• Title/Summary/Keyword: 터보압축기

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Design of Two Stage Axial Compressor of a Turbo Shaft Engine for Helicopters (헬리콥터용 터보샤프트엔진 2단 축류압축기 개량설계)

  • Kim, Jin-Han;Kim, Chun-Taek;Lee, Dae-Sung
    • 유체기계공업학회:학술대회논문집
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    • 1998.12a
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    • pp.183-190
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    • 1998
  • This paper introduces the part of efforts to develop a derivative type turbo-shaft engine from an existing baseline engine for multi-purpose helicopters targeting at 4000kg of take-off weight for 10-12 passengers. As a first step in meeting the development goal of increasing the output power to 840hp from 720hp with minimum modification, two stage axial compressor was redesigned to obtain the higher pressure ratio by removing the inlet guide vane and increasing the chord length. As a result, two stage axial compressors were designed to have the flow rate of 3.04 kg/s, the pressure ratio of 2.01 and the adiabatic efficiency of $85\%$. Its performance tests were carried out and verification of test results and redesign are under progress. Aerodynamic and structural analyses of the preliminary design are mainly described in this paper.

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TURBO TYPE AIR COMPRESSOR DESIGN FOR LOW VIBRATION LEVEL (저진동을 위한 터보형 공기압축기의 설계)

  • Kim, Myeong-Kuk;Jung, Yong-Soo;Park, No-gill
    • 유체기계공업학회:학술대회논문집
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    • 1998.12a
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    • pp.159-165
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    • 1998
  • Bearing design of turbo type geared centrifugal air compressor for low vibration level has been studied. The Transfer Matrix Method was used in this paper to analyze the air-compressor consisting of impellers, multi-stage geared rotors, and oil-film hearings. We have to consider this air-compressor as multi-geared rotating system, because characteristics of rotor-bearing system are different from conventional characteristics of non-rotating system. From the view point of Rotordynamics, the stiffness and damping coefficient of oil-film bearing in case of compressor system are more sensitive than other design parameters such as shaft length, shaft diameter and the weight of impellers, etc. Therefore, the stiffness and damping coefficients on each bearing were considered as design parameters. As the result of this study, turbo type air compressor with low vibration level can be achieved.

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Development of Air Supply System for Fuel Cell Electric Bus (연료전지 버스용 공기공급시스템 개발)

  • Kim, Woo-June;Park, Chang-Ho;Cho, Kyung-Seok;Oh, Chang-Hoon
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.06a
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    • pp.561-564
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    • 2007
  • FCEV uses electric energy which generated from the reaction between Hydrogen and Oxygen in fuel cell stack as driving force. As fossil fuels are exhausted, fuel cell is regarded as a potent substitute for next generation energy source, and thus, most of car-makers make every efforts to develop fuel cell electric vehicle (FCEV). In addition, fuel cell is also beneficial in aspect of environment, because only clean water is produced during chemical reaction process instead of harmful exhausted gas. Generally, Hydrogen is supplied from high-pressured fuel tank, and air blower (or compressor) supply Oxygen by pressurizing ambient air. Air blower which is driven by high speed motor consumes about $7{\sim}8$ % of energy generated from fuel cell stack. Therefore, the efficiency of an air blower is directly linked with the performance of FCEV. This study will present the development process of an air blower and its consisting parts respectively.

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Rotordynamic Design of a Turbo-Chiller Compressor Rotor-Bearing System (터보냉동 압축기 로터-베어링 시스템의 동특성 설계)

  • 이안성;이동환;최상규
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1998.04a
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    • pp.255-260
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    • 1998
  • A detailed rotordynamic design analysis is performed with a turbo-chiller compressor rotor-bearing system. A pinion is machined into a compressor shaft and the pinion is driven by a bull gear to a rated speed of 14,600 rpm. Utilizing a finite element method each bearing loads are calculated considering various gear loadings as well as the rotor weight itself. A Partial bearing and a 3-Lobe bearing are designed as the compressor impeller out-board bearing and in-board bearing, respectively. Finally a complex rotordynamic analysis of the compressor rotor-bearing system is carried out to evaluate the system whirl natural frequencies, stabilities, and unbalance responses.

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Development of Air Supply System for FCEV Bus (연료전지 버스용 공기공급시스템 개발)

  • Park, Chang-Ho;Cho, Kyung-Seok;Kim, Woo-June;Oh, Chang-Hoon
    • 한국신재생에너지학회:학술대회논문집
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    • 2006.11a
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    • pp.417-420
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    • 2006
  • FCEV uses electric energy generated from the reaction between Hydrogen and Oxygen in fuel cell stack as driving force. As fossil fuels are exhausted, fuel cell is regarded as a potent substitute for next generation energy source, and thus, most of car-makers make every efforts to develop fuel cell electric vehicle (FCEV). In addition, fuel cell is also beneficial in aspect of environment, because only clean water is produced during chemical reaction process instead of harmful exhausted gas. Generally, Hydrogen is supplied from high-pressured fuel tank, and air blower (or compressor) supplies Oxygen by pressurizing ambient air. Air blower which is driven by high speed motor consumes about $7{\sim}8%$ of energy generated from fuel cell stack. Therefore, the efficiency of an air blower is directly linked with the overall performance of FCEV. This study will present developing process of an air blower and its consisting parts respectively.

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Aerodynamic Design of Cathode Air Blower for Fuel Cell Electric Vehicle (연료전지 차량용 공기 블로워의 공력 설계)

  • Kim, Woo-June;Park, Chang-Ho;Jee, Yong-Jun;Cho, Kyung-Seok;Kim, Young-Dae;Park, Se-Young;Oh, Chang-Hoon
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.11a
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    • pp.197-200
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    • 2007
  • FCEV uses electric energy generated from fuel cell stack, thus all consisting parts must be re-designed to be suitable for electricity based system. Cathode air blower which supplies compressed air into fuel cell stack has similar shape of turbocharger, but a radial turbine of traditional turbocharger is removed and high speed BLDC motor is installed . Generally, maximum 10% of electric power of fuel cell stack is consumed in air blower, therefore an effective design of air blower can improve the performance of FCEV directly. This study will present an aerodynamic design process of an air blower and compare computational results with experimental data.

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The Development of a super high speed motor driving system for the direct drive type turbo compressor (직접 구동방식의 터보 압축기를 위한 초고속 전동기 구동 시스템 개발)

  • 권정혁;변지섭;최중경
    • Proceedings of the IEEK Conference
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    • 2002.06e
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    • pp.219-222
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    • 2002
  • There are screw, reciprocating type turbo compressor by structure in an air compressor which is essential equipment on the industrial spot. Recently, the application range of a turbo compressor tend to be wide gradually. And this type of compressor needs high speed rotation of impeller in structure so high ratio gearbox and conventional induction motor driving required. This mechanical system have results of increased moment of inertia and mechanical friction loss. Recent studies of modern turbo compressor have been applied to developing super high speed BLDC motor and driver which remove gearbox that make its size small and mechanical friction loss minimum. To accomodate this tendency, we tried to develope a super high speed motor drive system for 150Hp, 70,000rpm direct drive Turbo compressor using DSP(Digital Signal Processor) and SVPWM(Space Vector Modulation PWM) technique. The results of this specific application show that super high speed driver and controller could be implemented well with digital electronics.

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Computational Grid Generation for Navier-Stokes Design of Axial-Flow Compressors (축류압축기의 Navier-Stokes설계를 위한 계산격자점 생성기법 연구)

  • Chung H. T.
    • 한국전산유체공학회:학술대회논문집
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    • 1997.10a
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    • pp.38-42
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    • 1997
  • A multiblock grid generation has been applied to a Navier-Stokes design procedure of a axial-flow compressors. A multiblock structure simplifies the creation of structured H-grids about complex turbomachinery geometries and facilitate the creation of a grid in the tip flow region. The numerical algorithm adopts the combination of the algebraic and elliptic method to create the internal grids efficiently and quickly. The input module is made of the results of the preliminary design, i.e., flow-path, aerodynamic conditions along the spanwise direction, and the blade profile data. The final grids generated from each module of the system are used as the preprocessor for the performance prediction of the sectional blade, the blade-stacking process and the three-dimensional flow simulation inside the blade passage. Application to the blade design of the LP compressor was demonstrated to be very reliable and practical in support of design activities. This customized system are coupled strongly with the design procedure of the turbomachinery cascades using the Navier-Stokes technique.

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Rotordynamic Design and Analysis of the Rotor-Bearing System of a 600HP Gear Driven Turbo-Compressor (600HP급 기어구동형 터보 공기압축기 회전체계의 동역학적 설계 및 해석)

  • 최상규;김영철;권병수
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1997.10a
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    • pp.50-57
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    • 1997
  • A 600HP class high-speed gear driven 3-stage turbo-compressor (IGCC : Integrally Geared Centrifugal Compressor) driven by a 3600 rpm AC induction motor has been designed, of which low speed pinion runs at 35000 rpm and high speed pinion at 50000 rpm nominally. Due to its high speed operation, the system requires very reliable bearing selection and design as well as accurate rotordynamic analysis and prediction of its dynamic behavior to secure the operating reliability. Rotordaynamic analyses of the IGCC rotor-bearing system predicted that the low speed pinion rotor mounted on 5-pad tilting pad bearings has two critical speeds before its design speed and high speed pinion rotor only one critical speed, and estimated critical speeds of both pinion shafts are away from the continuous operating speed enough to satisfy the corresponding API requirement. The forced response analysis with API specified maximum allowable unbalances also showed that unbalance responses are small enough for smooth operation of the system.

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Feasibility Study of Pressure Letdown Energy Recovery from the Natural Gas Pressure Reduction Stations in South Korea (한국의 천연가스 도시정압기지에서 감압에너지 회수에 대한 타당성 연구)

  • Yoo, Han Bit;Hong, Seongho;Kim, Hyo
    • Journal of the Korean Institute of Gas
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    • v.19 no.3
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    • pp.9-17
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    • 2015
  • Almost all of the natural gas consumed in South Korea is compressed into very high pressure for the transportation through the underground pipelines, then reduced in pressure regulation stations before delivery to the consumer. For pressure reduction, expansion valves have been used due to the simple and effective installation, but recover none of the energy in the gas during compression. Hence, turbo-expanders are proposed instead of the valves to accomplish the same pressure letdown function and recover some of the compression energy in the form of shaft work converting into electric powers. Here we have theoretically calculated the electric powers at the pressure reduction from 68.7 bar to 23 bar (which are the average values taken at the inlet and outlet points of the expansion valve in medium-pressure regulation stations) according to the inlet conditions of temperature and flow rate. The natural gas is considered as two cases of a pure methane and the mixture of hydrocarbons with a very small amount of nitrogen, and the Peng-Robinson equation of state is employed for the calculation of required thermodynamic properties. The electric energy is recovered as much as 1596 MW(methane) and 1567 MW(mixture) based on the total supply of natural gas in 2013.