항공기용 2단 차동 GRA 개발open accessDevelopment of Aircraft 2-Stage Differential GRA
- Other Titles
- Development of Aircraft 2-Stage Differential GRA
- Authors
- 이강희; 임대진; 이선홍; 박슬기; 최진호
- Issue Date
- 2016
- Publisher
- 한국기계가공학회
- Keywords
- GRA(Geared Rotary Actuator; 기어식 회전 작동기); Planetary Gear(유성기어)
- Citation
- 한국기계가공학회지, v.15, no.6, pp 115 - 121
- Pages
- 7
- Indexed
- KCI
- Journal Title
- 한국기계가공학회지
- Volume
- 15
- Number
- 6
- Start Page
- 115
- End Page
- 121
- URI
- https://scholarworks.gnu.ac.kr/handle/sw.gnu/15950
- DOI
- 10.14775/ksmpe.2016.15.6.115
- ISSN
- 1598-6721
2288-0771
- Abstract
- The aircraft flight control system controls an aircraft’s direction and flying attitude, and actuators are key components of control systems. Actuators can be classified as Geared Rotary Actuator (GRA) and Ball Screw Actuator (BSA). GRA is used in mid-sized aircraft, and BSA is used in larger aircraft.
A two-stage differential GRA model was suggested in this paper, and structural analysis and performance tests were performed. According to the analysis and experiment, the stiffness of the two-stage differential GRA was 17.57% higher than that of the conventional GRA, and the structural safety was improved.
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Collections - 공학계열 > 기계항공우주공학부 > Journal Articles

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