Power systems and requirements for integration of smart structures into aircraft

Journal of Intelligent Material Systems and Structures

Volumn 15, Issue 4, 2004, Pages 305-315

  Lockyer, Allen J ^a   Martin, Christopher A ^c   Lindner, Douglas K ^d   Walia, Paramjit S ^a   Carpenter, Bernie F ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b LOCKHEED MARTIN   (United States)

^c INSTITUTE FOR DEFENSE ANALYSES   (United States)

^d VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

Aircraft electrical power system; Piezoelectric actuation; Shape memory alloy; Smart actuators; Smart materials; Smart wing; Vehicle electromagnetic effects (EME)

Indexed keywords

ACOUSTIC NOISE; ACTUATORS; AIRCRAFT; AIRCRAFT ENGINES; AIRFRAMES; COMPRESSED AIR MOTORS; ELECTRIC GENERATORS; ELECTROMAGNETISM; FLUTTER (AERODYNAMICS); OPTIMIZATION; PIEZOELECTRIC MATERIALS; STANDBY POWER SYSTEMS; STRAIN;

AIRCRAFT ELECTRICAL POWER SYSTEMS; PIEZOELECTRIC ACTUATION; SMART ACTUATORS; SMART WINGS; VEHICLE ELECTROMAGNETIC EFFECTS (EME);

INTELLIGENT STRUCTURES;

EID: 3042518842     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1177/1045389X04042800     Document Type: Review

References (9)

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2. Kudva, J.N., et al. March 2002. "Overview of the DARPA/AFRL/NASA Smart Materials and Structures - Smart Wing Program," SPIE Symposium on Smart Structures and Materials, San Diego, CA, Paper No SS-4698-04.
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7. MIL-STD-461E. 20 August 1999. "Requirements for the Control of Electromagnetic Interference of Subsystem and Equipment," Department of Defense Interface Standard.
8. Newton, D.V., et al. May 1996 "Piezoelectric Actuation Systems: Optimization of Driving Electronics," In: SPIE Proceedings, Vol. 2717, pp. 259-266.
9. Shah, N., et al. January 2000. "Power Management and Distribution System for a More-Electric Aircraft (MADMEL), Final Report," AFRL-PRWPTR2000-2043.