• Title/Summary/Keyword: CFRP Torsion Shaft

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Torsional Strength of CFRP Material for Application of Ship Shaft System (CFRP 소재의 선박용 축계 적용을 위한 비틀림강도 특성)

  • Kim, Min-kyu;Shin, Ick-gy;Kim, Seon Jin;Park, Dae Kyeom;Seo, Jung Kwan
    • Journal of the Society of Naval Architects of Korea
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    • v.58 no.6
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    • pp.431-439
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    • 2021
  • The Carbon Fiber Reinforced Plastic (CFRP) material is recently widely used in the composite industry with excellent rigidity and lightweight properties. A ship shaft system requires high standards of safety on torsional strength capacity. The purpose of this study is to verify the applicability of a CFRP shaft system to take the place of metal shaft systems for ships from a viewpoint of torsional strength. Selection of materials and manufacturing method are executed then two geometrically scaled CFRP shaft system models were designed and manufactured with three-layer patterns. The models were used for a series of torsion tests under single and repeated torsional loading conditions. Detailed design and manufacturing methods for a CFRP ship shaft system are documented and the torsion test results are listed in this paper. The results of this study could be useful guidelines on the development of CFRP ship shaft systems and a test method.

Development of composite torsion shaft for the aircraft structure under multiple load condition (복합하중을 받는 복합소재 중공 토크바 설계)

  • Jeong, Jong-Jae;Kim, Seung-Chul;Kim, Jeong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.6
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    • pp.484-491
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    • 2016
  • The purpose of this development is weight reduction of hollow type steel torque bar by changing the material from steel to composite. Structure analysis is executed by the finite element model generated by the structural load condition and geometric structure requirement. According to this analysis result, optimized ply sequence and wall thickness are defined. To simulate analysis result, torsion test for composite torque bar was performed. Throughout the test result, the stiffness and strength requirement of composite torque bar was verified.

A Study on the Application of Carbon Fiber Reinforced Plastics to PTO Shafts for Aircrafts (탄소섬유 강화 복합재료의 항공기용 PTO 샤프트 적용에 관한 연구)

  • Jeong, Kwang Il;Kim, Wonki;Jeong, Jae-Moon;Oh, Jaehyung;Bang, Yun Hyuk;Kim, Seong Su
    • Composites Research
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    • v.34 no.6
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    • pp.380-386
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    • 2021
  • This paper aims to improve the critical speed of power-take-off (PTO) shafts by using carbon fiber reinforced plastics (CFRPs). The PTO shaft was designed with titanium-CFRPs hybrid structure in order to compensate the low shear strength of CFRPs. Based on the requirements for PTO shafts, the dimensions of PTO shafts were determined through a parametric study. To evaluate the performance of the PTO shaft, a vibration test, a static torsion test, and a torsion durability test were performed. In the vibration test, the critical speed of PTO shafts was 20570 rpm, which was 7.5% higher than that of titanium shafts. Additionally, it was confirmed that the maximum allowable torque of the PTO shaft was 2300 N·m. Finally, under repeated load in the range of 11.3 to 113 N·m, the fatigue failure in the PTO shaft did not occur up to 106 cycles.