Analisis Geometri Dan Material Engsel Lentur Pada Rudder Model Isoleted Tail di Terowongan Angin

Prastiyo Siswo Prajoko, Yanuar Yanuar, I.Z Pane

Abstract


Pengujian hinge moments isolated tail di wind tunnel adalah pengujian yang bertujuan untuk mengetahui karakteristik fungsi kontrol kemudi rudder pada ekor pesawat terbang. Pengujian tersebut diperlukan pada saat pembuatan pesawat terbang. Engsel rudder memiliki peranan penting untuk menahan gaya saat diberikan hembusan angin, sehingga pesawat terbang tersebut mampu dikemudikan dengan efisien. Alat ukur yang digunakan untuk pengujian ini salah satunya adalah menggunakan sebuah engsel lentur simetris. Untuk dapat memperoleh alat ukur yang memadai, diperlukan pemilihan sensor strain guage dan material dengan melakukan analisa finite elemen pada tingkat deformasi dan stress test nya. Tingkat deformasi adalah kemampuan engsel lentur melakukan penyimpangan saat dibebankan oleh gaya. Material yang baik akan memiliki tingkat deformasi yang paling minimal. Terbatasnya referensi mengenai model deformasi untuk engsel lentur, menjadi tantangan penulis. Namun, sudah dilakukan validasi atas formulasi tingkat deformasi yang digunakan terhadap hasil perhitungan menggunakan persamaan parabolic dan software ANSYS 2023R2, dan diperoleh hasil pada tingkat validasi yang baik.
Kata kunci: Parabolik engsel lentur, finite element analisis, terowongan angin


Full Text:

PDF

References


Alan Pope J. B. Barlow, W. H. Rae, Jr, .1999.- Low Speed Wind Tunnel Testing. 1-John Wiley & Sons

C. F. Yang, J. H. Yan, and Z. B. Zhang, 2021 “Research on Moment Amplitude Modulation Coefficient of Unbonded Prestressed Concrete Continuous Beam,” in 2021 7th International Conference on Hydraulic and Civil Engineering and Smart Water Conservancy and Intelligent Disaster Reduction Forum, ICHCE and SWIDR 2021, Institute of Electrical and Electronics Engineers Inc., 2021, pp. 650–654. doi: 10.1109/ICHCESWIDR54323.2021.9656276.

CAI Wei-wei, YANG Le-ping, LIU Xin-jian, ZHU Yan-wei 2013 Robust Optimal Guidance for Hypersonic Glide Vehicle with Hinge Moment Constraint. IEEE Control Systems Society, Zhongguo xi tong gong cheng xue hui, Chinese Association for Artificial Intelligence, Chinese Association of Automation. Technical Committee on Control Theory, and Institute of Electrical and Electronics Engineers, 2013 25th Chinese Control and Decision Conference (CCDC) : May 25-27, 2013 : Guizhou Park Hotel, Guiyang, China.

Chen, Hongjiang .2011. Analysis of the Rigidity of Arc Flexible Hinge with Different Geometrical Parameters. 5th Computer and Computing Technologies in Agriculture (CCTA) https://inria.hal.science/hal-01361138

Chen, Xiaodong, Deng, Zilong, Hu, Siya, Gao, Jinhai,Gao, Xingjun. 2020. Design of a compliant mechanism based four-stage amplification piezoelectric-driven asymmetric microgripper https://www.mdpi.com/2072-666X/11/1/25

Chunhui Yang 2012 Calculation and Analysis of Parabolic Flexure Hinge Ha’erbin-Ligong-Daxue, Annual IEEE Computer Conference, International Conference on Measurement, I. and C. 2012. 05. 18-20 H., & MIC 2012.05.18-20 Harbin. (n.d.). International Conference on Measurement, Information and Control (MIC), 2012 18-20 May 2012, Harbin, China.

Dwi, Margi V. 2012. INTRODUKSI STRAIN GAUGE UNTUK PENGUJIAN MODEL PESAWAT DALAM WIND TUNNEL. INDEPT, Vol. 2, No. 3, Oktober 2012 2011 International Conference on Electrical and Control Engineering (ICECE) : Sept. 16-18, 2011, Yichang, China : Proceedings. (n.d.).

Gao Hao, Fan Jun-fang 2019 The Design Factor Analysis of a Miniaturized Rotating Guided Ammunition Actuator”. Proceedings of the 38th Chinese Control Conference July 27-30, 2019, Guangzhou, China

H. Li and J. Yang, 2019 “Study on one type of 4-position load simulator system technology based large moment of inertia and high torque,” in Proceedings - 2019 2nd World Conference on Mechanical Engineering and Intelligent Manufacturing, WCMEIM 2019, Institute of Electrical and Electronics Engineers Inc., Nov. 2019, pp. 364–368. doi: 10.1109/WCMEIM48965.2019.00078.

Huan Xie, Lixia Zhao, Wei Li, Bin Chen, ShengLin Xia, Jun Yin .2019 the optimization study on the mitigation strategy of hinge moment of aircraft with multi-control surfaces Institute of Electrical and Electronics Engineers, 2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence (ICUSAI).

J. He, B. Ai, X. Li, and R. Song, 2021 “Moment Test Technique of the Aircraft’s Water Rudder Hinge Based on Structural Loads,” in Proceedings - 2022 International Conference on Manufacturing, Industrial Automation and Electronics, ICMIAE 2022, Institute of Electrical and Electronics Engineers Inc., 2022, pp. 195–201. doi: 10.1109/ICMIAE57032.2022.00044.

Li, W., & Gao, C. (2010). Design and modeling of micro-displacement amplifying mechanism using revolute joints and flexible hinges. 2010 International Conference on Intelligent Computation Technology and Automation, ICICTA 2010, 1, 1147–1150. https://doi.org/10.1109/ICICTA.2010.681

Linß, S., Henning, S., & Zentner, L. (n.d.). Modeling and Design of Flexure Hinge-Based Compliant Mechanisms. www.intechopen.com

Liu, M., Li, Y., & Zhan, J. (2022). Multi-Material Topology Optimization of Flexure Hinges Using Element Stacking Method. Micromachines, 13(7). https://doi.org/10.3390/mi13070993

Liu, M., Zhang, X., & Fatikow, S. (2016). Design and analysis of a high-accuracy flexure hinge. Review of Scientific Instruments, 87(5). https://doi.org/10.1063/1.4948924

Masaaki Murakami, Koichi Yonemoto, Takahiro Fujikawa .2022. Ascent Guidance Trajectory Optimization Using Evolutionary Algorithm Considering Engine Gimbal and Aerodynamic Control International Journal of Aeronautical and Space Sciences (2022) 23:775–783 https://doi.org/10.1007/s42405-022-00466-3

Meymian, N. Z., Clark, N. N., Musho, T., Darzi, M., Johnson, D., & Famouri, P. (2018). An Optimization Method for Flexural Bearing Design for High-stroke High-Frequency Applications. https://www.elsevier.com/open-access/userlicense/1.0/

Miao Yang, Zhijiang Du, and Wei Dong 2015 Modeling and Analysis of a Superelastic Hinge Using Elliptic Flexure Co-rotational Beam Elements International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale (3M-NANO). (2015). IEEE.

Nicolae Lobontiu 2002 Compliant Mechanisms_ Design of Flexure Hinges-CRC Press

Nicolae Lobontiu 2020 Compliant Mechanisms_ Design of Flexure Hinges-CRC Press

Prasath, M., Ganesan, V. R., Sivaramakrishnan, A. E., Kurade, R., & Rao, S. (n.d.). ELEVATOR HINGE MOMENT STUDIES OVER GENERIC WINGED BODY CONFIGURATION.

Roopa, R., Navin Karanth, P., & Kulkarni, S. M. (2018). Effect of flexure beam geometry and material on the displacement of piezo actuated diaphragm for micropump. IOP Conference Series: Materials Science and Engineering, 310(1). https://doi.org/10.1088/1757-899X/310/1/012111

Smith, Stuart T. 2000 Flexures _ Elements of Elastic Mechanisms.-Chapman and Hall_CRC

Wang, C. N., Yang, F. C., Nguyen, V. T. T., Nguyen, Q. M., Huynh, N. T., & Huynh, T. T. (2021). Optimal design for compliant mechanism flexure hinges: Bridge-type. Micromachines, 12(11). https://doi.org/10.3390/mi12111304

Wang Tianhao, Qiu Junwen and Liu Xihe 2010 Definition Measurement Unit with Flexure Hinges for a Wind Tunnel Balance IEEE Robotics and Automation Society, Annual IEEE Computer Conference, IEEE International Conference on Information and Automation 7 2010.06.20-23 Harbin, & ICIA 7 2010.06.20-23 Harbin. (n.d.). IEEE International Conference on Information and Automation (ICIA), 2010 Harbin, China, 20-23 June 2010.

Wei, H., Wang, L., Niu, X., Zhang, J., Mao, Z., Simeone, A., & Zhang, Q. (n.d.). Study of Effective Hinge Thickness of Additive-manufactured Flexure Mechanisms.

Xia, L. (2023). Design and simulation analysis of flexible hinge structure in digital micromirror device. Proceedings - 2023 International Conference on Mechatronics, IoT and Industrial Informatics, ICMIII 2023, 196–198. https://doi.org/10.1109/ICMIII58949.2023.00043

X. Li, H. Zhu, W. Lin, W. Chen, and K. H. Low, 2021 “Structure-Controlled Variable Stiffness Robotic Joint Based on Multiple Rotary Flexure Hinges,” IEEE Transactions on Industrial Electronics vol. 68, no. 12, pp. 12452–12461, Dec. 2021, doi: 10.1109/TIE.2020.3044795.

Yang, J., Wei, H., & Li, Y. (2021). Modeling and analysis of CEAH revolute-notch type multi- A xis flexure hinges for spatial compliant mechanisms. 2021 IEEE International Conference on Manipulation, Manufacturing and Measurement on the Nanoscale, 3M-NANO 2021 - Proceedings, 222–225. https://doi.org/10.1109/3M-NANO49087.2021.9599811

Zhang, G. Q., Yu, S. C. M., & Chien, A. (2013). Investigation of the three-dimensional hinge moment characteristics generated by the ONERA-M6 wing with an aileron. Advances in Mechanical Engineering, 2013. https://doi.org/10.1155/2013/714168


Refbacks

  • There are currently no refbacks.


==============================================================================================================

Prosiding SEMNASTEK Fakultas Teknik
Universitas Muhammadiyah Jakarta
Jl. Cempaka Putih Tengah 27
Jakarta Pusat 10510
T. 021.4256024, 4244016 / F. 021.4256023

ISSN : 2407 – 1846
e-ISSN : 2460 – 8416

==============================================================================================================

Powered by Puskom-UMJ