/2020.oak/13205
http://chosun.dcollection.net/common/orgView/200000266205
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