• Proceedings of the Korean Society of Precision Engineering Conference
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• 1991.11a
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• pp.75-79
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• 1991

자동차 엔진, 점프, 모우터 둥과 같은 회전동력장치의 일률이나 효율을 측정하거나 혹은, 회전동력장치를 과부하 없이 운용하고자 할 때 토오크센서를 이용한다. 이 때 사용되는 토오크센서는 대부분 strain gage와 slip ring을 이용하고 있는 데, 이러한 종류의 센서들은 감지된 토오크를 회전하는 축으로부터 외부로 그 신호를 전달하기 위해서 slip ring 이나 magnetic coupler와 같은 중간의 신호 전달장치 ( signal transmitter )를 설치하여야 한다.(중략)

• The Korean Journal of Rheology
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• v.11 no.1
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• pp.57-65
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• 1999

In order to measure yield stress of PIM feedstocks simply and effectively, a yield stress measuring technique was developed by a vane method. The vane method had an advantage that there was no wall-slip, while it had a drawback that it could not measure viscosity change at various shear rates. A Newtonian fluid was tested for the appropriateness of the measuring technique. The end effect of a vane was checked to produce an acceptable error. The torque peak has been considered to be developed at yielding of non-Newtonian fluids with yield stress. However, it was influenced very much by control system of the instrument so that the torque value at the stable region was taken to calculate yield stress. Torque at zero rotational speed was obtained by extrapolating the torque values at various speeds to remove the effect of the rotational drag. As general verification, yield stress of feedstocks made of Tungsten carbide powder with wax-based binder was measured at different temperatures and various powder concentrations.

• 전기의세계
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• v.25 no.2
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• pp.40-45
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• 1976

유도전동기의 고주파진동토오크의 산정법에 대하여는 Morrill, Chang, Puchstein Kimball 및 Veinott씨 등에 의한 불평형공간자속분포의 대칭좌표법 또는 2회전자계법해석으로 많은 연구가 거듭되어 기계정수가 고주파토오크에 미치는 영향의 관계를 풀이하고 있다. 또한 Jordan과 Lax씨에 의하여 편심 및 기계적진동에 따른 전자력파의 분포력 mode수 및 그 주파수를 개발함으로서 소음방지대책에 많은 진전을 보았다. 소음진동측정방법으로는 원래 진동측정이 정밀한 장치에 의존하여야 하며 그 방법 또한 어려운 점이 많아 method of 1-point measurement of electromagnetic-force waves로 처리되어 왔으나 요즈음에는 anechoic chamber와 같은 장치에서의 특별한 조작에 의하여 method of resultant measurement of accoustic noise powers에 의하여 보다 합리적인 소음측정 및 해석이 가능하게 되었다.

• Proceedings of the KSME Conference
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• 2003.04a
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• pp.2018-2023
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• 2003

An experiment is conducted for measuring the performance of an air tool, which is operated at 100,000 RPM at the unloaded state with the low torque. An experimental apparatus is developed as the power absorption type dynamometer. Inlet static pressure, flow rate, RPM and force are measured simultaneously. Torque, output power and specific output power are obtained. Those experimental results are compared with the experimental results obtained on a commercial dynamometer. However, no commercial dynamometers are available for measuring the torque above 30,000RPM. In order to use the commercial dynamometer, a reduction gear is applied to the shaft of dynamometer. Torque and power obtained on the commercial dynamometer show 50% lower than those obtained on a power absorption type dynamometer, because the inertia force is added to the air tool rotor for the braking system. Moreover, the starting RPM on the commercial dynamometer is less than 40,000RPM. From the compared results, they show that the power absorption type dynamometer should be applied for measuring the performance of an air tool operating at low torque and high RPM.

• The korean journal of orthodontics
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• v.37 no.4
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• pp.293-304
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• 2007

The purpose of this study was to estimate the fracture resistance of commercially available ceramic brackets to torsional force exerted from arch wires and to evaluate the characteristics of bracket fracture. Methods: Lingual root torque was applied to maxillary central incisor brackets with 0.022-inch slots by means of a $022\;{\times}\;028-inch$ stainless steel arch wire. A custom designed apparatus that attached to an Instron was used to test seven types of ceramic brackets (n = 15). The torque value and torque angle at fracture were measured. In order to evaluate the characteristics of failure, fracture sites and the failure patterns of brackets were examined with a Scanning Electron Microscope. Results: Crystal structure and manufacturing process of ceramic brackets had a significant effect on fracture resistance. Monocrystalline alumina (Inspire) brackets showed significantly greater resistance to torsional force than polycrystalline alumina brackets except InVu. There was no significant difference in fracture resistance during arch wire torsional force between ceramic brackets with metal slots and those without metal slots (p > 0.05). All Clarity brackets partially fractured only at the incisal slot base and the others broke at various locations. Conclusion: The fracture resistance of all the ceramic brackets during arch wire torsion appears to be adequate for clinical use.

• Proceedings of the KIEE Conference
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• 2005.07b
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• pp.1771-1774
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• 2005

가변속 직접 구동형 영구자석 농기발전기와 감속기(38:1)를 2 MW의 유도전동기축에 직결로 결합하여 유도전동기의 속도제어 통하여 발전기 단자전압을 인버터의 출력으로 계통에 전력을 전송하는 시험을 전기연구원에서 수행하였다. 인버터 출력 60 Hz의 상용전원으로 계통과 연계되는 동기발전기의 정격출력은 800 kW이며, 손실분을 제외한 인버터의 정격출력은 750 kW이다. 동기발전기는 속도 9 rpm에서 발전을 시작하여 정격속도인 25 rpm에서 정상적인 출력을 내도록 되어있다. 시험은 유도전동기 속도를 가변으로 각각의 속도에서 발전기 단자전압과 토오크를 측정하고, 정격속도에서 토오크 제어를 통한 최대전력을 측정하였다. 본 논문에서는 시험결과 분석 및 계통사고, 발전기 단락사고와 같은 극한상황에서 전력변환 장치를 보호하기 위한 보호시스템에 대한 국내 규정에 준하는 시험에 대한 결과를 보이고자 한다.

• 한국신재생에너지학회:학술대회논문집
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• 2009.06a
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• pp.546-549
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• 2009

풍력을 이용한 풍력발전기의 효율적 전력변환 시스템을 연구개발하기 위해서는 바람의 특성을 실내에서 정확히 구현할 수 있는 모의시험장치인 시뮬레이터가 요구된다. 모의시험장치는 바람을 받아 회전하는 블레이드 대신 풍속 값을 입력하여 전동기가 발전기에 토오크(torque)를 공급하게 된다. 모의시험장치를 설계하고 구현에 있어서 중요한 요소는 블라인드의 관성시정수와 축소모델인 5.83kW 모델 발전기 설계제작 그리고 고효율의 전력변환장치 설계 및 인버터 특성 알고리즘 구현이다. 본 논문은 2MW Gearless형 풍력발전기 KBP-2000M을 400:1 축소하여 제작한 모의실험장치에 최고의 출력 파워를 얻도록 Pitch Control 알고리즘을 적용한 측정 결과를 소개한다.

• Aerospace Engineering and Technology
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• v.4 no.2
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• pp.50-59
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• 2005

This paper described performance test of 1st prototype "Tail-Fan" system. KARI(Korea Aerospace Research Institute) developed "Tail-Fan" system as a kind of helicopter anti-torque system(ATS) and designed ATS performance test-rig for Tail-Fan system performance test. For Tail-Fan system performance tests, firstly, test-rig operation tests were carried out for verification of design specifications. And natural frequencies of fan blade and test-rig were measured respectively. To find the operation rotating speed for performance tests, vibration tests using accelerometers on tail gear box(TGB) were carried out. Through the fanplot and vibration test results, rotational speed for Tail-Fan performance test to avoid a resonance were found and performance tests were carried out in flight conditions. We analyzed test data by non-dimensionalization. Through this results, 1st prototype "Tail-Fan" system was satisfied with design requirements.

• Journal of the Korean Magnetics Society
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• v.1 no.1
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• pp.30-36
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• 1991

A measurement system for magnetic anisotropy was built. The torque acting on the disc or sperical samples placed in uniform magnetic field was detected with a capacitive transducer which is connected with a transformer ratio-arm bridge. The output of the bridge was amplified with a lock-in amplifier. The cubic anisotropy constant for (100) of 3% Si-Fe was $3.3{\times}10^{4}\;J/m^{3}$. The calibration for the system was carried out with the shape anisotropy of a thin Ni wire.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.3
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• pp.10-16
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• 2004

In this paper the aeroacoustic characteristics of a helicopter main rotor system is measured by using a pair of scaled rotor blades. A low noise rotor test jig is developed for noise measurement and the rotational speed, thrust and torque are measured simultaneously in order to match the aerodynamic conditions with the full scale rotor. The accuracy of the force measurement device was checked through a calibration procedure. The measured thurst and torque with a 1.2m rotor are compared to the results of analytical prediction and showed that the thrust data at various rotational speed followed the prediction relatively well, but the torque data considered less accurate. It is also found that the background noise level of the test rig is sufficiently low, and the measured noise level from the rotor can be scaled with rotor tip speed. However, the Mach number dependancy and the directivity changes depend on the noise source characteristics.