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Physics / Piezoelectricity / Electric motor / Valve actuator / Machine / Helicopter rotor / Amplified piezoelectric actuator / Linear actuator / Actuators / Electromagnetism / Energy


Document Date: 2009-10-23 04:15:30

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Company

Smart Structures Technologies / SatCon Technology Corp. / Boeing / Philips / Finmeccanica Group / DSM / AgustaWestland / Integrated Systems / /

Continent

Europe / /

Country

United States / Denmark / /

Facility

University of South Carolina / Hall X-Frame / University of Maryland / Massachusetts Institute of Technology / Steven R Hall / /

IndustryTerm

metal / energy density criterion / active element energy / aerospace application / double amplification systems / electromagnetic actuation systems / high energy density / active device / Rotor blade flap technologies / active trailing edge applications / energy density / civil and military applications / active devices / aerospace / high energy levels / energy / steel / /

Organization

Hinge Tension / University of South Carolina / University of Maryland / Fixed / MIT / UK Technology Strategy Board / Massachusetts Institute of Technology / Output / /

Person

Eric F Prechtl / Frank Philips / Alan D. Stemple / V / Victor Giurgiutiu / Friedrich K. Straub / Blade Trailing-Edge / Dennis K. Kennedy / Theodora Tzianetopoulou / Mike Gerver / Terry S. Birchette / Eric F. Prechtl / Ralph Fenn / V.R. Anand / Dariusz Bushko / /

Position

driver / /

Product

CH-47D / /

ProvinceOrState

Maryland / South Carolina / Massachusetts / /

PublishedMedium

Smart Materials and Structures / /

Technology

Rotor blade flap technologies / /

URL

http /

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