• 한국소음진동공학회논문집
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• 제20권10호
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• pp.953-959
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• 2010

This paper deals with the process to identify the exciting forces generated from a rotary compressor. The equation of motion of a rigid compressor supported by several mounts was derived with 6 degree of freedom. The mass moment of inertia of compressor and the stiffness of rubber mounts were also identified by experiments. The exciting force at the center of mass of the compressor were estimated from the acceleration data measured at compressor shell. The piping system connected to the compressor was modeled. The acceleration of a pipe was predicted numerically by using the predicted exciting force. The numerical results showed good agreement with experimental results, which validated the identified exciting force.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2006년도 하계학술발표대회 논문집
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• pp.1095-1100
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• 2006

An experimental study has been performed to investigate the correlation on compressor discharge temperature of system A/C in heating mode. Indoor and outdoor temperatures, the heating capacity, compressor discharge temperature and loading time are measured by the psychrometric calorimeter. The system is controlled by applying the scroll compressor, which Is operated by PWM valve and loading duty. With increasing outdoor temperature, the heating capacity increases, With increasing indoor temperature, it decreases. Also, with increasing loading duty the heating capacity increases. According to the increase in outdoor temperature and loading duty, compressor discharge temperature increases. From these experimental data, the correlation on compressor discharge temperature is proposed. It is expressed as a function of indoor temperature, outdoor temperature, and loading duty. The correlation obtained from the present study is agreed with the experimental data within $2^{\circ}C$.

• 한국유체기계학회 논문집
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• 제14권6호
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• pp.96-101
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• 2011

Korea Aerospace Research Institute is performing 3 stage transonic axial compressor development program. This paper introduces design step of the compressor, the performance test results and its analysis. In the fore part of the paper, aerodynamic process of the 3 stage axial compressor is presented. To satisfy both of the mass flow and pressure rise, the compressor should rotate at a high rotational speed. Therefore the transonic flow field forms in the rotor stages and it is designed with a relatively high pressure rise per stage to satisfy its design target. The compressor stage consists of 3 stages, and the bulk pressure ratio is 2.5. The first stage is burdened with the highest pressure ratio and less pressure rises occur in the following stages. Also it is designed that tip Mach number of the first rotor row does not exceed 1.3, while the maximum relative Mach number in the rotor stage is between 1.3~1.4 to increase the compressor flow coefficient. The final design has been confirmed by iterating three dimensional CFD calculations to verify design target and some design intentions. In the latter part of the paper, its performance test processes and results are presented. The performance test result shows that the overall compressor performance targets; pressure ratio and efficiency are well achieved. The stator static pressure distributions show that the blade loading is gradually increasing from the downstream of the compressor.

• 대한기계학회논문집B
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• 제37권1호
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• pp.59-65
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• 2013

본 논문은 차량용 에어컨 압축기가 실차 연비에 미치는 영향에 대하여 실험적으로 연구한 것으로, 본 연구의 목적은 연비에 주요한 영향 인자인 압축기의 토출 용량별 구동 토크에 의한 실차 연비 기여도를 분석하는 것이다. 연비에 직접적인 영향을 주는 압축기의 부하를 측정하기 위하여 압축기 클러치에 직접 부착하는 토크 센서를 개발하였으며, 실차 평가전 벤치 토크 미터와의 비교 평가를 통하여 토크 센서의 신뢰성을 검증하였다. 토크 센서가 부착된 압축기를 장착한 차량을 환경 풍동에서 연비 측정을 할 수 있도록 장치를 구성한 상태에서 연비 평가를 수행하였다. 압축기의 토출 용량에 따른 구동 토크는 연비에 직접적인 영향을 주며, 동일 사양 압축기에서 토출 용량이 약 11% 커질 때 연비는 약 2~3% 악화됨을 알 수 있었다.

• 한국산학기술학회논문지
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• 제13권5호
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• pp.1976-1982
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• 2012

압축기는 다양한 유체기계에 널리 사용되고 있으며, 특히 압축기의 성능은 냉동공조 시스템의 성능계수에 직접적인 영향을 미치므로 압축기의 효율을 높이기 위한 노력이 계속되어 왔다. 용도에 맞게 다양한 종류의 압축기가 개발되었고, 그 중 스크롤 압축기는 그 크기에 비하여 압축 성능이 우수하여 여러 분야에서 선호하는 압축기이다. 스크롤 압축기의 개발을 위하여 실험적인 연구는 많이 수행되어 온 반면, 개발 목적에 맞게 압축기를 해석할 수 있는 모델은 많지 않은 실정이다. 따라서 본 연구에서는 스크롤 압축기를 기하학적으로 모델링하여 해석할 수 있는 모델을 1-D 상용 프로그램인 AMESim을 이용하여 개발하였으며, 실험 데이터를 이용하여 모델의 신뢰성을 검증하였다. 본 연구 결과는 추후 스크롤 압축기를 개발하는 과정에서 압축기의 성능을 예상하고 최적화 할 수 있는 방법을 제공할 것으로 기대된다.

• 한국전자통신학회논문지
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• 제17권1호
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• pp.173-180
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• 2022

근사 컴퓨팅은 효율적인 하드웨어 컴퓨팅 시스템을 설계하기 위한 유망한 방법이다. 근사 곱셈은 고성능, 저전력 컴퓨팅을 위한 근사 계산 방식에 사용되는 핵심적인 연산이다. 근사 4-2 compressor는 근사 곱셈을 위한 효율적인 하드웨어 회로를 구현할 수 있다. 본 논문에서는 저면적, 저전력 특성을 갖는 근사 곱셈기를 제안하였다. 근사 곱셈기 구조는 정확한 영역, 근사 영역, 상수 수정 영역의 세 영역으로 나누어진다. 새로운 4:2 근사 compressor를 사용하여 근사 영역의 부분 곱 축소를 단순화하고, 간단한 오류 수정 방식을 사용하여 근사로 인한 오류를 보상한다. 상수 수정 영역은 오차를 줄이기 위해 확률 분석을 통한 상수를 사용하였다. 8×8 곱셈기에 대한 실험 결과, 제안한 근사 곱셈기는 기존의 4-2 compressor 기반의 근사 곱셈기보다 적은 면적을 요구하면서 적은 전력을 소비함을 보였다.

• 설비공학논문집
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• 제24권5호
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• pp.385-390
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• 2012

This paper discusses the applicability of a compact rolling piston refrigeration compressor to portable refrigerators. The capacity of this compressor is 1 cc. Using a 12 V BLDC motor, the compressor is driven from 2500 rpm to 6000 rpm. The height of the compression module and motor is approximately 56 mm, and their weight is approximately 374 g. We confirmed the effective operation of the compressor components by evaluating their compression and cooling performance.

• Smart Structures and Systems
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• 제25권2호
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• pp.255-264
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• 2020

This paper deals with a defect classification technique that considers the structural characteristics of a refrigerant compressor. First, the pressure pulsation of the refrigerant flowing in the suction pipe of a normal compressor was measured at the same time as the acceleration of the shell surface, and then the transfer function between the two signals was estimated. Next, the frequency-weighted acceleration signals of the defect classification target compressors were generated using the estimated transfer function. The estimation of the variance of the transfer function is presented to formulate the frequency-weighted acceleration signals. The estimated frequency-weighted accelerations were applied to defect classification using frequency-domain features. Experiments were performed using commercial compressors to verify the technique. The results confirmed that it is possible to perform an effective defect classification of the refrigerant compressor by the shell surface acceleration of the compressor. The proposed method could make it possible to improve the total inspection performance for compressors in a mass-production line.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.237-243
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• 2002

A centrifugal compressor of 50HP for reverse brayton cryocooler using neon as a coolent has been developed. It has relatively low total-to-total pressure ratio but mass flow rate is very small and the voting gas, neon, has greater specific heat ratio than air. It was essential to have very high rotational speed of 100,000 RPM. The efficiency of compressor has great effects on overall system and the COP of cryocooler. To meet the design requirement of the compressor efficiency and to minimized the required rotational speed, highly efficiency impeller having low specific speed was designed. To maintain the overall system efficient high, gas bearing of bump type and high speed permanent magnet synchronus motor was developed and adopted. In this paper, design and performance prediction results of the compressor impeller is presented.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.264-270
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• 2002

This paper presents roughness effects on flow characteristics and efficiency of multi-stage axial compressor using numerical simulation. which is carried out with a commercially available software, CFX-TASCflow. In this paper, the third of four stages of GE low pressure compressor is considered including me stator and rue rotor. Mixing-plane approach is adopted to model the interface between the stator and the rotor: it is appropriate for steady state simulation. First, a flat plate simulation was performed to validate how exact the numerical simulation predicts the roughness effect for smooth and rough walls. Then GE compressor model was calculated about at each roughness height. Concluding, very small roughness height largely affects the performance of compressor and the increasing rate of loss decrease as roughness height increase.