• KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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• 제5B권3호
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• pp.207-214
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• 2005

After more than 100 years of development, rotating electric machines are a mature industrial product. Nevertheless, improvements are still possible for specific applications, and it is likely that the major evolution will be promoted by new materials and unconventional structures. Till now, plastic materials are an infrequent choice for the electric machines structural parts, but pioneering applications, such as aeronautical components, let some technological scouting: a low-weight/high-efficiency plastic axial flux motor for a solar flying platform is presented as an example of combined new-material/new-geometry development. The basic design aspects and the prototyping choices are presented and discussed together with the first experimental results.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2009년도 제40회 하계학술대회
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• pp.708_709
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• 2009

The small wind turbines under a few kW grades has the merits of setting up with low costs by individuals, and get the energy saving effects that, it has the secured, separate markets from the big range systems, and the developing of it is continuously proceeding. The objective of this paper is to provide the design characteristics analysis of a dual-rotor, ironless, Radial Flux Permanent Magnet(RFPM) machines for small wind turbine. This thesis is aiming mainly analyzing the characteristics of the output power of the Prototype to verify through the theoretical study and tests. The results reveal an indication of the machine best suited with respect to performance criterion for a particular design requirement.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2000년도 하계학술대회 논문집 D
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• pp.2522-2524
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• 2000

In this paper, a controller design for ironless linear synchronous motor is proposed. The designed controller is mainly composed of speed and current control, which are carried out by the high-speed digital signal processor(DSP). In addition the PWM inverter is controlled by space voltage PWM method. This system is implemented using by 32-bit DSP(TMS32OC31), a high-integrated logic device(EPM940), and IPM(Intelligent Power Module) for compact and powerful system design. The experimental results show the effective performance of controller for careless linear synchronous motor.

• 한국항공우주학회지
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• 제40권9호
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• pp.789-799
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• 2012

본 연구에서는 전기 항공기에 사용하기 적합한 높은 출력밀도를 발생시키는 고온초전도 모터를 설계하고 이를 항공기에 적용하는 것이 가능한지를 확인하는 연구를 수행하였다. 설계된 모터는 이트륨 바륨 구리 산화물 판, 비스무트-2223 산화물로 이루어진 초전도 코일을 사용하고, 철심을 사용하지 않는 공기 냉각 전기저항성 전기자를 사용하였다. 고온 초전도 판과 코일 쌍을 회전축 방향으로 증가시켜, 180 마력, 2700 분당회전수의 출력을 발생시키는 세스나급 항공기에 사용하는 O-360엔진과 18000 마력, 5000 분당회전수의 B-737급 항공기에 사용하는 CFM56엔진을 대체할 수 있는 동일 출력을 발생시키도록 설계하였다. 또한 기존 엔진의 출력밀도와 고온초전도 모터의 출력밀도를 비교하여 고온초전도 모터의 항공기 적용가능성을 평가하였다.