• Title/Summary/Keyword: Thrust Load

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Power Transmission Characteristics and Speed Ratio-Torque Load-Axial Force Relationship for a Metal V-Belt CVT (금속 V-벨트 CVT의 동력전달 특성과 변속비-부하토크-축력 관계)

  • 김광원;김현수
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.14 no.2
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    • pp.349-357
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    • 1990
  • Power transmission characteristics and speed ratio-torque load-axial force relationship for a metal V-belt CVT were investigated theoretically and experimentally. In the metal V-belt CVT drive, it was found that the power was transmitted by thrust force and that band tension should be greater than compression force between the metal blocks. The experimental results for the speed ratio-torque load-axial force relationship showed good agreement with those predicted using equations developed from theoretical considerations.

The Relationship between Critical Load and Frequency of Sinusolidally Non-symmetrically Tapered Member (정현상 비대칭으로 Taper진 부재의 임계하중과 고유진동수와의 관계)

  • Lee, Hyuck;Hong, Jong-Kook;Lee, Soo-Gon
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2000.10a
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    • pp.59-66
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    • 2000
  • It is generally known that the lateral frequency( ω) of the vibration of a prismatic beam-column decreases according to the rele (equation omitted) (ω/sub 0/=natural frequency). In the cases of tapered members, the determination of P/ sub/ cr/(elastic critical load) and ω/ sub 0/ are not easy. Furthermore, the relationship between the compressive load and frequency can not be determined by the conventional analytical method. The axial force-frequency relationship of sinusolidally non-symmetrically tapered members with different shapes were investigated using the finite element method. To obtain the two eigenvalues, the axial thrust was increased step by step and the corresponding frequency was calculated. The result indicated that the axial thrust of the elastic critical load ratio and the square of the frequency ratio can be approximately represented in any case by a straight line. Finally, the linear relationship is also applicable to the sinusolidally non-symmetrically tapered member.

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Bearing Design of the HDD Spindle Motors Using a Thrust Yoke (트러스트 요크를 이용한 HDD용 스핀들모터의 베어링 설계)

  • Kim, Sang-Uk;Kim, Yong-Jin;Kim, Jin-Hwan;Kim, Yong-Geun;Kim, Young-Bong
    • Proceedings of the KIEE Conference
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    • 2007.11c
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    • pp.175-178
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    • 2007
  • This paper is presented for the design of the thrust yoke for the spindle motors. HDD spindle motors are rotated by fluid dynamic bearing which consists of the shaft and the sleeve with the groove to generate the pressure. Because the thrust and journal clearances between shaft and sleeve is too small, around 8um and 2.5um, respectively, it is very difficult to design the bearing to come up to the disks to read and write the data. By the way, it is also so hard to overcome the load of the disks with only the thrust bearing. So, the paper is proposed for the trust yoke to come up to the disks considering of the force of the thrust bearing. In this paper, we proposed the thrust yoke with an unique fluid dynamic bearing in comparison with the motors without thrust yoke. Experimental results show the performance of the thrust yoke of the spindle motors for an HDD.

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Structural Design of Injector Head Part of 7ton class Thrust Chamber (7톤급 연소기 헤드부 구조설계)

  • Ryu, Chul-Sung;Lee, Keum-Oh;Heo, Seong-Chan;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.249-252
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    • 2012
  • Structural design of the injector head part of a 7ton class thrust chamber was preformed. Structural stability of an injector head part is a very important factor for a thrust chamber of a liquid rocket engine because it is loaded by high pressure of liquid oxidizer and fuel in addition to thrust load. Structural design requirements were first defined to design the injector head part of the 7ton class thrust chamber and the basic configuration was designed on the basis of the design requirements. A high strength steel that has been locally developed was applied to the injector head part of the thrust chamber. A total of twelve design configurations have been analyzed to select structurally the most stable design configuration.

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Magnetic and Thermal Analysis of a Water-cooled Permanent Magnet Linear Synchronous Motor

  • Zhang, Xinmin;Lu, Qinfen;Cheng, Chuanying;Ye, Yunyue
    • Journal of international Conference on Electrical Machines and Systems
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    • v.1 no.4
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    • pp.498-504
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    • 2012
  • The water-cooled Permanent Magnet Linear Synchronous Motor (PMLSM) has a wide range of applications due to high efficiency, high thrust force density and high acceleration. In order to ensure normal operation and maximum output, both the magnetic and thermal performance are vital to be considered. Based on ANSYS software, electromagnetic and thermal finite-element analysis (FEA) models of a 14-pole, 12-slot water-cooled PMLSM are erected adopting suitable assumptions. Firstly, the thrust force and force ripple with different current densities are calculated. Secondly, the influence of different water flow on the motor heat dissipation and force performance under different operationional conditions are investigated and optimized. Furthermore, for continuous operation, the temperature rise and thrust feature are studied under the rated load 8A, the proper temperature $120^{\circ}C$ and the limited temperature $155^{\circ}C$. Likewise, for short-time operation, the maximum duration is calculated when applied with a certain large current. Similarly, for intermittent operation, load time as well as standstill time are determined with the optimal current to achieve better thrust performance.

Analyses of Thrust Bearing in a Scroll Compressor Considering Oldham Ring (올댐링을 고려한 스크롤 압축기 스러스트 베어링의 해석)

  • Park, Sang-Shin;Lee, Seung-Ryoul
    • Tribology and Lubricants
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    • v.23 no.3
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    • pp.109-116
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    • 2007
  • A scroll compressor is on the increase in the use for the cooling and ambition machinery because of the advantages about high efficiency, low vibration and low noise. The design of thrust bearing for scroll compressor has depended on the experience. The lubrication considering the squeeze flow was applied for high side shell and low side shell of scroll thrust bearing. This work was based on governing fluid lubrication equation at the general coordinate. It shows the behavior for an orbiting scroll with direct numerical analysis using FDM. This study obtained the theoretical design value by finding load capacity and tilting angle of an orbiting scroll for thrust bearing in a scroll compressor. Especially this work performed the analysis about the design parameter. The program was written using Visual C++ to enhance user to change the design parameter easily. In particular the result value and the pressure profile were displayed as windows in every step for user to understand without difficulty.

Effect of Interconnected Boundary Between Journal and Thrust Bearings on the Performance of Self-Acting Air-Lubricated Bearings (저널-스러스트 베어링 사이의 상호 연결 경계가 동압 공기 윤활 베어링의 성능에 미치는 영향)

  • Kang, Ji-Hoon;Kim, Sung-Ki;Kim, Kyung-Woong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.27 no.4
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    • pp.608-613
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    • 2003
  • In this paper, the effect of interconnected boundary between journal and thrust bearings on the performance of self-acting air-lubricated bearings is investigated. When journal and thrust bearings have common boundary, conventional boundary condition which assumes that the boundary pressure is equal to atmosphere is no more valid. Instead, new boundary condition by mass conservation at interconnected boundary is needed. To do this, a duct model satisfying mass conservation at interconnected boundary is developed. Using this model, pressure distribution at interconnected boundary is numerically analyzed with changing the volume of interconnecting part. As a result, it is shown that load capacity of thrust bearing can be greatly increased when journal and thrust have a common boundary.

Design and Thrust Force Measurement of LSM for High-Speed Maglev Train (초고속 자기부상열차용 LSM 설계 및 추력 측정 시험)

  • Oh, Se-Young;Lee, Chang-Young;Lee, Ju
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.63 no.10
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    • pp.1473-1478
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    • 2014
  • This paper deals with design and thrust force measurement of EMS type LSM for propulsion of the high-speed maglev train. The load of maglev train is calculated, and the design equations of the LSM are presented, and the LSM which is suitable for the operation of short-distance test track is designed. In addition, the finite element analysis is performed to confirm the back-EMF and thrust force characteristics of the LSM designed model. A short length LSM prototype model is manufactured. Finally, the thrust force of the LSM is measured by the method applying dc current to the stator winding instead of three-phase ac current. And the validity of the design and analysis is verified by this measurement.

Evaluation of Structural Stability for a 75-tonf Class Thrust Chamber Mixing Head (75톤급 연소기 헤드부의 구조안정성 평가)

  • Ryu, Chul-Sung;Lee, Keum-Oh;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.515-519
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    • 2011
  • Structural tests for the mixing head of a 75tonf class thrust chamber were performed to verify structural stability. The mixing head of a thrust chamber is loaded by high pressure with regeneratively cooled fuel and cryogenic liquid oxygen(LOx) as well as it transfers thrust load generated by liquid rocket engine. Therefore structural stability of mixing head is a very important factor to work without any plastic deformation or structural failure. In this study, two mixing heads were manufactured using different welding methods, Tungsten Inert Gas(TIG) welding and Electron Beam Welding(EBW) and evaluated a structural stability. The results of structural tests showed that the mixing head assembled by EBW can withstand the applied design load without any structural failures and be structurally more stable than that of TIG welding.

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Evaluation of Dynamic Thrust Under Wind Shear in Wind Turbine Below Rated Wind Speed (정격풍속 이하에서 풍력터빈의 윈드쉬어 추력 동하중 개발)

  • Lim, Chae-Wook
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.40 no.4
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    • pp.407-414
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    • 2016
  • As wind turbines are getting larger in size with multi-MW capacity, the blades are getting longer, over 40 m, and hence the asymmetric loads produced during the rotation of the rotor blades are increasing. Some factors such as wind shear, tower shadow, and turbulence have an effect on the asymmetric loads on the blades. This paper focuses on a method of modeling the dynamic load acting on a blade because of thrust variation under wind shear. A method that uses thrust coefficient is presented. For this purpose, "wind shear coefficient of thrust variation" is defined and introduced. Further, we calculate the values of the "wind shear coefficient of thrust variation" for a 2 MW on-shore wind turbine, and analyze them for speeds below the rated wind speed. Then, we implement a dynamic model that represents the thrust variation under wind shear on a blade, using MATLAB/Simulink. It is shown that it is possible to express thrust variations on three blades under wind shear by using both thrust coefficient and "wind shear coefficient of thrust variation."