Advanced piezoelectric servo flap system for rotor active control

National Aerospace Laboratory NLR - 32nd European Rotorcraft Forum, ERF 2006

Volumn 1, Issue , 2007, Pages 350-357

  Jänker, Peter ^a   Hermle, Frank ^a   Friedl, Stephan ^a   Lentner, Konrad ^a   Enenkl, Bernhard ^b   Müller, Christine ^b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b EUROCOPTER DEUTSCHLAND GMBH   (France)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT CONTROL SYSTEMS; HINGES; OPTIMIZATION; PIEZOELECTRIC MATERIALS; POWER ELECTRONICS; RELIABILITY THEORY;

SERVO FLAP SYSTEM; SIGNAL TRANSMISSION; TRAILING EDGE FLAPS;

ROTORS;

EID: 34547580239     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. th European Rotorcraft Forum, Bristol, 2002
2. th European Rotorcraft Forum, Rome, 1999
3. nd AHS Annual Forum, Phoenix, AZ, USA, May 2006
4. B. Grohmann, C. Maucher, P. Jänker, A. Altmikus, D. Schimke: "Aero-ServoEleastic Predesign of a Smart Trailing-Edge Tab for an Adaptive Helicopter Rotor Blade"; IFASD, Munich, 2004
5. B. Grohmann, P. Konstanzer, B. Kröplin: "Decentralized vibration control and coupled aeroservoelastic simulation of helicopter rotor blades with adaptive airfoils"; In IUTAM Symposium on Smart Structures and Structronic Systems, Magdeburg, 2000