• Title/Summary/Keyword: Pilot Test

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Gasification melting characteristics of Automobile shredder residue in 5t/d shaft pilot plant (5톤/일 shaft형 pilot plant에서 자동차 폐차 잔재의 가스화 용융 특성)

  • Roh, SeonAh;Kim, WooHyun;Yun, JinHan;Hong, ByeongKwon
    • 한국신재생에너지학회:학술대회논문집
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    • 2010.11a
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    • pp.160-160
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    • 2010
  • ELVs (End-of-Vehicles) in Korea incrasease continusely because of increase of used car. Automobile Shredder Residue (ASR) is final product of ELVs (End-of-Vehicles) after recycling. Automobile Shredder Residue are composed of light and heavy fluffs and soil/dust. In this study, 5 ton/day pilot plant of shaft type has been designed and constructed and 15 times of test run were performed. For the stable operation, operation conditions such as the amount of fed ASR and cokes, air flow and temperature in the gasification melting system have been changed and the composition of the produced gas such as $H_2$, CO and $CH_4$ and air pollution compound including dioxin discharged from the stack have been analyzed.

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Design of Course Keeping Controller for RIB-type USV Using a Pilot's Steering Pattern (조종자 입력패턴을 활용한 RIB형 무인선의 침로제어기 설계)

  • Yun, Kun-Hang;Yeo, Dong-Jin;Yoon, Hyeon-Kyu
    • Journal of the Society of Naval Architects of Korea
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    • v.47 no.3
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    • pp.462-468
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    • 2010
  • A new course keeping controller for RIB(Rigid Inflatable Boat)-type USV(Unmanned Surface Vehicle) is developed using pilot's steering pattern. A pilot's simple steering pattern is found out from various course change tests. It is used to course keeping algorithm, suitable for large course change more than 60 degrees. To validate the course keeping controller, sea trial tests are conducted. From sea trial test, new course keeping controller shows good performance with less overshoot, maximum roll angle less than $20^{\circ}$, which makes it possible that fast course changes without slip motion of USV.

Development of Linear DC Motor Pilot Model for High Thrust (고추력용 리니어직류모터 Pilot 모델 개발)

  • 정재한;서경일;박재완;박재한
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.1002-1005
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    • 2000
  • The goal of this study is to develop a linear DC motor with high thrust, speed and stiffness for machine tool. In the first phase of this study, We has made a pilot model and measuring system. Using the measuring system, We could finished the performance test of the pilot model, which continuous thrust is 1, 391N. Experimental values agree with the theoretical results well. In a certain sense, We are expecting the realization of linear motor with continuous thrust of 6, 000 to 7, 000N next time.

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Development of a Rice Circulating Concurrent-flow Dryer (I) - Performance Test of Pilot Scale Dryer - (순환식 병류형 곡물건조기 개발 (I) -시작기의 성능시험 -)

  • Han J.W.;Keum D.H.;Han J.G.;Kim H.;Hong S.J.
    • Journal of Biosystems Engineering
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    • v.31 no.4 s.117
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    • pp.349-354
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    • 2006
  • This study was performed to evaluate the performances for a concurrent flow rice dryer of pilot scale with devices for circulating rice. The pilot scale dryer with the capacity of 700 kg was developed to obtain design informations for the development of actual scale dryer of holding capacity of 10 tons. Three drying tests were conducted at two temperature levels of $100^{\circ}C\;and\;120^{\circ}C$, and two air flow rates levels of $28.5cmm/m^2\;and\;57.1cmm/m^2$. Drying conditions for Test-1, Test-2 and Test-3 were $100^{\circ}C\;-28.5cmm/m^2,\;120^{\circ}C-28.5cmm/m^2\;and\;120^{\circ}-57.1cmm/m^2}$ respectively. Drying rates were 0.73%(w.b./h) for Test-1, 0.90%(w.b./h) for Test-2 and 1.46%(w.b./h) for Test-3. The crack ratios of brown rice after drying ranged from 2.4% to 8.4%, and increased with the increase of drying rate and airflow rate. The energy consumptions were from 6,225 kJ/kg to 6,993 kJ/kg which was higher than that of conventional cross-flow rice circulating type dryer used in Korea. This results were due to the lower ambient air temperatures of $4.5^{\circ}C\;to\;13.4^{\circ}C$ during drying tests.

A Study on Operational Benefits of ADS-B through experimental Flight Test in Tae-An Airport (비행시험을 통한 ADS-B 운영상의 효과에 관한 연구)

  • Hong, Gyo-Young;Kim, Do-Hyun;Oh, Kyung-Ryoon
    • Journal of Advanced Navigation Technology
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    • v.11 no.2
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    • pp.137-145
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    • 2007
  • The flight test of ADS-B is to demonstrate operational benefits to air traffic controllers and pilots when other aircraft data including the aiming altitude is displayed on CDTI. Additionally, This ADS-B study is to provide first operational experience of ADS-B in ATCS environment of South Korea and provide practical information to ATCS before deployment of ADS-B in South Korea is considered. Participation in the flight test has been limited to 2 Aircraft of H University which are installed ADS-B equipment and the ground station has installed in Tae-An airport. This test have been experimented according to the pre-arranged flight procedures of Tae-An airport. As a result of the test, it has shown that the number of radio transmitting and the time of radio occupied between controller and pilot are remarkably reduced. Besides, as both pilot and air traffic controller are able to see the traffic information in the vicinity of the aircraft, the test has demonstrated that it is possible for ADS-B not only to decline the controller's workload, but also to enhance pilot situational awareness in the near future.

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Ground Test and Evaluation of a Flight Control Systemfor Unmanned Aerial Vehicles

  • Suk, Jin-Young
    • International Journal of Aeronautical and Space Sciences
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    • v.5 no.1
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    • pp.57-63
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    • 2004
  • UAV(Unmanned Aerial Vehicle) has become one of the most popularmilitary/commercial aerial robots in the new millennium. In spite of all theadvantages that UAVs inherently have, it is not an easv job to develop a UAVbecause it requires very systematic and complete approaches in full developmentenvelop. The ground test and evaluation phase has the utmost importance in thesense that a well-developed system can be best verified on the ground. In addition,many of the aircraft crashes in the flight tests were resulted from the incompletedevelopment procedure. In this research, a verification procedure of the wholeairbome integrated system was conducted including the flight management system.An airbome flight control computer(FCC) senses the extemal environment from thepehpheral devices and sends the control signal to the actuating system using theassigned control logic and flight test strategy. A ground test station controls themission during the test while the downlink data are transferred from the flightmanagement computer using the serial communication interface. The pilot controlbox also applies additional manual actuating commands. The whole system wastested/verified on the wind-tunnel system, which gave a good pitch controlperformance with a preUspecified flight test procedure. The ground test systemguarantees the performance of fundamental functions of airbome electronic systemfor the future flight tests.

Development of the First LNG Bunkering Barge System in Korea (한국 최초의 LNG벙커링 바지시스템 개발)

  • Jung, Dong-Ho;Oh, Seung-Hoon;Jung, Jae-Hwan;Hwang, Sung-Chul;Sung, Hong-Gun;Lee, Jae-Ik;Kim, Eun-Seok
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2018.11a
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    • pp.162-163
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    • 2018
  • This study introduces the R&D project of development of the 1st LNG bunkering barge in Korea. The Design and pilot test of Barge-To-Ship 500cbm LNG bunkering barge system for coastal trading LNG-fueled ship is proposed. The following technologies will be developed from the project ; Basic/Detail design and pilot test of LNG Bunkering barge system, Basic/Detail design and pilot test of LNG bunkering process system considering LNG loading/unloading, Basic/Detail design and pilot test of 500cbm LNG tank in type-C, Evaluation of bunkering performance according to conditions (environment, SIMOPs) by numerical simulation, Performance evaluation of bunkering barge, towed barge and Barge-To-Ship motion considering ocean environment load, and scenario in Barge-To-Ship LNG bunkering. This project will contribute expansion to LNG-fueled ship industry and pave the way to establish LNG bunkering hub port.

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Performance Evaluation of Frame Synchronization Using Pilot Patterns in W-CDMA System (W-CDMA 시스템의 파일럿 패턴을 이용한 프레임 동기 성능 분석)

  • Song Young-Joon;Kim Han-Mook
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.17 no.3 s.106
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    • pp.272-279
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    • 2006
  • In this paper, we evaluate the performance of frame synchronization words of pilot bit patterns which are used for the channel estimation and frame synchronization confirmation in W-CDMA(Wide band Code Division Multiple Access) system. W-CDMA system also uses compressed mode to make measurements from another frequency without a full dual receiver terminal. It is confirmed by using computer simulation that the proposed frame synchronization words also maintain the frame synchronization property in the compressed mode by using the complementary mapping relationship of preferred pair ROC(Receiver Operating Characteristic) curves with probability of detection and false alarm are used to analized the performance of the proposed frame synchronization words by using the various detection metrics such as LLRT(Log Likelyhood Ratio Test), GLRT(Generalied Likelyhood Ratio Test), soft and hard correlation tests in AWGN and Rayleigh fading channels. It is expected that the research results fer the performance of pilot bit patterns of this paper can be useful reference for the design and implementation of frame synchronization in 3rd generation W-CDMA system.

EIRP Measurements of WCDMA Base Station Using Pilot Channel in Line-of-Sight Environments (가시선 환경에서 Pilot 채널을 이용한 WCDMA 기지국의 EIRP 측정)

  • Jang, Byung-Jun;Moon, Sung-Won;Lim, Jae-Bong
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.22 no.5
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    • pp.545-551
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    • 2011
  • In this paper, we described a measurement method of an EIRP(Effective Isotropic Radiated Power) of a WCDMA base station using a pilot channel in line-of-sight environments. Especially we measured it in real base station environments in order to apply this method to domestic base station inspection test. Estimated EIRP results from measured value is -2 dB lower than theoretical values, which is calculated by the data of transmit antenna. The deviation of -2 dB is verified as a polarization mismatch between the base station antenna and a receiver antenna, and it can be calibrated. Therefore, we verified that our measurement method could be an effective tool to measure an EIRP in WCDMA base station inspection test.

Test Run of Pilot Plant for Recycling of the Leached Residue in the Processing of Waste Aluminum Dross (알루미늄 폐드로스 침출잔사 처리 파일롯트 플랜트 시운전 결과)

  • 박형규;이후인
    • Resources Recycling
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    • v.13 no.3
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    • pp.50-57
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    • 2004
  • Waste aluminum dross is a major waste in the aluminum scrap smelters and its components are mostly alumina and remained metallic aluminum. In the process to extract the remained aluminum from the waste dross by leaching with sodium hydroxide solution, residue is generated and its main component is alumina. This residue could be recycled into ceramic materials such as alumina castable refractories by going through a series of treatments such as washing, drying and roasting. In this study, a pilot plant was constructed and tested to demonstrate the developed technology. One thousand tons of waste aluminum dross could be processed, and about seven hundred tons of ceramic materials produced in the demonstration line. From the test run of the pilot plant, although it was confirmed that the developed technology could be applied to commercialization, several technical improvements were found to be necessary for reducing impurities such as Na, Fe and for reforming drying equipment.