Resonant-Converter-fed Induction Machine Part II: Hardware Prototype
暂无分享,去创建一个
[1] M. D. Kankam,et al. Potential starter/generator technology for future aerospace application , 1996 .
[2] T.A. Lipo,et al. Design and performance of a high frequency link induction motor drive operating at unity power factor , 1988, Conference Record of the 1988 IEEE Industry Applications Society Annual Meeting.
[3] Thomas A. Lipo,et al. A versatile power converter for high-frequency link systems , 1988 .
[4] Eike Richter,et al. Performance evaluation of a 250 kW switched reluctance starter generator , 1995, IAS '95. Conference Record of the 1995 IEEE Industry Applications Conference Thirtieth IAS Annual Meeting.
[5] S.R. MacMinn,et al. A very high speed switched-reluctance starter-generator for aircraft engine applications , 1989, Proceedings of the IEEE National Aerospace and Electronics Conference.
[6] M. D. Kankam,et al. Motor drive technologies for the Power-By-Wire (PBW) program: options, trends and tradeoffs. II. Power electronic converters and devices , 1995, IEEE Aerospace and Electronic Systems Magazine.
[7] S. R. Jones,et al. Performance of a high-speed switched reluctance starter/generator system using electronic position sensing , 1995, IAS '95. Conference Record of the 1995 IEEE Industry Applications Conference Thirtieth IAS Annual Meeting.
[8] S. R. Jones,et al. Design and implementation of a five-hp, switched reluctance, fuel-lube, pump motor drive for a gas turbine engine , 1995 .
[9] O. Wasynczuk,et al. Simulation of a switched reluctance, More Electric Aircraft power system using a graphical user interface , 1997, IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203).
[10] J. S. Cloyd,et al. A status of the United States Air Force's More Electric Aircraft initiative , 1997, IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203).
[11] N. M. Shah,et al. Power management and distribution system for a more-electric aircraft (MADMEL)-program status , 1996 .
[12] R. Krishnan,et al. Variable speed constant frequency power conversion with a switched reluctance machine , 1994, Proceedings of 1994 IEEE Applied Power Electronics Conference and Exposition - ASPEC'94.
[13] A.K. Wallace,et al. Experimental evaluation of a variable-speed, doubly-fed wind-power generation system , 1993, Conference Record of the 1993 IEEE Industry Applications Conference Twenty-Eighth IAS Annual Meeting.
[14] Thomas A. Lipo,et al. Power Conversion Distribution System using a Resonant High Frequency AC Link , 1986, 1986 Annual Meeting Industry Applications Society.
[15] S. R. Jones,et al. Detailed design of a 30-kW switched reluctance starter/generator system for a gas turbine engine application , 1993 .
[16] S.R. MacMinn,et al. Control of a switched-reluctance aircraft engine starter-generator over a very wide speed range , 1989, Proceedings of the 24th Intersociety Energy Conversion Engineering Conference.
[17] S. R. Jones,et al. Performance evaluation of a switched reluctance starter/generator system under constant power and capacitive type loads , 1995, Proceedings of 1995 IEEE Applied Power Electronics Conference and Exposition - APEC'95.
[18] Thomas A. Lipo,et al. Control of a polyphase induction generator/induction motor power conversion system completely isolated from the utility , 1994 .
[19] A. V. Radun. Generating with the switched reluctance motor , 1994, Proceedings of 1994 IEEE Applied Power Electronics Conference and Exposition - ASPEC'94.
[20] R.W. De Doncker,et al. Control of three phase power supplies for ultra low THD , 1991, [Proceedings] APEC '91: Sixth Annual Applied Power Electronics Conference and Exhibition.
[21] Thomas A. Lipo,et al. Study of the generator/motor operation of induction machines in a high frequency link space power system , 1987 .
[22] Thomas M. Jahns,et al. System design considerations for a high-power aerospace resonant link converter , 1993 .
[23] M. D. Kankam,et al. Motor drive technologies for the power-by-wire (PBW) program: options, trends and tradeoffs. I. Motors and controllers , 1995 .
[24] Thomas A. Lipo,et al. System and component design and test of a 10 hp, 18,000 rpm AC dynamometer utilizing a high frequency AC voltage link, part 1 , 1991 .
[25] T. L. Skvarenina,et al. Simulation and analysis of a switched reluctance generator/More Electric Aircraft power system , 1996, IECEC 96. Proceedings of the 31st Intersociety Energy Conversion Engineering Conference.
[26] T. M. Jahns,et al. A new resonant link aircraft power generating system , 1993 .
[27] E.E. Bowles,et al. Advanced power converters for More Electric Aircraft applications , 1996, IECEC 96. Proceedings of the 31st Intersociety Energy Conversion Engineering Conference.
[28] Jayant G. Vaidya,et al. Electrical machines technology for aerospace power generators , 1991 .
[29] Thomas A. Lipo,et al. Field oriented control of an induction machine in a high frequency link power system , 1988, PESC '88 Record., 19th Annual IEEE Power Electronics Specialists Conference.
[30] G. L. Fronista,et al. An electromechanical actuator for a transport aircraft spoiler surface , 1997, IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203).
[31] Thomas A. Lipo,et al. Performance testing of a high frequency link converter for space station power distribution system , 1989, Proceedings of the 24th Intersociety Energy Conversion Engineering Conference.
[32] A.V. Radun,et al. High power density switched reluctance motor drive for aerospace applications , 1989, Conference Record of the IEEE Industry Applications Society Annual Meeting,.
[33] A. V. Radun,et al. Two-channel switched reluctance starter/generator results , 1998 .