• 제목/요약/키워드: Compressor speed control

검색결과 118건 처리시간 0.02초

중형항공기용 터보팬 엔진의 성능최적화를 위한 LQR 제어기 설계 (II) (A LQR Controller Design for Performance Optimization of Medium Scale Commercial Aircraft Turbofan Engine (II))

  • 공창덕;기자영
    • 한국추진공학회지
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    • 제2권3호
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    • pp.99-106
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    • 1998
  • 현재 국내에서 개발되어왔던 중형항공기 후보엔진인 터보팬 엔진의 성능해석과 성능최적화를 위한 제어기법을 연구하였다. 선행된 연구에서 동적모사 및 실시간 선형모사를 수행한 결과 지상 정지조건 하에서 70% 엔진로터 회전수에서 100% 엔진로터 회전수로 급상승하는 경우 고압터어빈 입구온도에서 오버슈트가 발생하여 제한온도인 3105 $^{\cire}R$ 을 넘어감을 확인할 수 있었다 또한 압축기의 서지여유도 협소하여 엔진에 손상을 가져올 수 있다. 이에 본 연구에서는 보다 빠른 가속성능과 함께 엔진 성능의 최적화를 위해 LQR 제어기를 설계하였다. 제어기의 설계를 위해서는 선형모델을 구성해야하며 엔진의 비선형 거동에 보다 근접한 선형화를 위해서는 실시간 선형모사가 요구된다. 선형모델에 필요한 행렬은 자동점에 %의 섭동을 주어 5% 간격으로 구하였으며, 최소자승법을 이용하여 저압 엔진로터 회전수의 함수로 보간하는 방법으로 실시간 선형모사를 수행하였다. 제어변수는 연료유량의 증가속도와 압축기 블리드 공기유량으로 하였으며, 제어 결과 고압 터빈입구온도의 오버슈트를 제거하였으며 최대 압축기 서지여유도 0.55 이하로 확보였다. 비연료소모율도 0.353에서 0.43으로 안정됨을 확인할 수 있었다.

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터보냉동기의 소음원 파악 및 저소음화에 대한 연구 (A Study on the Identification of Noise Source and the Noise Reduction Method of a Turbo Chiller)

  • 전완호
    • 한국유체기계학회 논문집
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    • 제7권3호
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    • pp.7-13
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    • 2004
  • In this paper, we identify the noise source and the path of a chiller. This chiller is newly developed for R-l34a refrigerant and 250 RT cooling capacity. The measured overall SPL of the developed turbo-chiller is about 100 dBA. Due to the high rotating speed of the centrifugal impeller, the nun noise source of the chiller is the blade passing frequency and its higher harmonics of the centrifugal impeller. This generated soundpropagates through the duct, and then transmits and radiates to the outer field. From the experiment, it is found that the high frequency noise is mostlytransmitted and radiated through the elbow duct, but the low frequency noise is transmitted and vadiated through the condenser wall. Therefore applying the absorbing material is an effective way of reducing the high and low frequency noise simultaneously. Measurement results show that the application of the sound absorbing material to the elbow duct reduced the overall sound pressure level by 4 dB compared to the 9 dBA reduction for the case of full enclosure. In order to control the generated noise, a dissipativetype silencer is also designed and tested. The silencer reduced the radiated noise about 7.5 dBA.

A Study on Winter Season Measurement Results to cope with Dynamic Pricing for the VRF System

  • Kim, Hwan-yong;Kim, Min-seok;Lee, Je-hyeon;Song, Young-hak
    • Architectural research
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    • 제17권3호
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    • pp.109-115
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    • 2015
  • The dynamic pricing of electricity, where the electricity rate increases in a time zone with a high demand for electricity is typically applied to a building whose power reception capacity is greater than a certain size. This includes the time of use(TOU) electricity pricing in Korea which can induce the effect of reducing the power demand of a building. Meanwhile, a VRF (Variable Refrigerant Flow) system that uses electricity is regarded as one of the typical heating and cooling systems along with central air conditioning (central HVAC) for its easy operation and application to the building. Thus, to reduce power energy and operating costs of a building in which the TOU and VRF systems are applied simultaneously, we suggested a control for changing the indoor temperature setting within the thermal comfort range or limiting the rotational speed of an inverter compressor. In this study, to describe the features of the above-mentioned control and verify its effects, we evaluated the results obtained from the analysis of its operation data. Through the actual measurements in winter operations for 73 days since mid- December 2014, we confirmed a reduction of 10.9% in power energy consumption and 12.2% in operating costs by the new control. Also, a reduction of 13.3% in power energy consumption was identified through a regression analysis.

Steady-State/Transient Performance Simulation of the Propulsion System for the Canard Rotor Wing UAV during Flight Mode Transition

  • Kong, Changduk;Kang, Myoungcheol;Ki, Jayoung
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.513-520
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    • 2004
  • A steady-state/transient performance simulation model was newly developed for the propulsion system of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) during flight mode transition. The CRW type UAV has a new concept RPV (Remotely Piloted Vehicle) which can fly at two flight modes such as the take-off/landing and low speed forward flight mode using the rotary wing driven by engine bypass exhaust gas and the high speed forward flight mode using the stopped wing and main engine thrust. The propulsion system of the CRW type UAV consists of the main engine system and the duct system. The flight vehicle may generally select a proper type and specific engine with acceptable thrust level to meet the flight mission in the propulsion system design phase. In this study, a turbojet engine with one spool was selected by decision of the vehicle system designer, and the duct system is composed of main duct, rotor duct, master valve, rotor tip-jet nozzles, and variable area main nozzle. In order to establish the safe flight mode transition region of the propulsion system, steady-state and transient performance simulation should be needed. Using this simulation model, the optimal fuel flow schedules were obtained to keep the proper surge margin and the turbine inlet temperature limitation through steady-state and transient performance estimation. Furthermore, these analysis results will be used to the control optimization of the propulsion system, later. In the transient performance model, ICV (Inter-Component Volume) model was used. The performance analysis using the developed models was performed at various flight conditions and fuel flow schedules, and these results could set the safe flight mode transition region to satisfy the turbine inlet temperature overshoot limitation as well as the compressor surge margin. Because the engine performance simulation results without the duct system were well agreed with the engine manufacturer's data and the analysis results using a commercial program, it was confirmed that the validity of the proposed performance model was verified. However, the propulsion system performance model including the duct system will be compared with experimental measuring data, later.

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대평판 글라스 이송용 공기 부상 이송장치의 개발 (Development of the Air Floating Conveyor System for the Large Glass Sheet)

  • 이태걸;유진식;정효재;김종형;김준현
    • 한국생산제조학회지
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    • 제22권4호
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    • pp.635-642
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    • 2013
  • We have prepared a DEMO conveyor device for conveying a large 8G class glass sheet using ahorizontal air-cushion system. This device consists of the body frame and the driving frame that are combined to realize a frame for conveying glass without any contact.The driving frame comprises an air flotation table (bed), drive roller supported at both ends, and ASU. Part of the ASU serves to control the airflow as the chamber consists of a porous pad and fan. Fiber filters replace the porous pad and axial fans serve as an air compressor. In addition, to determine the appropriate glass levitation from the air table, this study examined the design specifications of the applied filter (discharge speed of HEPA and ULPA filters, and flow rate) as well as the height of the and the proper supporting roller height (14mm). Then, after adjusting the position of the ASU and the number of ASUs required to configure the UNIT air floating C/V, we analyzed the height and flatness of the glass and derived the appropriate layout (1140-mm distance between ASUs).

냉매 내 공기혼입에 따른 에어컨 시스템의 냉각성능 저하 (Cooling Performance Deficiency of Air Conditioning System According to Air Quantity Included in Refrigerant)

  • 문성원;민영봉;정태상
    • Journal of Biosystems Engineering
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    • 제34권6호
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    • pp.470-475
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    • 2009
  • This study was performed to present the diagnosis basis of cooling performance deficiency according to air quantity included in refrigerant of air-conditioner by detecting the temperatures and pressures of refrigerant pipeline. The car air-conditioner of SONATA III (Hyundai motor Co., Korea) was tested by maximum cooling condition at 1500 rpm of engine speed in the room with controlled air condition at $33\sim35^{\circ}C$ and 55~57% RH. Measured variables were temperature differences between inlet and outlet pipe surface of the compressor (Tcom), condenser (Tcon), receive dryer (Trec) and evaporator (Teva), and high pressure (HP) and low pressure (LP) in the refrigerant pipeline, and temperature difference (Tcoo) between inlet and outlet air of the cooling vent of evaporator. Control variables were the refrigerant charging weight and the vacuum degree in the refrigerant pipeline before charging refrigerant. From the test, it was represented that the measuring values of (Tcom), LP and (Tcoo) were enabled to make the diagnosis of cooling performance deficiency according to quantity included in refrigerant of air-conditioner. The ranges of Tcom, LP and Tcoo to make the diagnosis of cooling performance deficiency were respectively less than $55^{\circ}C$, more than 166.7 kPa-g(1.7 kgf/$cm^2$) and less than $13.7^{\circ}C$. In the case of using only external sensors and the condition under the normal performances of air conditioner, it was considered that the ranges of LP and Tcoo to make the diagnosis of cooling performance deficiency were respectively more than 166.7 Pa and less than $12^{\circ}C$.

설비공학 분야의 최근 연구 동향 : 2016년 학회지 논문에 대한 종합적 고찰 (Recent Progress in Air-Conditioning and Refrigeration Research : A Review of Papers Published in the Korean Journal of Air-Conditioning and Refrigeration Engineering in 2016)

  • 이대영;김사량;김현정;김동선;박준석;임병찬
    • 설비공학논문집
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    • 제29권6호
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    • pp.327-340
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    • 2017
  • This article reviews the papers published in the Korean Journal of Air-Conditioning and Refrigeration Engineering during 2016. It is intended to understand the status of current research in the areas of heating, cooling, ventilation, sanitation, and indoor environments of buildings and plant facilities. Conclusions are as follows. (1) The research works on the thermal and fluid engineering have been reviewed as groups of flow, heat and mass transfer, the reduction of pollutant exhaust gas, cooling and heating, the renewable energy system and the flow around buildings. CFD schemes were used more for all research areas. (2) Research works on heat transfer area have been reviewed in the categories of heat transfer characteristics, pool boiling and condensing heat transfer and industrial heat exchangers. Researches on heat transfer characteristics included the results of the long-term performance variation of the plate-type enthalpy exchange element made of paper, design optimization of an extruded-type cooling structure for reducing the weight of LED street lights, and hot plate welding of thermoplastic elastomer packing. In the area of pool boiling and condensing, the heat transfer characteristics of a finned-tube heat exchanger in a PCM (phase change material) thermal energy storage system, influence of flow boiling heat transfer on fouling phenomenon in nanofluids, and PCM at the simultaneous charging and discharging condition were studied. In the area of industrial heat exchangers, one-dimensional flow network model and porous-media model, and R245fa in a plate-shell heat exchanger were studied. (3) Various studies were published in the categories of refrigeration cycle, alternative refrigeration/energy system, system control. In the refrigeration cycle category, subjects include mobile cold storage heat exchanger, compressor reliability, indirect refrigeration system with $CO_2$ as secondary fluid, heat pump for fuel-cell vehicle, heat recovery from hybrid drier and heat exchangers with two-port and flat tubes. In the alternative refrigeration/energy system category, subjects include membrane module for dehumidification refrigeration, desiccant-assisted low-temperature drying, regenerative evaporative cooler and ejector-assisted multi-stage evaporation. In the system control category, subjects include multi-refrigeration system control, emergency cooling of data center and variable-speed compressor control. (4) In building mechanical system research fields, fifteenth studies were reported for achieving effective design of the mechanical systems, and also for maximizing the energy efficiency of buildings. The topics of the studies included energy performance, HVAC system, ventilation, renewable energies, etc. Proposed designs, performance tests using numerical methods and experiments provide useful information and key data which could be help for improving the energy efficiency of the buildings. (5) The field of architectural environment was mostly focused on indoor environment and building energy. The main researches of indoor environment were related to the analyses of indoor thermal environments controlled by portable cooler, the effects of outdoor wind pressure in airflow at high-rise buildings, window air tightness related to the filling piece shapes, stack effect in core type's office building and the development of a movable drawer-type light shelf with adjustable depth of the reflector. The subjects of building energy were worked on the energy consumption analysis in office building, the prediction of exit air temperature of horizontal geothermal heat exchanger, LS-SVM based modeling of hot water supply load for district heating system, the energy saving effect of ERV system using night purge control method and the effect of strengthened insulation level to the building heating and cooling load.

항공전자기기용 냉각시스템의 대체냉매 적용에 관한 실험적 연구 (Experimental Study of Adoption of Alternative Refrigerant for Avionic Equipment Cooling System)

  • 강훈;정종호;정민우;지용남;유용선;최희주;변영만;김영진;오광윤;김용찬
    • 대한기계학회논문집B
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    • 제37권5호
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    • pp.431-439
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    • 2013
  • 항공전자기기의 정상적인 동작을 위해서는 내부에서 발생되는 열부하를 적절히 처리해야 하기 때문에 냉각시스템의 장착이 요구된다. 본 연구에서는 항공용 냉각시스템으로의 대체냉매 적용 가능성을 분석하기 위하여 증기압축 사이클 방식의 밀폐 공기순환 냉각시스템을 설계 제작하였다. 대체냉매로 가장 유력한 R236fa를 냉각시스템에 적용하여 냉매 충전량, 팽창밸브 개도, 그리고 압축기 운전회전수 변화에 따른 성능특성을 실험적으로 고찰하였다. 또한, 실험결과를 기존 냉매인 R124의 실험결과와 비교 평가를 수행하여, R236fa가 대체냉매로서 적용 가능함을 확인하였다. 최종적으로 R236fa를 적용한 냉각시스템의 효율 향상을 위한 설계 개선안을 제시하였다.