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A Candidate Electrical Power System for Next Generation Military Aircraft
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English
Abstract
An electrical system composed of an integral main engine electrical starter/generator and a power management and distribution system for a high performance more electric airplane is presented. The paper emphasizes the fault tolerance and high reliability requirements and discusses the necessary architecture to satisfy them. A number of critical technical issues associated with the more electric airplane, such as severe EMI environment, regenerative power, and system integration and stability are discussed.
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Citation
Said, W., Ferreira, C., and Leonard, C., "A Candidate Electrical Power System for Next Generation Military Aircraft," SAE Technical Paper 951425, 1995, https://doi.org/10.4271/951425.Also In
References
- Weimer, J.A. et. al. “Power Technology for the More Electric Aircraft,” AIAA/AHS/ASEE Aerospace Design Conference Irvine, CA Feb. 16-19 1993
- Quigley, R.E. “More Electric Aircraft,” Conference Proceedings, IEEE Applied Power Electronics Conference March 7-11 1993 906 911
- Ferreira, C.A. Richter E. “Detailed Design of a 250 KW Switched Reluctance Starter/Generator for an Aircraft Engine,” SAE 1993 Trans. 102 Journal of Aerospace 289 300
- Radun, A. Richter E. “A Detailed Power Inverter Design for a 250 KW Switched Reluctance Aircraft Engine Starter Generator,” 1993 SAE Aerospace Atlantic Conference and Exposition Dayton OH April 20-23 1993