• Title/Summary/Keyword: 유성기어 열

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An Investigation on the Characteristics of Gear Trains of Wind turbines (풍력발전기용 기어트레인의 특성에 관한 연구)

  • Park, No-Gill;Lee, Hyoung-Woo
    • Journal of Advanced Marine Engineering and Technology
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    • v.34 no.6
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    • pp.806-815
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    • 2010
  • Gear trains are combined with the planetary gear units and helical gear units. It is known that the combination type is decisive to the system performances of the transmissions. In this paper, within the commonly used range of the design requirements for medium and large scaled (1~8 MW) wind turbines, the transmission characteristics of the typical layouts of the gear train are investigated. According to the international standard by ANSI/AGMA/AWEA 6006-A03, the gear boxes are basically designed and compared with respect to the system lifes of 99% reliability, total weight, the power densities, overall diameter/length and the maximum stresses of the gear teeth. With these comparison works, the characteristics of the layouts of gear trains are discussed.

Study on Design Characteristics of Gearbox for Wind Turbine Considering the Type of Gear Train (기어열의 형태를 고려한 중대형 풍력 발전기용 기어박스의 설계 특성 연구)

  • Lee, Ki-Hun;Park, Jae-Hee;Lee, Geun-Ho;Nam, Yong-Yun
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.06a
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    • pp.387-390
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    • 2007
  • The gearbox for wind turbine have been increased the size by the wind turbine is needed to produce bigger power. The optimal sizing for gearbox is demanded because of limited space on the nacelle. The volume and weight for the gearbox are influenced especially for size of it. Therefore, the purpose of this study investigates the design characteristics considering types of gear train structure for optimizing the volume and weight of the gearbox.

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Optimum Shape Design of Gearbox Housing for 5MW Wind Turbines (5MW급 풍력발전기용 기어박스 하우징의 형상 최적설계)

  • Jeong, Ki-Yong;Lee, Dae-Yeon;Choi, Eun-Ho;Cho, Jin-Rea;Lim, O-Kaung
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.25 no.3
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    • pp.237-243
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    • 2012
  • The thickness optimization of the gearbox housing for 5MW wind turbine is carried out with the help of the efficient structure analysis model and the approximation model of objective function. Wind turbine gearbox is a complex structural system composed of a number of gear trains, shafts, bearing and gearbox housing, requiring a tremendous number of elements for the structural analysis and design. In this paper, an effective analysis and design model considering the tooth stiffness of helical gears is proposed. It enables to significantly reduce the total element number and the analysis time. Through the numerical optimization of housing thickness making use of the effective gearbox model and the approximate model of objective function, the total weight of the gearbox housing is minimized. It has been observed from the numerical experiment that the approximation model is reliable and the optimization result is acceptable and verified analysis.

The Critical Speed Analysis of the Differential Planetary Gear Train of a Concrete Mixer Truck Mixer Reducer (콘크리트 믹서 트럭용 믹서 감속기의 차동 유성 기어 트레인에 대한 위험속도 해석)

  • Bae, Myung Ho;Bae, Tae Yeol;Kim, Dang Ju
    • Journal of Drive and Control
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    • v.14 no.1
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    • pp.1-7
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    • 2017
  • The power train of a concrete truck mixer reducer includes differential planetary gears to get a large reduction ratio for operating the mixer drum in a compact structure. These differential planetary gears are a very important part of the mixer reducer where strength problems are the main concern. Gear bending stress, gear compressive stress and scoring failure are the main concerns. Many failures in differential planetary gears are due to the insufficient gear strength and resonance problems caused by major excitation forces such as gear mating failure in the transmission. In the present study, where the excitation frequencies are the gear tooth passing frequencies of the mating gears, a Campbell diagram is used to calculate differential planetary gear critical speeds. Mode shapes and natural frequencies of the differential planetary gears are calculated by CATIA V5. These are used to predict gear resonance failures by comparing the working speed range with the critical speeds due to the gear transmission errors of the differential planetary gears.

Performance Evaluation of a Washing Machine of Unconstrained Transmission (불구속 동력전달 세탁기의 성능 평가)

  • Kim, Yeong Man;Choi, Woo Chun
    • Journal of the Korean Society for Precision Engineering
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    • v.31 no.4
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    • pp.343-351
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    • 2014
  • Washing machines designed to clean laundry have been more widely used at home as they reduce household labor and boost the quality of life. Technological advances and better standards of life increase demand for laundry washing performance. Energy efficiency regulations and consumer demand for the larger trend, washing machine makers should be done in performance studies to reduce power, and water consumption and the load on power transmission devices. In this study, performance of a fully automatic washing machine with unconstrained transmission is analyzed through experiment and CFD simulation. It is found that the interaction between laundry and transmission change the washing behavior and affect washing performance with regard to the degree of freedom. The results obtained in this study can be used in developing new washing machine transmissions and make them more robust.

Release Mechanism for small satellite using micro DC motor (소형 위성용 소형직류모터를 이용한 분리장치)

  • Tak, Won-Jun;Jo, Jae-Uk;Lee, Min-Soo;Kim, Byung-Kyu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.8
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    • pp.767-773
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    • 2010
  • This paper describes development of a non-explosive separation device which can be equipped on small satellites. The spur geared micro DC motor, which has high reliability and advantage of price, is adopted as an actuator. The proposed separation device has resettability and it does not need extra jig to reload. In addition, the simple structure makes it easy to fabricate and assemble. To verify the performance of the proposed device, the response time tests, maximum preload tests and maximum shock level tests were performed. Also, through the vibration tests and thermal vacuum tests, feasibility of the proposed separation device was shown in launching and space environments. Therefore, we expect that the proposed separation device can replace the imported separation devices in near future.