• Journal of the KSME
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• v.32 no.6
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• pp.514-523
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• 1992

스트레인 게이지를 이용하여 변형측정을 할 때 온도변화의 영향으로 나타나는 겉보기 변형도와 게이지 상수의 변화에 대하여 설명하였고 실제 측정시 정확한 측정값을 얻기위한 온도보상 방 법에 대하여 기술하였다. 온도변화에 의한 겉보기 변형도의 값은 기계적 하중에 의한 변형도에 비하여 무시할 수 없는 큰 값을 나타내기 때문에 적절한 보상에 의하여 정확한 측정값을 얻어 내야 한다. 항공우주산업, 원자력산업 등의 분야에서 널리 응용되는 극저온 환경에서 겉보기 변 형도와 게이지 상수의 측정결과를 제시하였다. 극저온에서는 자체 온도보상된 스트레인 게이지라 할지라도 대단히 큰 온도영향을 받기 때문에 본시험에서 제시한 바와 같이 측정결과를 온도보 상하여 처리해야만 의미있는 결과를 얻을 수 있다. 본 시험에서 4차식으로 구해진 겉보기 변형 도에 대한 특성곡선과 게이지 상수에 대한 시험결과는 극저온에서 변형을 측정할 때 직접적으로 보상하여 사용될 수 있다.

• Journal of the KSME
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• v.33 no.7
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• pp.661-670
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• 1993

스트레인 게이지를 이용한 응력측정 방법 및 응력 측정시의 오차 발생의 원인에 대해서 설명하 였고 현재 많이 사용되고있는 스트레인 게이지식 로드셀의 원리 및 구조에 대해서도 설명하였다. 스트레인 게이지를 이용하여 변형도를 측정할 경우 1% 이내의 정확도를 유지하는 것이 가능하나 측정된 변형도로부터 응력을 계산할 경우 재료상수들의 부정확성으로 인하여 5% 정도의 오차가 발생할 수 있다. 스트레인 게이지를 이용한 응력 측정값은 부착위치에서의 값이므로 구조물의 최대 응력을 측정하고자 할 경우 구조물의 응력 상태를 제대로 파악하지 못하면 큰 오차가 발 생할 수 잇다. 따라서 정확한 측정을 위해서는 정확한 게이지 작업 기술과 함께 하중에 대한 대상물의 거동을 파악하는 기술 습득이 요구된다. 스트레인 게이지식 로드셀을 직접 설계 및 제작하기 위해서는 용량, 정밀도, 설치 공간, 사용조건 등을 고려하여 감지부의 형상, 감지부의 재질, 스트레인 게이지의 종류, 부착 방법, 보상회로 구성방법, 보호 케이스의 부착 여부 등을 결정하여야 하고 제작이 완료된 후 힘 표준기 등으로 교정검사를 실시하여 사용하여야만 정확한 측정을 기대할 수 있다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.17 no.9
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• pp.2205-2213
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• 1993

The characteristic test for gage factors of temperature self-compensated strain gages at cryogenic temperature is presented. By joining the international round robin test on electrical strain gages at cryogenic temperatures, the gage factors of three kinds of widely-used strain gages are obtained at the room temperature, the temperatures of liquid nitrogen and liquid helium. The calibration system which produce precise bending strain is by mechanical loading at cryogenic temperature. This paper also presents the creep characteristic of strain gages at maximum strain level.

• Journal of IKEEE
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• v.16 no.1
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• pp.34-44
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• 2012

This paper proposes a practical compensation method by using digital signal processing over the creep error which is representative in strain gauge loadcell. The signal compensation method carry out the simulation by deciding compensation constant (time constant) and coefficient measuring the loadcell output response. Then, compensation constant and coefficient are stored on the microprocessor. By using calculated on microprocessor creep error compensation values, weighting value is showed as a digital signal by reducing error values measured through output signals of loadcell. In addition, we apply error compensation method in order to have a dedicated software for loadcell electronic scale. This technique is useful because it has great influence on error rate reduction that has been produced by conventional electronic scales (0.03%). As a result our technique gives better accuracy (0.01%~0.003%) as what is given by digital electronic scale, while it has less complex operation processing.

• Journal of the Korean Society for Precision Engineering
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• v.19 no.5
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• pp.126-132
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• 2002

Misaligned shafts of the rotating machinery have caused noise, vibration. bearing failures, and stress concentration of coupling parts which decrease the efficiency and life of shaft systems. Therefore the proper shaft alignment of those system should be monitored continuously in dynamic condition. To solve these problems under dynamic condition a telemetry system is used. In this study, the condition of the least bending moment which is known by analyzing the structure and stress induced by misalignment is found. After the shaft is aligned by dial gage, a telemetry system with strain gages is installed on shaft. The relationship between bearing displacement and moment of coupling part influenced by misalignment is investigated. The moment derived from two shaft strain at the nearby coupling is measured. The bending strain is measured 5 times for average in static state as well as in dynamic state with 100∼700 rpm.

• Composites Research
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• v.31 no.5
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• pp.238-245
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• 2018

The hydrodynamic ram (HRAM) phenomenon is one of the main types of ballistic battle damages of a military aircraft and has great importance to airframe survivability design. The HRAM effect occurs due to the interaction between the fluid and structure, and damage can be investigated by measuring the pressure of the fluid and the dynamic strains on the structure. In this paper, HRAM test of a composite T-Joint was performed using a ram simulator which can generate HRAM pressure. In addition, calibration tests of PVDF sensor were performed to determine the circuit capacitance and time constant of the measurement system. The failure behavior of the composite T-Joint due to HRAM pressure was examined using the strain gauges and a PVDF sensor which were attached to the surface of the composite T-Joint.

• Journal of Sensor Science and Technology
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• v.9 no.3
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• pp.163-170
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• 2000

Optical frequency modulated fiber optic interferometric sensor was developed to sense the mechanical quantities, such as displacement, strain, force etc. It has been difficult to distinguish whether the increase of the mechanical quantities or the decrease of the quantities measured by the conventional fiber optic interferometric sensors because their signals only have a sinusoidal wave pattern related to the change of mechanical quantities. In this study, in order to measure the mechanical quantifies with the distinction of the changing direction of the quantities, the fiber of optic Michelson interferometric sensor was simply constructed by the laser light modulated with saw tooth wave pattern. The output signal of the sensor was controlled as the sinusoidal wave. The signal processing was based on the counting of the wave number of the output signal during constant time duration. The strain was determined by the cumulative value of the wave number producted by the gage factor. In order to verify the strain measurement capability of this sensor, the strain increase-decrease test was performed by universal testing machine installed with the aluminum specimen bonded with the fiber optic sensor and electrical strain gage. In the result of the test, the strain from the fiber optic sensor had a good agreement with the values from the electrical strain gage.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.22 no.2
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• pp.268-277
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• 1998

The numerical procedure for calculating non-uniform residual stress fields by using relieved strain data from incremental hole drilling method is presented. Finite element calculations are described to evaluate the relieved coefficients required for the determination of residual stresses. From the results of simulations it is found that this numerical method is well adopted to measuring non-uniform residual stress in the hole depth range of 0.8 times of the hole diameter from the surface. In order to examine the practicability of this method, the hole drilling procedure for the four point bending test is performed. This method is applied to the measurement of residual stresses in the cold-rolled steel pipe. It is shown that the magnitude of residual stress in the pipe is not negligible when compared with yield stress and the residual stress should be duly considered in designing structures with this pipes.

• The Journal of the Korea institute of electronic communication sciences
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• v.15 no.4
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• pp.671-678
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• 2020

In this paper, a wireless measurement system has been developed which can measure the deformation of a tire in real time by utilizing strain gauge sensors and Zigbee wireless communication. A strain gauge sensor is mounted inside the tire and then the strain on the tire is obtained using the DSP module. The acquired sensor values are transmitted into the vehicle by radio communication. The wireless receiver module installed inside the vehicle can monitor the deformation of the tire in real time. The deformation of the tire can be used for measuring the load applied to each tire or the speed of the tire. The load or speed applied to the tires are essential parameters for the stable control of autonomous vehicles.