Determination of protection system requirements for dc unmanned aerial vehicle electrical power networks for enhanced capability and survivability

A growing number of designs of future unmanned aerial vehicle (UAV) applications utilise DC for the primary power distribution method. Such systems typically employ large numbers of power electronic converters as interfaces for novel loads and generators. The characteristic behaviour of these systems under electrical fault conditions, and in particular their natural response, can produce particularly demanding protection requirements. Although a number of protection methods for multi-terminal DC networks have been proposed in the literature, these are not universally applicable and will not meet the specific protection challenges associated with the aerospace domain. Through extensive analysis, this study seeks to determine the operating requirements of protection systems for compact DC networks proposed for future UAV applications, with particular emphasis on dealing with the issues of capacitive discharge in these compact networks. The capability of existing multi-terminal DC network protection methods and technologies are then assessed against these criteria in order to determine their suitability for UAV applications. Recommendations for best protection practice are proposed and key inhibiting research challenges are discussed.

[1]  M.E. Baran,et al.  Overcurrent Protection on Voltage-Source-Converter-Based Multiterminal DC Distribution Systems , 2007, IEEE Transactions on Power Delivery.

[2]  Barrie Mecrow,et al.  A fault tolerant electric drive for an aircraft nose wheel steering actuator , 2010 .

[3]  W. M. Davidson,et al.  A-C and D-C short-circuit tests on aircraft cable , 1944, Electrical Engineering.

[4]  Rebecca Todd,et al.  Ultra-compact Intelligent Electrical Networks , 2008 .

[5]  F. Cohen,et al.  The architecture of the electric power system of the International Space Station and its application as a platform for power technology development , 2000, Collection of Technical Papers. 35th Intersociety Energy Conversion Engineering Conference and Exhibit (IECEC) (Cat. No.00CH37022).

[6]  Mark Sumner,et al.  Fault detection for the aircraft distribution systems using impedance estimation , 2008 .

[7]  J.-M. Meyer,et al.  A DC hybrid circuit breaker with ultra-fast contact opening and integrated gate-commutated thyristors (IGCTs) , 2006, IEEE Transactions on Power Delivery.

[8]  Graeme Burt,et al.  Transient analysis of the more-electric engine electrical power distribution network , 2008 .

[9]  Nigel Schofield,et al.  Generator Operation of a Switched Reluctance Starter/Generator at Extended Speeds , 2009, IEEE Transactions on Vehicular Technology.

[10]  A. Apostolov IEC 61850 based bus protection — Principles and benefits , 2009, 2009 IEEE Power & Energy Society General Meeting.

[11]  A.R. Bendre,et al.  IGCTs vs. IGBTs for circuit breakers in advanced ship electrical systems , 2009, 2009 IEEE Electric Ship Technologies Symposium.

[12]  Alex Q. Huang,et al.  The emitter turn-off thyristor-based DC circuit breaker , 2002, 2002 IEEE Power Engineering Society Winter Meeting. Conference Proceedings (Cat. No.02CH37309).

[13]  R. W. Ashton,et al.  Selection and stability issues associated with a navy shipboard DC zonal electric distribution system , 2000 .

[14]  Allan N. Greenwood,et al.  Generalized Damping Curves and Their Use in Solving Power-Switching Transients , 1963 .

[15]  A. Greenwood,et al.  Electrical transients in power systems , 1971 .

[16]  A. Sannino,et al.  Protection of Low-Voltage DC Microgrids , 2009, IEEE Transactions on Power Delivery.

[17]  C. Tenning,et al.  Design of the Boeing 777 electric system , 1992, Proceedings of the IEEE 1992 National Aerospace and Electronics Conference@m_NAECON 1992.

[18]  Mehrdad Ehsani,et al.  Aircraft power systems: technology, state of the art, and future trends , 2000 .

[19]  D. Howe,et al.  Stability assessment of distributed DC power systems for ‘more-electric’ aircraft , 2008 .

[20]  M. Steurer,et al.  A Novel Hybrid Current-Limiting Circuit Breaker for Medium Voltage: Principle and Test Results , 2002, IEEE Power Engineering Review.

[21]  Graeme Burt,et al.  Evaluation of Overvoltage Protection Requirements for a DC UAV Electrical Network , 2008 .

[22]  J. R. McDonald,et al.  Power System Protection of All Electric Marine Systems , 2008 .

[23]  J.A. Ortega,et al.  Moving towards a more electric aircraft , 2007, IEEE Aerospace and Electronic Systems Magazine.

[24]  Boon-Teck Ooi,et al.  DC overvoltage control during loss of converter in multiterminal voltage-source converter-based HVDC (M-VSC-HVDC) , 2003 .

[25]  Peter E. Sutherland DC short-circuit analysis for systems with static sources , 1998, 1998 IEEE Industrial and Commercial Power Systems Technical Conference. Conference Record. Papers Presented at the 1998 Annual Meeting (Cat. No.98CH36202).

[26]  A.R. Bendre,et al.  Circuit Breaker Technologies for Advanced Ship Power Systems , 2007, 2007 IEEE Electric Ship Technologies Symposium.

[27]  A. Siu Discrimination of miniature circuit breakers in a telecommunication DC power system , 1997, Proceedings of Power and Energy Systems in Converging Markets.

[28]  Jin Yang,et al.  Multiterminal DC Wind Farm Collection Grid Internal Fault Analysis and Protection Design , 2010, IEEE Transactions on Power Delivery.

[29]  G.M. Burt,et al.  Mitigation against overvoltages on a DC marine electrical system , 2009, 2009 IEEE Electric Ship Technologies Symposium.

[30]  Robert M. Cuzner,et al.  The Status of DC Micro-Grid Protection , 2008, 2008 IEEE Industry Applications Society Annual Meeting.

[31]  L. Andrade,et al.  Design of Boeing 777 electric system , 1992, IEEE Aerospace and Electronic Systems Magazine.

[32]  H. Ayakawa,et al.  New protection method for HVDC lines including cables , 1995 .

[33]  Boon-Teck Ooi,et al.  Locating and Isolating DC Faults in Multi-Terminal DC Systems , 2007, IEEE Transactions on Power Delivery.