Helicopter vibration reduction in forward flight with induced-shear based piezoceramic actuation

Smart Materials and Structures

Volumn 13, Issue 3, 2004, Pages 599-608

  Thakkar, Dipali ^a   Ganguli, Ranjan ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; ELASTIC MODULI; FEEDBACK CONTROL; HARMONIC GENERATION; HELICOPTER ROTORS; KINETIC ENERGY; MANEUVERABILITY; MATHEMATICAL MODELS; PIEZOELECTRIC MATERIALS; STRAIN; VOLTAGE CONTROL;

LEAD ZIRCONATE TITANATE; PIEZOCERAMIC MATERIALS; POWER CONSUMPTION; ROTOR BLADES;

CERAMIC MATERIALS;

EID: 2942536197     PISSN: 09641726     EISSN: None     Source Type: Journal    
DOI: 10.1088/0964-1726/13/3/019     Document Type: Article

References (38)

1. Friedmann P 1999 Renaissance of aeroelasticity and its future J. Aircr. 36 105-21
2. Giurgiutiu V 2000 Review of smart-materials actuation solutions for aeroelastic and vibration control J. Intell. Mater. Syst. Struct. 11 525-43
3. Chopra I 2002 Review of state of art of smart structures and integrated systems AIAA J. 40 2145-87
4. Crawley E 1994 Intelligent structures for aerospace: a technology overview and assessment AIAA J. 32 1689-99
5. Sirohi J and Chopra I 2000 Fundamental understanding of piezoelectric strain sensors J. Intell. Mater. Syst. Struct. 11 246-57
6. Durr J, Schmidt U and Zaglauer W 1999 On the integration of piezoceramic actuators in composite structures for aerospace applications J. Intell. Mater. Syst. Struct. 10 880-9
7. Damjanovic D 1998 Ferroelectric, dielectric and piezoelectric properties of ferroelectric thin films and actuators Rep. Prog. Phys. 61 1267-322
8. Chen P and Chopra I 1996 Induced strain actuation of composite beams and rotor blades with embedded piezoceramic elements Smart Mater. Struct. 5 35-48
9. Chen P and Chopra I 1997 Hover testing of smart rotor with induced-strain actuation of blade twist AIAA J. 35 6-16
10. Bernhard A and Chopra I 1998 Hover testing of active rotor blade-tips using a piezo-induced bending-torsion coupled beam J. Intell. Mater. Syst. Struct. 9 963-74
11. Bernhard A and Chopra I 2001 Analysis of a bending-torsion coupled actuator for a smart rotor with active blade tips Smart Mater. Struct. 10 35-52
12. Barrett R, Frye P and Schliesman M 1998 Design, construction, and characterization of a flightworthy piezoelectric solid state adaptive rotor Smart Mater. Struct. 7 422-31
13. Rodgers J and Hagood N 1998 Design, manufacture, and testing of an integral twist-actuated rotor blade 9th Int. Conf. on Adaptive Structures and Technology (Cambridge, MA)
14. Wilkie W et al 1999 Aeroelastic analysis of the NASA/army/MIT active twist rotor 55th Annual Forum, American Helicopter Society (Montreal)
15. Derham R and Hagood N 1996 Rotor design using smart materials to actively twist blades 52nd Annual Forum, American Helicopter Society (Washington, DC)
16. Chattopadhyay A, Lin Q and Gu H 2000 Vibration reduction in rotor blades using active composite box beam AIAA J. 38 1125-31
17. Cesnik C and Shin S 2001 Dynamic response of active twist rotor blades Smart Mater. Struct. 10 62-76
18. Sun C and Zhang X 1995 Use of thickness-shear mode in adaptive sandwich structures Smart Mater. Struct. 4 202-6
19. Benjeddou A, Trindade M and Ohayon R 1999 New shear actuated smart structure beam finite element AIAA J. 37 378-83
20. Benjeddou A, Trindade M and Ohayon R 1999 Piezoelectric actuation mechanisms for intelligent sandwich structures Smart Mater. Struct. 9 328-35
21. 15 shear response Appl. Phys. Lett. 72 2526-8
22. 15 shear response J. Intell. Mater. Syst. Struct. 11 456-68
23. Li S, Cao W and Cross L 1991 The extrinsic nature of nonlinear behavior observed in lead zirconate titanate ferroelectric ceramic J. Appl. Phys. 69 7219-24
24. Mueller V and Zhang Q 1997 Shear response of lead zirconate titanate J. Appl. Phys. 83 3754-61
25. Mueller V and Beige H 1998 Nonlinearity of soft pzt piezoceramics for shear and torsional actuator applications Proc. IEEE Int. Symp. on Application of Ferroelectrics (Piscataway, NJ: IEEE) pp 459-62 (IEEE catalog number 98CH362455)
26. Smith E 2002 Induced-shear piezoelectric actuators for active twist rotor blades AIAA-2002-1446-CP
27. Masys A, Ren W, Yang G and Mukherjee B 2003 Piezoelectric strain in lead zirconate titanate ceramics as a function of electric field, frequency, and dc bias J. Appl. Phys. 94 1155-62
28. Hodges D and Dowell E 1974 Nonlinear Equations of Motion for the Elastic Bending and Torsion of Twisted Nonuniform Rotor Blades NASA TN D-7818
29. Smith E 1994 Vibration and flutter of stiff-inplane elastically tailored composite rotor blades J. Math. Comput. Modeling 19 27-45
30. Ganguli R and Chopra I 1996 Aeroelastic optimization of a helicopter rotor using two-cell composite blades AIAA J. 34 835-41
31. Inthra P and Gandhi F 2001 Optimal control of helicopter vibration through cyclic variations in blade root stiffness Smart Mater. Struct. 10 96-103
32. Bir G et al 1992 University of Maryland Advanced Rotorcraft Code (UMARC) Theory Manual UM-AERO Report 92-02
33. Gjelsvik A 1981 The Theory of Thin Walled Bars (New York: Wiley-Interscience)
34. Chen W and Saleeb A 1952 Constitutive Equations for Engineering Materials vol 1 Elasticity and Modeling (New York: Wiley-Interscience)
35. Lin C, Hsu C and Huang H 1996 Finite element analysis on deflection control of plates with piezoelectric actuators J. Compos. Struct. 35 423-33
36. Thakkar D and Ganguli R 2004 Dynamic response of rotating beams with piezoceramic actuation J. Sound Vib. 270 729-53
37. Ganguli R 2002 Optimum design of a helicopter rotor for low vibration using aeroelastic analysis and response surface model J. Sound Vib. 258 327-44
38. Leishman J and Beddoes T 1990 A generalized model for unsteady aerodynamic behaviour and dynamic stall using the indicial method J. Am. Helicopter Soc. 36 14-24