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한국형 기동헬기 꼬리 날개 디페인팅 현상을 통한 도장 품질 향상에 관한 연구

A study on improvement of painting quality through a de-painting phenomenon of KUH-1 tail blade

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초록

Purpose: The purpose of this study was to explain de-painting phenomenon of KUH-1 tail blade and to propose useful solution of it by test. The proposed solution was evaluated by real flight, and then it applied to mass product to improve the paint qual ity of KUH-1 tail bl ade. Methods: This study investigated an adhesive ability of primer following surface sanding condition. The cross cut and scratch test were conducted to evaluate the adhesive strength. And the water flow test was designed to simulate a real flight condition under rain. Through water flow test, an optimal condition of tail blade to prevent a de-painting phenomenon was deduced. Finally, the improvement method was evaluated by real flight under rain. Results: The results of this study are as follows; The sequential polishing was most excellent method in primer painting quality. The results of test including cross cut, scratch and water flow showed that MIL-DTL-53039 paint with epoxy primer has excellent adhesive ability. To proof the effect of improvement, a real flight during a rain condition was conducted. Finally, the comparison between original and improvedconfiguration was conducted. Conclusion: The painting quality of KUH-1 tail blade was improved through deriving an optimal painting condition. In detail, a condition of optimal sanding and a sort of primer and paint was showed. Finally, the reliability of tail blade was guaranteed through improving the quality of painting.

Abstract

Purpose: The purpose of this study was to explain de-painting phenomenon of KUH-1 tail blade and to propose useful solution of it by test. The proposed solution was evaluated by real flight, and then it applied to mass product to improve the paint qual ity of KUH-1 tail bl ade. Methods: This study investigated an adhesive ability of primer following surface sanding condition. The cross cut and scratch test were conducted to evaluate the adhesive strength. And the water flow test was designed to simulate a real flight condition under rain. Through water flow test, an optimal condition of tail blade to prevent a de-painting phenomenon was deduced. Finally, the improvement method was evaluated by real flight under rain. Results: The results of this study are as follows; The sequential polishing was most excellent method in primer painting quality. The results of test including cross cut, scratch and water flow showed that MIL-DTL-53039 paint with epoxy primer has excellent adhesive ability. To proof the effect of improvement, a real flight during a rain condition was conducted. Finally, the comparison between original and improvedconfiguration was conducted. Conclusion: The painting quality of KUH-1 tail blade was improved through deriving an optimal painting condition. In detail, a condition of optimal sanding and a sort of primer and paint was showed. Finally, the reliability of tail blade was guaranteed through improving the quality of painting.

참고문헌 (15)

  1. American Institute of Marine Science(AIMS), "Airbus Industry Material Specification External paint system : wash primer + primer + top coat Material Specification", AIMS 04-04-012, ~ (2001)
  2. American Society for Testing Materials(ASTM), "Standard Test Methods for Measuring Adhesion by Tape Test", ASTM D3359-09, ~ (2009)
  3. American Society for Testing Materials(ASTM), "Standard Test Method for Adhesion of Organic Coatings by Scrape Adhesion", ASTM D2197-13, ~ (2013)
  4. British Standards, "Paint and Varnishes-Determination of scratch resistance-part1, Constant -Loading Method", EN ISO 1518, ~ (2011)
  5. Defense Acquisition Program Administration(DAPA), "KUH process specification for finish requirement", A88MP0001, 6~7 (2013)
  6. Defense Acquisition Program Administration(DAPA), "Korean Utility Helicopter", KDS 1520-4001, ~ (2013)
  7. Defense Acquisition Program Administration(DAPA), "Rotary Wing Blade Specification", KDS 1615-4003, 6~15 (2013)
  8. DoD(Department of Defense), "Coating compound metal pretreatment", MIL-C-8514, ~ (1967)
  9. DoD(Department of Defense), "Water Dispensible Aliphatic Polyurethane, CARC", MIL-DTL-64159, ~ (2002)
  10. DoD(Department of Defense), "Coating, Aliphatic Polyurethane, Single Component, CARC", MIL-DTL-53039, ~ (2011)
  11. DoD(Department of Defense), "Primer coatings, epoxy, high solids", MIL-PRF-23377, ~ (2012)
  12. Kim, Soon-Kyung., "A study on the Effect of Surface Roughness os Strip for Automobile in the paintability", Journal of The Korean Society of Mechanical Engineers, A(7), pp.1326~1335 (1998)
  13. Moon, Seung-Hyun., "The Characteristics of Roughness and Scratch by the Coating Effect on Aluminum Sheet", Spring Conference of The Korean Society of Mechanical Engineers, pp.557~560 (2009)
  14. 심재동, "생체의료용 티타늄합금의 연구개발 동향", 생체재료학회지, 15(4), pp.176~183 (2011), 한국생체재료학회
  15. 윤한기, "알루미늄 판재의 센딩조건에 따른 도장특성 평가", 한국해양공학회지, 25(1), pp.44~48 (2011), 한국해양공학회

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