• Title/Summary/Keyword: Weight Reduction Shaft

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Design of a Composite Propeller Shaft with the Reduced Weights and Improved NVH (경량화 및 NVH 향상을 위한 복합재료 프로펠러 축의 설계)

  • Yoon, Hyung-Seok;Kim, Cheol;Moon, Myung-Soo;Oh, Sang-Yeob
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.1
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    • pp.151-159
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    • 2003
  • The front 2 pieces of the 3-piece steel propeller shaft installed on a 8.5-ton truck were redesigned with a 1 -piece composite propeller shaft with steel yokes and spline parts to get the reduction of weight and the improvement of NVH characteristics. Based on the analysis of bending vibration, strength and cure-induced residual stresses of the composite propeller shaft, proper composite materials and stacking sequences were selected. The composite propeller shaft requires a reliable joining method between the shaft and steel end parts through a steel connector. From 3-D contact stress analyses of the laminated composite shaft with bolted Joints, the 3-row mechanical joint which satisfies the torque transmission capability has been designed. Several full-scale composite shafts were fabricated and tested to verify the design analyses. The design requirements are shown to be satisfied. With the newly designed composite shaft, the weight reduction more than 50% and improvements in NVH characteristics have been achieved.

Counter Weight Design of Multi-stage Reciprocating Air Compressors (다단 왕복동 공기압축기의 평형추 설계)

  • Kim, Young-Cheol;Kim, Byung-Ok;Shin, Hyun-Ik
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.656-661
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    • 2003
  • Modem reciprocating air compressors have tendency to a multi-stage W-type or V-type cylinder arrangement for the purpose of high outlet pressure, compactness and low vibration and noise. A valid counter weight calculation method using the complex expression is proposed for reducing the inertia forces of the compressor. Counter weight removes only 1st forward whirl component. Counter weight formulations are applied to the six various compressor structures which are (a) 1 cylinder single-throw crank shaft, (b) 2 cylinder single-throw crank shaft (c) 2 cylinder double-throw clank shaft, (d) 3 cylinder single-throw crank shaft, (e) 4 cylinder single-throw crank shaft and (f) 4 cylinder double-throw crank shaft. The improvement of performance is verified through available vibration test.

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A Study on the Optimum Design of a Motor Shaft in Electric Vehicle Using HEEDS (HEEDS를 이용한 전기자동차에서의 모터 축 최적설계에 관한 연구)

  • Kim, Bong-Hwan;Jeong, Young-Jae;Lee, Chang-Ryeol;Lee, Byung-Ho
    • Journal of the Korean Society of Mechanical Technology
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    • v.20 no.6
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    • pp.751-756
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    • 2018
  • A study on the weight reduction of a motor shaft in electric vehicle by using optimum design technique was carried out. The structural analysis of a motor shaft was performed by using ANSYS to investigate the structural safety. We also used HEEDS to find the optimal hollow shaft thickness. When the material of the hollow shaft is changed to SCM822H by using ANSYS 14.5 and HEEDS MDO, the weight could be reduced by about 53 % compared to the conventional solid one. From this study, the optimized dimensions of a hollow shaft were determined for light weight design.

Process Design of Monobloc Tube for Steering Input Shaft in Cold Drawing (일체형 스티어링 휠 튜브의 인발에 관한 연구)

  • Lee S. K.;Moon H. S.;Kim B. M.;Lee J. H.;Lee Y. S.
    • Transactions of Materials Processing
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    • v.14 no.9 s.81
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    • pp.779-784
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    • 2005
  • MTS(Monobloc Tube Shaft) has been used for the reduction in weight of shaft and increase in supply of power in the auto industry nowadays. Cold drawing process having high productivity and reduction in the cost has been regarded as the effective technology that is able to substitute for swaging process as forming MTS with constant outer diameter or hollow shaft without surface defects. The objective of this study is not only to (md out the optimal process conditions understanding the effect of process parameters on carrying out cold drawing process of SIS(Steering Input Shaft) but also to control the defects resulted from inappropriate process conditions. Therefore, the proper drawing conditions are presented using FE-Analysis and experiment in the paper.

Process design of Monobloc Tube for Steering Input Shaft in cold drawing (일체형 스티어링 휠 튜브의 인발공정 설계)

  • Moon H. J.;Lee S. G.;Lee J. H.;Lee Y. S.;Lee J. W.;Kim B. M.
    • Proceedings of the Korean Society for Technology of Plasticity Conference
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    • 2005.10a
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    • pp.431-434
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    • 2005
  • MTS(Monobloc Tube Shaft) has been used for the reduction in weight of shaft and increase in supply of power in the auto industry nowadays. Cold drawing process having high productivity and reduction in the cost has been regarded as the effective technology that is able to substitute for swaging process as forming MTS with constant outer diameter or hollow shaft without surface defects. The objective of this study is not only to find out the optimal process conditions understanding the effect of process parameters on carrying out cold drawing process of SIS(Steering Input Shaft) but also to control the defects resulted from inappropriate process conditions. Therefore, the proper drawing conditions are presented using FE-Analysis and experiment in the paper.

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A Study on Stress Analysis for Design of Composites Shaft on Small Ship by Filament Winding Process (필라멘트 와인딩 공법에 의한 소형 선박용 복합재료 축 설계를 위한 응력해석에 관한 연구)

  • 배창원;임철문;왕지석;김윤해
    • Journal of Advanced Marine Engineering and Technology
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    • v.25 no.3
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    • pp.617-622
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    • 2001
  • The purpose of this study is to design and the analyze the stress of composited shaft which is wound by filament winding method. The composites shaft has high strength and reduction in weight compared to metal shaft. The classical laminate plate theory(CLT) was used fro analysis the stress, and for structure design. In order to replace metal shaft by composites shaft, the diameter of shaft was determined to $\phi$ 40. The ration of diameter was determined to 0.4 for torsional moment with CLT. In this result of analyzing the stress, composites shaft was safe $30^{\circ}~60^{\circ}$C of winding angle, and was fractured on $90^{\circ}$.

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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.

Improvement of Fatigue Life and Vibrational Characteristics of Composite Material Propeller Shaft of Vehicle (수송기계용 복합재료 추진축의 피로수명 및 진동특성 향상에 관한 연구)

  • 공창덕;정진호;정종철;김기범
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.1
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    • pp.104-117
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    • 1999
  • The Composite materials has been used in the field of high technology industry because of high specific stiffness and high specific strength. Specially, the composite materials has been widely applied to the field of the aircraft and the transportation by the effectiveness of light weight due to low specific weight and reduction of the parts due to bonding, molding and so on. These advantages about the composite have led to study and apply in the transmission shaft for the aircraft and the drive shaft for the automobile. The composite material propeller shaft with the high vibrational stability was designed and analyzed. In order to verify the analysis, two types of experimental test which are the FFT analyzer with impact hammer and the rotational equipment were applied.

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Optimal Design for Weight Reduction of Rotorcraft Shaft System (회전익기의 축계 경량화를 위한 최적설계)

  • Kim, Jaeseung;Moon, Sanggon;Han, Jeongwoo;Lee, Geun-Ho;Kim, Min-Geun
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.35 no.4
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    • pp.243-248
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    • 2022
  • Weight optimization was performed for a rotorcraft shaft system using one-dimensional Euler-Bernoulli beam elements. Torsion, shaft support stiffness such as bearings, flange mass are all considered. To guarantee structural dynamic stability, eigenvalue analysis was performed to avoid critical speed and tooth mesh excitation form the gearbox. The weight optimization was performed by adjusting the thickness and radius while the length of the shaft was fixed, and the optimization process was divided into two stages. In the first, the weight is optimized with the torsional strength constraint. In the second, the difference between the primary mode of shaft and the critical speed is maximized so that the primary mode of the shaft can avoid the critical speed while the constraint on the torsional strength of the shaft is satisfied according to the standard for shaft system stability (AMC P 706-201, 1974). The proposed method was verified by comparing the results of the optimal design using the given one-dimensional beam elements with the stress results of the 3D finite element and the actual manufactured shaft.

Dynamic Analysis Design of Balance Shaft for Reducing Engine Inertia Force and Pitching Moment (엔진 관성력과 피칭모멘트 저감을 위한 밸런스샤프트의 동역학 설계)

  • Kim, Byeong Jun;Boo, Kwang Suk;Kim, Heung Seob
    • Journal of the Korea Convergence Society
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    • v.13 no.4
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    • pp.307-313
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    • 2022
  • The importance of engine vibration reduction is increasing as the vehicle interior noise becomes more serious due to higher output and lighten weight trends. Recently, the balance shaft attachment has been proposed as a representative method for the engine vibration reduction. The balance shaft is a device that cancels the vibrations generated in the reciprocating motion of the piston and the conrod by using an arbitrary eccentric mass, and can improve fuel efficiency and ride comfort at the same time. This paper proposes the unbalance amount and shape of the balance shaft to induce and offset the inertia force generated by the engine structure. The proposed two-shaped balance shaft was implemented as an ADAMS multi-body dynamics model, and the reduction of the inertial force in the actual behavior was confirmed through dynamic simulation.