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Volumn 46, Issue 2, 2009, Pages 692-696

Smart spring control of vibration on helicopter rotor blades

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; DEGREES OF FREEDOM (MECHANICS); HELICOPTER ROTORS; STRUCTURAL DYNAMICS; TURBOMACHINE BLADES;

EID: 63349108346     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.27914     Document Type: Article
Times cited : (23)

References (19)
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  • 2
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    • Vibration Reduction in Rotorcraft Using Active Control: A Comparison of Various Approaches
    • doi:10.2514/3.21445
    • Friedmann, P. P., and Millott, T. A., "Vibration Reduction in Rotorcraft Using Active Control: A Comparison of Various Approaches," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 4, pp. 664-673. doi:10.2514/3.21445
    • Journal of Guidance, Control, and Dynamics , vol.18 , Issue.4 , pp. 664-673
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  • 3
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    • FurtherExamination of the Vibratory Loads Reduction Results From The NASA/Army/MIT Active Twist Rotor Test
    • Royal Aeronautical Society, Bristol, England, U.K
    • Wilbur, M. L., Yeager, W. T., and Sekula, M. K., "FurtherExamination of the Vibratory Loads Reduction Results From The NASA/Army/MIT Active Twist Rotor Test," American Helicopter Society 58th Annual Forum, Royal Aeronautical Society, Bristol, England, U.K., 2002, pp. 60.1-60.15.
    • (2002) American Helicopter Society 58th Annual Forum
    • Wilbur, M.L.1    Yeager, W.T.2    Sekula, M.K.3
  • 5
    • 0343559156 scopus 로고
    • Can Smart Materials Modify the Blade Root Boundary Conditions to Attenuate Helicopter Vibration?
    • Technomic Publishing
    • Nitzsche, F., Lammering, R., and Breitbach, E., "Can Smart Materials Modify the Blade Root Boundary Conditions to Attenuate Helicopter Vibration?," Fourth International Conference on Adaptive Structures, Technomic Publishing, 1994, pp. 139-150.
    • (1994) Fourth International Conference on Adaptive Structures , pp. 139-150
    • Nitzsche, F.1    Lammering, R.2    Breitbach, E.3
  • 7
    • 0004840826 scopus 로고    scopus 로고
    • Structural Component Having Means for Actively Varying its Stiffness to Control Vibrations,
    • U.S. Patent No. 5,973,440, October
    • Nitzsche, F., Grewal, A., and Zimcik, D., "Structural Component Having Means for Actively Varying its Stiffness to Control Vibrations," U.S. Patent No. 5,973,440, October 1999.
    • (1999)
    • Nitzsche, F.1    Grewal, A.2    Zimcik, D.3
  • 8
  • 9
    • 0034135721 scopus 로고    scopus 로고
    • Helicopter Vibration Reduction Through Cyclic Variations in Blade Root Stiffness
    • Anusonti-Inthra, P., and Ghandi, F., "Helicopter Vibration Reduction Through Cyclic Variations in Blade Root Stiffness," Journal of Intelligent Material Systems and Structures, Vol. 11, No. 2, pp. 153-166, 2000.
    • (2000) Journal of Intelligent Material Systems and Structures , vol.11 , Issue.2 , pp. 153-166
    • Anusonti-Inthra, P.1    Ghandi, F.2
  • 10
    • 3042543538 scopus 로고    scopus 로고
    • Active Twist Rotor Blade Modeling Using Particle-Wake Aerodynamics and Geometrically Exact Beam Structural Dynamics
    • doi:10.1016/jfluidstructs.2004.01.007
    • Cesnik, C. E. S., Opoku, D. G., Nitzsche, F., and Cheng, T., "Active Twist Rotor Blade Modeling Using Particle-Wake Aerodynamics and Geometrically Exact Beam Structural Dynamics," Journal of Fluids and Structures, Vol. 19, pp. 651-668. doi:10.1016/jfluidstructs.2004.01.007
    • Journal of Fluids and Structures , vol.19 , pp. 651-668
    • Cesnik, C.E.S.1    Opoku, D.G.2    Nitzsche, F.3    Cheng, T.4
  • 11
    • 0342418535 scopus 로고
    • Differential Equations of Motion for Combined Flapwise Bending, Chordwise Bending, and Torsion of Twisted Nonuniform Rotor Blades
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    • Houbolt, J.C.1    Brooks, G.W.2
  • 14
    • 23144467649 scopus 로고    scopus 로고
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    • June
    • Nitzsche, F., and Opoku, D. G., "Acoustic Validation of a New Code Using Particle Wake Aerodynamics and Geometrically Exact Beam Structural Dynamics," The Aeronautical Journal, Vol. 109, No. 1096, June 2005, pp. 257-267.
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    • Nitzsche, F.1    Opoku, D.G.2
  • 15
    • 0020767530 scopus 로고
    • Some Analysis Methods for Rotating Systems with Periodic Coefficients
    • doi:10.2514/3.8167
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  • 16
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    • March
    • Nitzsche, F., "Aeroelastic Analysis of a Helicopter Blade with Active Impedance Control at the Root," Canadian Aeronautics and Space Journal, Vol. 47, March 2001, pp. 7-16.
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    • Nitzsche, F.1
  • 18
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    • Harold, T., and Nitzsche, F., "The Smart Spring-An Indirect Active Low-Power Adaptive Structure Device for Vibration Attenuation," High Performance Structures and Materials II, edited by C. A. Brebbia and W. P. DeWilde, WIT Press, Southampton, England, U.K., 2004, pp. 297-306.
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.