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Development of Aircraft 2-Stage Differential GRA

항공기용 2단 차동 GRA 개발

  • Lee, Kang-Hee (Corporation KIM) ;
  • Im, Dae-Jin (Corporation KIM) ;
  • Lee, Sun-Hong (Corporation KIM) ;
  • Park, Seul-Ki (Research Center for Aircraft Parts Technology, School of Mechanical and Aerospace Engineering, Gyeongsang National UNIV.) ;
  • Choi, Jin-Ho (Research Center for Aircraft Parts Technology, School of Mechanical and Aerospace Engineering, Gyeongsang National UNIV.)
  • Received : 2016.11.10
  • Accepted : 2016.12.08
  • Published : 2016.12.30

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.

Keywords

References

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