무인기용 발사장비의 추진와이어 파단 및 구조변형 방지를 위한 형상변경 사례

• Published in: 品質經營學會誌 Vol. 50; no. 3; pp. 533 - 543
• Main Authors: 임다훈, Lim Dahoon, 박경환, Park Gyeong Hwan
• Format: Journal Article
• Language: Korean
• Published: 한국품질경영학회 30.09.2022
• Subjects: Configuration Change; Fracture; Launch System; Structural Deformation; UAV; 학제간연구; Configuration Change; Fracture; Structural Deformation; UAV; Launch System
• ISSN: 1229-1889; 2287-9005
• DOI: 10.7469/JKSQM.2022.50.3.533

Purpose: The purpose of this study is to identify and resolve the causes of defects in the unmanned aerial vehicle launch system(propulsion wire fracture, rear rail deformation) and to prevent recurrence. Methods: The causes of the two defects were derived through fault tree analysis for each of the two defects and fault reproduction tests. In the case of propulsion wire, the installation of a high speed camera to check the behavior of wire was the driving force behind the defect resolution. Results: The results of this study are as follows; It was determined that the thickness of the washer was less than the maximum tolerance of the pulley was the cause of the propulsion wire fracture defect. Failure to comply with the launch procedure and insufficient safety margin were judged as the cause of the rear rail deformation defect. Accordingly, the configuration was changed to remove each defect. Conclusion: The case of this study was conducted to eliminate defects in the launch system for UAV. The causes of defects were estimated through fault tree analysis. After the configuration change, Structural analysis and launch tests were performed to demonstrate the safety and effectiveness of the modified configuration. As a result, the effect of the modified configuration was verified.