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Novel forward mode AC/AC converters with high frequency link 被引量:1
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作者 李磊 陈道炼 胡育文 《Journal of Southeast University(English Edition)》 EI CAS 2003年第3期246-249,共4页
A circuit configuration and a circuit topologic family of the novel forward mode AC/AC converters with high frequency link are presented. The circuit configuration is constituted of input cycloconverter, high frequenc... A circuit configuration and a circuit topologic family of the novel forward mode AC/AC converters with high frequency link are presented. The circuit configuration is constituted of input cycloconverter, high frequency transformer, output cycloconverter, input and output filters. The circuit topologic family includes eight circuit topologies, such as full-bridge-full-wave mode, etc. The bi-polarity phase-shifted control strategy and steady principles are thoroughly investigated. The output characteristics are obtained. By using the bi-polarity phase-shifted control strategy with phase-shifted control between the output cycloconveter and the input cycloconverter, commutation overlap period of the output cycloconverter, and polarity selection of the output filtering inductance current and the input voltage, the leakage inductance energy and the output filtering inductance current are naturally commutated, and surge voltage and surge current of the cycloconverters are overcome. The converters have such advantages as simple topology, two-stage power conversions(LFAC/HFAC/LFAC), bi-directional power flow, high frequency electrical isolation, good output waveforms, and strong ability to stabilize voltage. The converters lay key technical foundation on a new-type of regulated sinusoidal AC power supplies and electronic transformers. The correction and advancement of the converters are well verified by a principle test. 展开更多
关键词 forward mode high frequency link AC/AC converter bi-polarity phase-shifted control CYCLOCONVERTER
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Dynamic flight stability of a bumblebee in forward flight 被引量:9
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作者 Yan Xiong Mao Sun 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2008年第1期25-36,共12页
The longitudinal dynamic flight stability of a bumblebee in forward flight is studied. The method of computational fluid dynamics is used to compute the aerodynamic derivatives and the techniques of eigenvalue and eig... The longitudinal dynamic flight stability of a bumblebee in forward flight is studied. The method of computational fluid dynamics is used to compute the aerodynamic derivatives and the techniques of eigenvalue and eigenvector analysis are employed for solving the equations of motion. The primary findings are as the following. The forward flight of the bumblebee is not dynamically stable due to the existence of one (or two) unstable or approximately neutrally stable natural modes of motion. At hovering to medium flight speed [flight speed Ue = (0-3.5)m s^-1; advance ratio J = 0-0.44], the flight is weakly unstable or approximately neutrally stable; at high speed (Ue = 4.5 m s^-1; J = 0.57), the flight becomes strongly unstable (initial disturbance double its value in only 3.5 wingbeats). 展开更多
关键词 Bumblebee Dynamic stability Forward flight Navier-Stokes simulation Natural modes of motion
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