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Volumn , Issue , 2010, Pages

Failure mechanisms and design considerations for fault tolerant aerospace drives

Author keywords

Actuators; Aerospace industry; Aircraft power systems; Bearings (mechanical); Fault tolerance; Safety; Synchronization; Variable speed drives

Indexed keywords

AIRCRAFT POWER SYSTEMS; BEARINGS (MECHANICAL); COMMERCIAL AIRCRAFT; DESIGN CONSIDERATIONS; DESIGN ISSUES; FAILURE CONDITIONS; FAILURE MECHANISM; FAULT TOLERANT DRIVE; FAULT-TOLERANT; SAFETY; VARIABLE SPEED;

EID: 78649595860     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICELMACH.2010.5607981     Document Type: Conference Paper
Times cited : (12)

References (21)
  • 2
    • 0027649071 scopus 로고
    • Boeing 777 High Lift Control System
    • Aug
    • Rea, J. "Boeing 777 High Lift Control System", IEEE Aerospace and Electronic Systems Magazine, Aug 1993, Volume: 8, Issue: 8, pp.15-21.
    • (1993) IEEE Aerospace and Electronic Systems Magazine , vol.8 , Issue.8 , pp. 15-21
    • Rea, J.1
  • 16
    • 43649088032 scopus 로고    scopus 로고
    • Testing of a 250-kilowatt fault-tolerant permanent magnet power generation system for aeroengines
    • DOI 10.2514/1.32158
    • Wang J, Sun Z, Ede J.D, Jewell G.W, Cullen J.J.A, Mitcham A.J, "Testing of a 250-kilowatt fault-tolerant permanent magnet power generation system for large aeroengines", AIAA Journal of Propulsion and Power, Vol. 24(2), 2008, pp.330-335. (Pubitemid 351683642)
    • (2008) Journal of Propulsion and Power , vol.24 , Issue.2 , pp. 330-335
    • Sun, Z.1    Ede, J.D.2    Wang, J.3    Jewell, G.W.4    Cullen, J.J.A.5    Mitcham, A.J.6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.