• Title/Summary/Keyword: Pulse test

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Performance test of 100 W linear compressor

  • Ko, J.;Koh, D.Y.;Park, S.J.;Kim, H.B.;Hong, Y.J.;Yeom, H.K.
    • Progress in Superconductivity and Cryogenics
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    • v.15 no.3
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    • pp.35-39
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    • 2013
  • In this paper, we present test results of developed 100 W class linear compressor for Stirling-type pulse tube refrigerator. The fabricated linear compressor has dual-opposed configuration, free piston and moving magnet type linear motor. Power transfer, efficiency and required pressure waveform are predicted with designed and measured specifications. In experiments, room temperature test with flow impedance is conducted to evaluate performance of developed linear compressor. Flow impedance is loaded to compressor with metering valve for flow resistance, inertance tube for flow inertance and buffer volumes for flow compliance. Several operating parameters such as input voltage, current, piston displacement and pressure wave are measured for various operating frequency and fixed input current level. Behaviors of dynamics and performance of linear compressor as varying flow impedance are discussed with measured experimental results. The developed linear compressor shows 124 W of input power, 86 % of motor efficiency and 60 % of compressor efficiency at its resonant operating condition.

Development of Virtual Target Signal Generator for Verifying the Shipborne Tracking Radar Performance (함정용 추적레이더 성능 검증을 위한 모의표적신호발생장치 개발)

  • Yi, Hui-Min;Son, Jae-Hyun;Na, Young-Jin;Kim, Dong-Hawn
    • Journal of the Korea Institute of Military Science and Technology
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    • v.15 no.1
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    • pp.66-74
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    • 2012
  • The virtual target signal generator was developed to verify the shipborne tracking radar performance. It was used to DRFM(Digital RF Memory) method to generate the virtual moving targets. The target signal includes Doppler shift and RCS according to the target motion. And the signal generator can make jamming signal and clutter to test shipborne radar performance at real environmental condition. This paper described the functional diagram and the hardware configuration items to meet the test requirements for the tracking radar. And it showed the critical design points for the sub-systems. The signal generator which was developed in this paper shared the operational information of the radar with the radar command and control part. To test the frequency agility of the radar, it had the local oscillator which could do high speed frequency switching according to radar information. By communicating between the signal generator and the radar command and control part, the local oscillator of signal generator could be controlled every pulse. It reduced the instantaneous bandwidth of signal generator and minimized the spurious. So it lowered the probability of generating wrong targets.

A Study on the Radar Jamming Signal Simulator Design for the Test & Evaluation (시험평가용 레이다 재밍신호 시뮬레이터 설계 연구)

  • 최성린;이상훈;정회인
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.27 no.2B
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    • pp.160-169
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    • 2002
  • While radar operator recognizes and tracks threat targets through the scope, it is essential to overcome the jamming signal that disturbs the normal operation of the radar. Therefore, to train operator and test the EW capability of the radar, this paper proposed the jamming signal simulation algorithm and design results to generate the deception jamming(range, velocity, angle deception and multiple false targets) and noise jamming signals(spot, barrage, swept spot and cover pulse noise). And also, the radar jamming signal simulator composed of the 6 constituents is developed on basis of the proposed algorithm and digital circuit design technique and confirmed the validity of the developed simulator by means of the test results to generate the various jamming signal.

The Study on the Effect of Seatbelt anchorage points using Q6 in sled test (좌석안전띠 부착장치 위치에 따른 어린이 충돌안전성 연구)

  • Kim, Siwoo;Ryu, Hyun;Kim, Yonggil;Baek, Seonhyeon;Kim, Minwoo;Park, Jihun
    • Journal of Auto-vehicle Safety Association
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    • v.6 no.2
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    • pp.49-54
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    • 2014
  • Development in vehicle industry could increase interest in children's safety recently. However the research of children safety is not being conducted as many as that of adult's. Especially the basic study for the vehicle crash on-board children was not much. This study focused on the effect of seatbelt anchorage points to evaluate children's safety in frontal crash. The current regulation of the seatbelt anchorage points is suitable for ranged from female 5% to male 95%. The assessment of children's safety at buckle up of no used CRS(child restraint system) was performed using frontal sled tests. The frontal crash pulse in sled tests was designed to the average of about 30 KNCAP frontal crash pulses. To reduce number of experiments, DOE is used. The Q6 child dummy and standard seat in UN R 129 were used. According to the analysis of test results, children's safety has been influenced by the points of seatbelt anchorage.

Development of the Spark-gap Switch with Dual Trigger System (쌍방향 시동방식의 고속투입스위치 개발)

  • Kim, Maeng-Hyeon;Seo, Yun-Taek;Park, Seung-Jae;Park, Byeong-Rak;Go, Ui-Seok
    • The Transactions of the Korean Institute of Electrical Engineers A
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    • v.49 no.7
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    • pp.359-364
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    • 2000
  • This paper is introducing a newly developed spark-gap switch with dual trigger system, into which the current from the voltage source is injected along with the test sequence during the synthetic testing of high voltage circuit-breaker. The currently-used spark gap switch is narrow in operating range due to the use of the method of triggering energy being injected by single way. As a result, the frequent happening of misoperation has greatly reduced the test quality and test efficiency and has required the cost of maintenance excessively. In this study, accordingly, in order to basically remove these problems, another triggering system is installed to the opposite direction on the existing triggering system; attaching the same time and the same rising time of pulse wave as on the existing system, so that at a comparatively trigger gap distance from the main electrode(the gap can be operated at 60% of self-break voltage, while at 80% in the current system), the main electrode has been enabled to be closed by the development of spark gap switch with dual trigger system.

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Design and Quench Characteristics of a 6 kJ SMES Coil (6 kJ SMES 코일의 설계 및 퀜치특성)

  • Ryu, K.;Kim, H.J.;Seong, K.C.;Lee, E.Y.;Cho, J.W.;Jin, H.B.;Ryu, K.S.;Choi, B.J.
    • Proceedings of the KIEE Conference
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    • 1998.07a
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    • pp.104-106
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    • 1998
  • For the development of the 0.7 MJ small-sized superconducting magnetic energy storage (${\mu}$SMES) device, quench currents of a kA class superconducting cable were tested for various winding tensions because a dry superconducting coil is usually quenched by an abrupt heat pulse due to strand motions. The test coil similar to parameters of the optimally designed 0.7 MJ ${\mu}$SMES except a stored energy and a size was fabricated based on the test results of the kA class superconducting cable and tested. These experimental results show that the highly prestressed test coil has an excellent DC performance in spite of a dry type coil but its quench current is much degraded even at the low field ramping rate of about 0.4 T/s.

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Development of High Performance Micro Turbojet Engine (고성능 초소형 터보제트엔진 개발)

  • Paeng, Ki-Seok;Ahn, Chul-Ju;Min, Seong-Ki;Kim, Yu-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.548-551
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    • 2010
  • A 150 lbf-thrust class micro turbojet engine has been developed. The engine could be applied to power plant for small aviation vehicle such as UAV, decoy and anti-radar missile and was designed with concepts that has small size, low-cost and high performance. A prototype was manufactured and performed the ground static test and high altitude test. This paper outlines the features and layout of 150 lbf turbojet engine and also describes the design characteristics and test results of the engine and components.

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Design and development of enhanced criticality alarm system for nuclear applications

  • Srinivas Reddy, Padi;Kumar, R. Amudhu Ramesh;Mathews, M. Geo;Amarendra, G.
    • Nuclear Engineering and Technology
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    • v.50 no.5
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    • pp.690-697
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    • 2018
  • Criticality alarm systems (CASs) are mandatory in nuclear plants for prompt alarm in the event of any criticality incident. False criticality alarms are not desirable as they create a panic environment for radiation workers. The present article describes the design enhancement of the CAS at each stage and provides maximum availability, preventing false criticality alarms. The failure mode and effect analysis are carried out on each element of a CAS. Based on the analysis, additional hardware circuits are developed for early fault detection. Two different methods are developed, one method for channel loop functionality test and another method for dose alarm test using electronic transient pulse. The design enhancement made for the external systems that are integrated with a CAS includes the power supply, criticality evacuation hooter circuit, radiation data acquisition system along with selection of different soft alarm set points, and centralized electronic test facility. The CAS incorporating all improvements are assembled, installed, tested, and validated along with rigorous surveillance procedures in a nuclear plant for a period of 18,000 h.

Changes in Respiratory Function Due to Differences in Mask Blocking Grade and Effects on Cardiovascular Function during Aerobic Exercise with Mask

  • Park, Kwanghyeon;Lee, Sangyeol
    • Physical Therapy Rehabilitation Science
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    • v.10 no.3
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    • pp.289-296
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    • 2021
  • Objective: The purpose of this study was to changes in respiratory function due to differences in mask blocking grade, and effects on cardiovascular function during aerobic exercise. Design: Comparative study using paired t-test and analysis of variance measures. Methods: Male and female subjects were randomly divided into 4 groups according to mask blocking grade and measured respiratory functions before and after wearing the mask using spirometers, and their cardiovascular capabilities were measured using pulse oxygen meters and blood pressure meters before and after running for 10 minutes wearing mask. Used paired t-test, one-way ANOVA and Bonferroni post-test to compare the differences according to the mask blocking grade. Results: The experimental results verified that three groups except for the Non-mask group had a significant reduction in all values of FVC, FEV1, MVV, and PEF after wearing a mask compared to those before wearing a mask(p<0.05). Also a significant difference in cardiovascular functions was also observed after aerobic exercises wearing mask in all groups and there was a significant difference between all four groups(p<0.05). Conclusions: Lung patients with poor breathing, elderly and children with poor lung function, and professional groups who need to wear masks and take high-intensity work or aerobic movements are encouraged to take frequent breaks in advance, wear masks and social distancing at moderate and low levels.

Correlation study between propeller noise and cavitation erosion with inclined propeller model test (경사축 추진기 모형시험에서 추진기 소음과 캐비테이션 침식 상관관계 연구)

  • Seol, Hanshin;Paik, Bu-Geun
    • The Journal of the Acoustical Society of Korea
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    • v.38 no.3
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    • pp.328-333
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    • 2019
  • In this paper, to investigate the cavitation erosion phenomenon on the ship propeller, the correlation between the propeller noise and the cavitation intensity was analyzed. Cavitation erosion is closely related to cavitation collapsing intensity, which can be defined as the frequency and intensity of cavitation collapse. The pressure wave generated by cavitation collapse appears as a continuous acoustic pulse and this result is analyzed with the cavitation behavior to determine the relationship of the propeller noise to cavitation collapse intensity. This technique is applied to the propeller erosion test using the inclined shaft propeller model.