DOI QR코드

DOI QR Code

Modeling of MR Damper Landing Gear Considering Incompletely Developed Fluid Flow

불완전 발달 유체 유동을 고려한 MR댐퍼 착륙장치 모델링

  • Lee, Hyo-Sang (Dept. of Aerosapce of Mechanical Engineering, Graduate at KAU) ;
  • Jang, Dae-Sung (Dept. of Aerosapce of Mechanical Engineering, Korea Aerospace University) ;
  • Hwang, Jai-Hyuk (Dept. of Aerosapce of Mechanical Engineering, Korea Aerospace University)
  • 이효상 (한국항공대학교 항공우주 및 기계공학과) ;
  • 장대성 (한국항공대학교 항공우주 및 기계공학부) ;
  • 황재혁 (한국항공대학교 항공우주 및 기계공학부)
  • Received : 2020.07.06
  • Accepted : 2020.11.06
  • Published : 2021.02.28

Abstract

A semi-active MR damper landing gear is a damper that generates a fluid damping force and a magnetic field control damping force when the MR fluid passes through annular flow paths. In the case of MR fluid passing through annular flow paths, an incompletely developed flow inevitably occurs, causing an error in calculating damper inner forces including the fluid damping force. This error results in an inaccurate design of damper structural parameters and control gain selection, resulting in deterioration of dynamic characteristics and shock absorption performance of the landing gear. In this paper, we derived a mathematical model of an MR damper landing gear considering additional damping force generated in the entrance region of annular flow paths of the MR damper. If the mathematical modeling derived from this paper is applied to the design and optimization process of an MR damper landing gear, excellent performance of the MR damper landing gear is expected.

반능동형 MR댐퍼 착륙장치는 MR유체가 환형 유로를 지날 때 유체감쇠력 및 자장 제어 감쇠력을 발생시키는 댐퍼이다. 환형 유로를 지나는 MR 유체의 경우 필연적으로 불완전 발달 유동이 발생하게 되어, 이는 유체 감쇠력을 포함하는 댐퍼 내력 계산에 오차를 발생시키는 원인이 된다. 이로 인해 댐퍼 구조적 파라미터 설계 및 제어 이득 선정이 부정확해지며, 착륙장치의 동특성 및 충격흡수성능 저하를 초래하게 된다. 본 논문에서는 MR댐퍼 환형 유로의 입구영역에서 발생하는 추가적인 감쇠력을 고려한 MR댐퍼 착륙장치의 수학적 모델을 유도하였다. 본 논문에서 유도한 수학적 모델링을 MR댐퍼 착륙장치의 설계 및 최적화 과정에 적용한다면 좀 더 정확한 내력 예측으로 우수한 성능의 MR댐퍼 착륙장치를 설계할 수 있을 것으로 판단된다.

Keywords

References

  1. J. M. Tak, "A Hybrid Control Technique of the Intelligent Landing Gear with Variable Damping Force," MS Thesis, Korea Aerospace University, Gyeong-gi, Republic of Korea, February, 2018.
  2. Chulhee Han, Byung-Hyuk Kang, Seung-Bok Choi, Jun Mo Tak and Jai-Hyuk Hwang, "Control of Landing Efficiency of an Aircraft Landing Gear System With Magnetorheological Dampers," Journal of Aircraft, Vol. 56, pp. 1981-1986, September, 2019.
  3. Ahuree-Powell, L. A., "Magnetorheological Fluids and Applications to Adaptive Landing Gear for a Lightweight Helicopter," Ph. D. Thesis, University of Maryland, Maryland, United States of America, 2014.
  4. Eroglu, M. A., "Observer Based Control of an Magnetorheological Damper," Ph. D. Thesis, University of Sheffield, Sheffield, United Kingdom, 2013.
  5. Quoc Viet Luong, Dae-Sung Jang and Jai-Hyuk Hwang, "Robust Adaptive Control for an Aircraft Landing Gear Equipped with a Magnetorheological Damper," Applied Sciences, Vol. 10, pp. 1459-1475, 2020. https://doi.org/10.3390/app10041459
  6. J. M. Tak, L. Q. Viet, and J. H. Hwang, "Hybrid Control of Aircraft Landing Gear using Magnetorheological Damper," Journal of Aerospace System Engineering, Vol.12, No.1, pp.1-9, February, 2018. https://doi.org/10.20910/JASE.2018.12.1.1
  7. Y. O. Hyun, "Semi-Active Force Control of Landing Gear using Magneto-Rheological Damper," Ph. D. dissertation, School of Aerospace and Mechanical Engineering, Korea Aerospace University, 2009.
  8. T. S. LUNDGRENG, E. M. SPARROW, J. B. STARR, "Pressure Drop Due to the Entrance Region in Ducts of Arbitrary Cross Section," ASME Trans. Journal of Basic Engineering, Vol. 86, pp. 620-626, September 1964. https://doi.org/10.1115/1.3653186
  9. Jae-Up hwang, jae-hyuk hwnag, jae-Sung Bae, young-O Hyun, Kyoung-ho Lim, Doo-Man Kim, Tae-Wook Kim, "Smi-Active Control of helicompter Landing Gear using Magneto-Rheological Damper," Journal of Aerospace System Engineering, Vol. 36, pp. 346-351, February, April, 2008.
  10. Bo-Gyu Kim, Chulhee Han, Seung-Bok Choi, "Design and Analysis of MR Damper for Airplane Landing Gear," Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 28, pp. 102-109, February, 2018. https://doi.org/10.5050/KSNVE.2018.28.1.102
  11. Byung-Hyuk Kang, Chulhee Han, Seung-Bok Choi, "Design of Sky-ground Hook Controller for MR Damper of Aircraft Landing Gear," Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 29, pp. 222-229, 2019. https://doi.org/10.5050/KSNVE.2019.29.2.222
  12. Mahboubeh Khani, "Magneto-Rheological (MR) Damper for Landing Gear System," MS Thesis, Concordia University, Montreal, Quebec, Canada, June, 2010.
  13. Young-Tai Choi, Norman M. Wereley, "Vibration Control of a Landing Gear System Featuring Electrorheological/Magnetorheological Fluids," Journal of Aircraft, Vol. 40, No. 3, May-June, 2003.
  14. Milwitzky, B., and Cook, F., "Analysis of Landing Gear Behavior," NACA TN 2755, 1952.
  15. Currey, N., "Aircraft Landing Gear Design Principles and Practices," AIAA Education Series, 1988.
  16. Janusa Wojtkowiak, Czeslqw O. Popiel, "Inherently Linear Annular-Duct-Type Laminar Flowmeter," ASME Trans. Journal of Fluids Engineering, Vol.128, January 2006.
  17. Milwitzky, B., and Cook, F., "Analysis of Landing Gear Behavior," NACA TN 2755, 1952.
  18. Guang Yang, B.S, "Large-Scale Magnetorheological Fluid for Vibration Mitigation: Modeling, Testing and Control," MS Thesis, University of Notre Dame, Notre Dame, Indiana, United States of America, December, 2001.