• Title/Summary/Keyword: shaft system

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A Calibration and Uncertainty Analysis on the Load Monitoring System for a Low Speed Shaft and Rotor Blade of a Wind Turbine (풍력발전기 주축 및 날개 부하 측정시스템의 보정 및 불확실성 해석)

  • Park Moo-Yeol;Yoo Neung-Soo;Nam Yoon-Su
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.30 no.5 s.248
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    • pp.560-567
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    • 2006
  • The exact load measurements for the mechanical parts of a wind turbine are important step both fur the evaluation of a specific wind turbine design and for a certification process. A common method for a mechanical load measurement is using a strain gauge sensing. Two main problems ought to be answered in order for this method to be applied to the wind turbine project. These are strain gauge calibration and non-contact signal transmission from the strain gauge output to a load monitoring system. This paper suggests reliable solutions fer these two problems. A Bluetooth, a short range wireless data communication technology, is used to solve the second problem. The first one, the strain gauge calibration methodology for a load measurement in a wind turbine application, is fully explained in this paper. Various mechanical loadings for a strain gauge calibration in a wind turbine load measurement are introduced and analyzed. Initial experimental results which are obtained from a 1 kW small size wind turbine are analyzed, and the uncertainty problem in estimating mechanical loads using a calibration matrix is fully covered in this paper.

Motion characteristics along the shape of the activating body of a floating wave energy convertor

  • Kim, Sung-Soo;Lee, Su-Bong;Lee, Soon-Sup;Kang, Dong-Hoon;Lee, Jong-Hyun
    • Journal of Advanced Marine Engineering and Technology
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    • v.40 no.8
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    • pp.704-709
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    • 2016
  • Wave energy generation systems can be divided into oscillating water chamber type, over topping device type and wave activating body type. The wave activating body type converts wave energy to kinetic energy, and the power generation amount increases as the motion of an activating body increases. In this paper, the wave energy convertor consists of a main body, which has an H-shape, and the activating body. These are connected by a bar-type bridge. By the incident wave, when the activating body moves with vertical motion this motion is consequently converted into rotational motion. The twisting moment and angular velocity at a shaft of convertor are calculated according to various conditions of the incident wave and the shape of the activating body. This can be used as a basic idea for determining the design of wave activating body type convertor.

Measurement of Fluid Film Thickness on the Valve Plate in Oil Hydraulic Axial Piston rumps (I) - Bearing Pad Effects -

  • Kim, Jong-Ki;Jung, Jae-Youn
    • Journal of Mechanical Science and Technology
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    • v.17 no.2
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    • pp.246-253
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    • 2003
  • The tribological mechanism between the valve plate and the cylinder block in oil hydraulic axial piston pumps plays an important role on high power density. In this study, the fluid film thickness between the valve plate and the cylinder block was measured with discharge pressure and rotational speed by use of a gap sensor, and a slip ring system in the operating period. To investigate the effect of the valve plate shapes, we designed two valve plates with different shapes . the first valve plate was without a bearing pad, while the second valve plate had a bearing pad. It was found that both valve plates behaved differently with respect to the fluid film thickness characteristics. The leakage flow rates and the shaft torque were also experimented in order to clarify the performance difference between the valve plate without a bearing pad and the valve plate with a bearing pad. From the results of this study, we found out that in the oil hydraulic axial piston pumps, the valve plate with a bearing pad showed better film thickness contours than the valve plate without a bearing pad.

Development of Transient Simulation Program for Smart UAV Propulsion System (스마트 무인기 추진기관의 천이 모사 프로그램 개발)

  • Lee, Chang-Ho;Ki, Ja-Young
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.6
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    • pp.63-69
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    • 2011
  • The Smart UAV must have the control characteristics of propulsion system necessary for both rotary aircraft and fixed wing aircraft though it equips turbo-shaft engine. To develop an electronic engine controller in the future, it is necessary to accumulate the experience of engine operation and data of tilt rotor aircraft. For this purpose, the computer programs which predict engine performance in the steady state and transient state can be utilized for the supplementation of flight test data. In this work, we developed a dynamic analysis program using engine performance data gathered during the flight tests. In addition the accuracy of the program was verified through comparison with flight test data and the results of steady-state performance analysis program.

A Study on Oil Path Design in the Journal Bearing of a Reciprocating Compressor (왕복동식 압축기의 저널 베어링 오일 패스 설계를 위한 연구)

  • Cho, Ihn Sung;Jung, Jae Youn
    • Journal of the Korean Society for Precision Engineering
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    • v.30 no.8
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    • pp.839-846
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    • 2013
  • Because the performance of a reciprocating compressor in refrigeration and air-conditioning systems is influenced by the lubrication characteristics of sliding components, the lubrication characteristics between the crankshaft and journal bearing have to be researched for the design and the performance improvement of reciprocating compressors. Thus, the proper supply of lubricant for a lubrication between the crankshaft and journal bearing is essential, and an oil path for lubricant supply is installed in the shaft or bearing. However, in order to guarantee the lubrication performance of the journal bearing, it is necessary to design the position of the oil path. Therefore, it is studied to find the optimum position of the oil path by the analysis of the pressure distribution in the journal bearing. The results show that the position of the oil path is significantly influenced by the pressure distribution of the oil film in the journal bearing.

A Study on Measuring Clutch Dynamic Torque (클러치 동적 토크 계측에 관한 연구)

  • Lee, Sung-Koo;Kim, Dong-Young;Hur, Man-Dae
    • Transactions of the Korean Society of Automotive Engineers
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    • v.20 no.5
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    • pp.65-70
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    • 2012
  • Torque fluctuation of engine generate gear rattle noise of transmission and many researches have been studied to decrease rattle noise by adjusting clutch damper system. So design optimization of clutch system is very important to decrease rattle noise and need knowing clutch dynamic torque at real vehicle driving condition. This makes it possible to measure clutch dynamic torque by using a small-size magnetic sensor. We install a small-size magnetic sensor on the input shaft of the transmission and measure the relative angular displacement between clutch hub and disc plate. We can obtain the clutch torque correspond to the angular displacement in the clutch torsional characteristics test. The object of this research is to measure clutch dynamic torque on real vehicle condition. Therefore, Clutch dynamic torque is very useful for investigating operating range of clutch according to engine torque and predicting the damping performance of torsional vibration on the powertrain.

An Exploratory Study on the Speed Limit of Compound Gyroplane(1) : Aerodynamic Analysis of Rotor and Airframe (복합 자이로플레인의 한계 속도에 대한 탐색연구(1) : 로터와 기체의 공력해석)

  • Shin, Byung-joon;Kim, Hak-Yoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.11
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    • pp.971-977
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    • 2015
  • A numerical analysis for the performance of compound gyroplane in forward flight was performed. TSM(Transient Simulation Method) was used to analyze the performance of autorotating rotor. CFD was conducted for the fuselages to recognize the variation of aerodynamic performance according to flight speed. At given conditions; airspeed, shaft angle and collective pitch, the quasi-static states of autorotation were determined and the variation of rotor performance was observed. Performance analysis results showed that the effect of aerodynamic characteristics in accordance with the shape of fuselage is so important that the streamlined fuselage is essential to fly fast. Forward flight speed limit is dependent on the autorotation performance of rotor.

Characteristics Analysis of a Direct-Drive AFPM Generator for 5kW Wind Turbine (직접 구동용 5kW AFPM 풍력 발전기 특성 해석)

  • Kim, Hyoung-Gil;Kim, Chul-Ho;Seo, Young-Taek;Oh, Chul-Soo
    • Proceedings of the KIEE Conference
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    • 2006.07b
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    • pp.773-774
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    • 2006
  • Nowadays, the global interests are concentrated on the preserving of the clean environment, and the diminishing of the dependence on the fossil energy, and among the possible alternative energies, the wind turbine generating system is considered to be the best suited to produce high efficiency energy, without affecting the natural environment. The permanent magnet generators were been used for the wind power generating, for long time, with continuous efforts to improve the generating efficiency. And the latest trend on it is to develop an AFPM(Axial Flux Permanent Magnet)type, which is composed in the structure of rotor and stator shaped in the disc forms, and the direction of the flux at the air gap runs in parallel to the shaft. This thesis is on the study concerning with the analysis of the characteristics of the 5 kW at 300rpm direct drive AFPM generator which is suitable for the small scale wind turbine generating system. In it, the Electro-magnetically Coreless AFPM was been analyzed, the prototype generators been made, concentrated on interpreting the characteristics of the power output, and verifying it through the theoretical study and practical tests.

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A Combined Rotary Compressor-vane Expander (일체형 로타리 압축기-베인 팽창기)

  • Kim, Hyun Jin;No, Young Jae;Kim, Yong Hee
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.3
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    • pp.12-19
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    • 2015
  • As a means of improving cycle performance of a R410A air-conditioning system, a combined structure of compressor and expander was introduced. A vane rotary type expander was designed to share a common shaft with twin type rolling piston rotary compressor in a housing. Numerical simulation on the performance of the combined compressor and expander was carried out. At ARI condition, the volumetric and total efficiencies of the designed vane expander were 69.37% and 30.23%, respectively. With the application of this expander, the compressor input was reduced by 3.91%, and the cooling capacity was increased by 3.98%. As a result, COP of the air-conditioning system was improved by 8.2%. As the pressure difference between the condenser and the evaporator becomes large, COP improvement increases unless the mass flow rate in the expander exceeds that in the compressor.

Design and Analysis of Voice Coil Actuator to Drive Fuel Pump in Automobile (자동차 연료펌프 구동용 보이스 코일 전자기 엑츄에이터의 설계 및 해석)

  • Park, Se-Myung;Kim, Jin-Ho;Bai, Cheol-Ho
    • Journal of the Korean Magnetics Society
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    • v.20 no.6
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    • pp.234-238
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    • 2010
  • Solenoid diaphragm fuel pump, which to replace mechanical fuel pump system by utilizing cam-shaft driving force, is in the spotlight for being a high efficient green car component. However, there is a drawback in power consumption as a solenoid diaphragm fuel pump only relies on solenoid for its flux needed in reciprocating motion. Therefore, this research proposes permanent magnet type VCM (Voice Coil Motor) fuel pump system to minimized power consumption. Furthermore, the study compares and analyzes power consumption and dynamic performance between the current and the former solenoid diaphragm pump by conducting finite element analysis with the commercial electromagnetic solver, MAXWELL.