• Title/Summary/Keyword: 회전 시험

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Test and evaluation of a large scale composite rotor blade for wind turbine (풍력발전용 대형 복합재 회전날개의 구조시험 및 평가에 관한 연구)

  • ;;;Y. Sugiyama
    • Journal of the Korean Society of Propulsion Engineers
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    • v.5 no.1
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    • pp.76-81
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    • 2001
  • A structural test of the wind turbine rotor blade is to evaluate the uncertainty of design due to selection of material, design concepts, production processes and so on, and their possible impacts on the structural integrity. In the full-scale static strength test, the measuring parameters are strain and displacements vs. loads, weight and the center of gravity. In order to simulate the aerodynamics load, the three-point loading method is applied. There is slight difference between the measured results and the predicted results for the reference fiber volume fraction of 60% . However, the agreement between the measured results and the predicted results with the actual fiber volume fraction of 52.5% is good. Even though a slightly non-linearity from 80% loading to 100% loading exists, a linear static solution is sufficient for the design purpose due to te small amount of non-linearity. Comparison between measured and predicted strain results at the maximum thickness positions of the blade profile for 0.236R(5.56m), 0.493R(11.59m) and 0.574R(13.43m), under 20%, 40%, 60%, 80% and 100% loadings for the upper part of the blade. The predicted values are in good agreement with the measured values.

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High Frequency Signal Analysis of LOx Pump for Liquid Rocket Engine under Cavitating Condition (캐비테이션 환경에서의 액체로켓엔진용 산화제펌프의 고주파 신호 분석)

  • Kim, Dae-Jin;Kang, Byung Yun;Choi, Chang-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.1093-1098
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    • 2017
  • High frequency signals are analyzed which are measured at the inlet / outlet pipeline and pump casing during cavitation tests of the LOx pump for the liquid rocket engine. RMS values of data are shown according to the cavitation number. RMS values of the synchronous frequency, its harmonic frequencies and frequencies of cavitation instabilities are also calculated. The pressure pulsations of the inlet and outlet pipeline are affected by cavitation instabilities. 3x component is predominant in the outlet pulsation sensor since 3x component generated at the inducer is amplified at the impeller. The cavitation instability is also found at the accelerometer signal of the casing.

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Advanced Method for an Initial Pole Position Estimation of a PMLSM (PMLSM의 개선된 초기 자극위치 추정방법)

  • Lee Jin-Woo
    • The Transactions of the Korean Institute of Power Electronics
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    • v.10 no.2
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    • pp.124-129
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    • 2005
  • This paper presents an advanced method for an initial pole position estimation of a Permanent Magnet Linear Synchronous Motor(PMLSM) that has an accurate incremental encoder for servo applications but does not have Hall sensors as a magnetic pole sensor. By appropriately using the secant method as a numerical method the proposed algorithm finds either of two zero force positions and then the correct d-axis by applying a q-axis test current. It only requires the tuned current controller and the relative position information md so it can be simply applicable to a rotary PMSM. The experimental results show the validity of the proposed method, which has an excellent performance with respect to an accurate pole position estimation under the minimal moving distance(average of about 85㎛) during the estimation process.

Design of High-Speed LSM Rotary Type Testing Machine in Consideration of Mechanical Strength (기계적 강도를 고려한 초고속 선형동기전동기 회전형 시험기 설계)

  • Seol, Hyun-Soo;Park, Eung-Seok;Lee, Ju;Park, Chan-Bae
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.64 no.5
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    • pp.824-829
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    • 2015
  • The rotary type testing machine undergoes mechanical stress as an external force is applied. In case of the rotary type testing machine, even a tiny flaw results in a fatal demage because the size of the machine is huge. Therefore, when designing the rotary type testing machine, it is necessary to secure a safety factor with the mechanical stress analysis in order to prevent the machine from being destroyed due to scattering or transformation of rotating field. This thesis proposes a LSM rotary type tesitng machine which rotates at the speed of up to 600km/h. And the mechanical stress is considered in order that the safety factor remains above 1.5 at the maximum speed. In addition, because normal force as well as thrust occurs in the machine, the normal force exerted was considered through the strength analysis. Finally, a design plan which enables to weaken the normal force affecting the rotary type testing machine is introduced and its validity is proved by the results of FEM analysis.

A Study on the Behavior of Spheroid Configuration Bobbin (회전타원체 보빈 형상의 거동에 관한 연구)

  • Kang, Seung-Hee;Ahn, Sung-Ho;Rim, One-Kwon;Kim, Hye-Ung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.5
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    • pp.717-724
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    • 2010
  • The initial trajectory of a spheroid configuration bobbin for precision guidance has been investigated by analyzing its aerodynamic load and six-degree-of-freedom motion. The effects of changes in the spheroidal head configuration, flow angle and lateral center-of-gravity offset are numerically studied using the commercial software "FLUENT". A wind tunnel test is also conducted to validate the numerical scheme and to examine effect of the Reynolds number on the flow around the bobbin. It is shown that the size of the separation bubble formed on the surface decreases significantly when the Reynolds number is varied between 110,000 and 140,000. At a zero flow angle, an oblate spheroidal head shows relatively moderate rotation while a prolate spheroidal head shows rapid rotation. The bobbin with a spherical head shape has little effect on the flow direction; however, the oblate bobbin is sensitive to the flow angle. The roll motion of the bobbin is greatly influenced by the lateral center-of-gravity offset and maximum dispersion is observed at half of the radius.

Thermal Characteristics of 600 W Brushless DC Motor under Axial Loading Condition (회전축 부하를 고려한 BLDC 모터의 열적 특성에 관한 실험 및 수치 해석적 연구)

  • Kwon, Hwabhin;Lee, Won-Sik;Kim, Gyu-Tak;Park, Heesung
    • Journal of the Korean Society for Precision Engineering
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    • v.33 no.12
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    • pp.999-1005
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    • 2016
  • A brushless direct current (BLDC) motor electronically performs rectification without brushes. It therefore does not have the typical mechanical friction contacts between the brushes and commutators. The BLDC motor has the advantages of high speed, low noise, and electronic noise reduction in addition to high durability and reliability. Therefore, it is mainly used in electric vehicles and electric equipment. However, iron loss and copper loss due to long-term use induce temperature increases in the motor, which reduces its performance and life. The temperatures of the stator and permanent magnet are predicted to be $62.3^{\circ}C$ and $32.2^{\circ}C$, respectively. This study shows the enhanced temperature distribution in a 600 W BLDC motor using unsteady and three-dimensional (3D) numerical investigations validated with experimental data.

Crack Growth Instability for Ductile Material Using the Compact Tension Specimen (컴팩트 인장 시편을 이용한 연성 재료의 불안정 균열 성장에 관한 연구)

  • 이홍서;김희송
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.5
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    • pp.928-937
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    • 1989
  • Applicability of $T_{\delta}$ proposed by Shin et al as an instability parameter for ductile material is investigated, Both general fracture test and instability fracture test are performed using compact tension specimens of structural alloy steel(SCM4), The values of ( $T_{\delta}$)$_{app}$(applied tearing modules) estimated from the real load vs. crack growth curve measured from experiments are compared with those estimated from the limit load vs. crack growth curve. The results are:(1) the $T_{\delta}$ parameter may be used as a crack instability parameter:(2) the use of ( $T_{\delta}$)$_{app}$ estimated from the load-crack growth curve, proposed in this study is reasonably justified.ified.d.

Verification and Analysis of Characteristics of Mechanical Pulsation for Combustion Stability Study in a Model Chamber (모형 연소기의 연소 불안정성 연구용 섭동 장치의 기능 검증 및 분석)

  • Min, Yong-Ho;Sohn, Chae-Hoon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.28-30
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    • 2012
  • A mechanical pulsator is manufactured for study of combustion instabilities in a model chamber with impinging-jet injectors. Artificial disturbance is generated by the device and thereby, artificial instability can be examined experimentally. A sample F(fuel)-O(dxidizer)-O-F impinging-jet injector is adopted for the test. The model chamber was designed based on the methodologies proposed in the previous work regarding geometrical dimensions and operating conditions. Pressure fluctuation data, which is obtained from the dynamic pressure transducers installed in combustion chamber, is analyzed.

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Phase Modulation effects on the imamging performance of the binocular objective having rotationally symmetrical aberrations (위상변조가 회전대칭적 수차를 갖는 쌍안경 결상력에 미치는 효과)

  • 홍경희;오병완;정창섭
    • Korean Journal of Optics and Photonics
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    • v.3 no.3
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    • pp.143-147
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    • 1992
  • 1)iscussed in this paper are the effects of phase modulation on the line spread functions (LSF) and MTFs of ;I binocular objective system. The binocular objective lens is made in Korea. It has rotationally symmetric aberrations. The LSFs and MTFs are measured experimentally. The phase modulation is carried out by applying phase retardation $\pi$ on the aperture. The area where the phase is not retarded presents a double annular type. The OTF curves of phase modulated aperture are compared with that of unmodulated aperture. The comparison shows that there is the aberration compensation effect in aberration loaded system. Therefore the performance of many optical system can be improved without any loss of light energy by properly modulating the phase on the aperture.

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Design and fabrication of Smart Skin Antenna for Phased Array Applications (위상배열 응용을 위한 스마트 스킨 안테나 설계 및 제작)

  • Son, Seong-Ho;Hwang, Woon-Bong
    • Composites Research
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    • v.20 no.3
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    • pp.25-30
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    • 2007
  • This paper describes the basic design and fabrication of smart skin antenna for phased array applications. The smart skin phased array antenna, of which radiation pattern can be electrically steerable without mechanical rotation, has to meet the both mechanical and electrical performance. The smart skin antenna is a honeycomb sandwich structure to enhance the mechanical performance such as strength, weight and so on. The example of smart skin antenna integrated with radome is designed with the resonant frequency of 5 GHz, circular polarization, 2 by 2 subarray, and a coaxial probe-fed excitation. In addition, the performance of raw microstrip patch antenna uncovered radome is investigate. The fabricated smart skin antenna shows a reasonable performance with gain of 12.2 dBi and frequency bandwidth of 6.4 %.