Dynamic modeling and coupling characteristics of rotating inclined beams with twisted-shape sections

Jin ZENG , Chenguang ZHAO , Hui MA , Bangchun WEN

Front. Mech. Eng. ›› 2020, Vol. 15 ›› Issue (3) : 374 -389.

PDF (2565KB)
Front. Mech. Eng. ›› 2020, Vol. 15 ›› Issue (3) : 374 -389. DOI: 10.1007/s11465-019-0580-8
RESEARCH ARTICLE
RESEARCH ARTICLE

Dynamic modeling and coupling characteristics of rotating inclined beams with twisted-shape sections

Author information +
History +
PDF (2565KB)

Abstract

In the existing literature, most studies investigated the free vibrations of a rotating pre-twisted cantilever beam; however, few considered the effect of the elastic-support boundary and the quantification of modal coupling degree among different vibration directions. In addition, Coriolis, spin softening, and centrifugal stiffening effects are not fully included in the derived equations of motion of a rotating beam in most literature, especially the centrifugal stiffening effect in torsional direction. Considering these deficiencies, this study established a coupled flapwise–chordwise–axial–torsional dynamic model of a rotating double-tapered, pre-twisted, and inclined Timoshenko beam with elastic supports based on the semi-analytic method. Then, the proposed model was verified with experiments and ANSYS models using Beam188 and Shell181 elements. Finally, the effects of setting and pre-twisted angles on the degree of coupling among flapwise, chordwise, and torsional directions were quantified via modal strain energy ratios. Results showed that 1) the appearance of torsional vibration originates from the combined effect of flapwise–torsional and chordwise–torsional couplings dependent on the Coriolis effect, and that 2) the flapwise–chordwise coupling caused by the pure pre-twisted angle is stronger than that caused by the pure setting angle.

Keywords

elastic-support boundary / pre-twisted beam / semi-analytic method / modal strain energy ratio / torsional vibration

Cite this article

Download citation ▾
Jin ZENG, Chenguang ZHAO, Hui MA, Bangchun WEN. Dynamic modeling and coupling characteristics of rotating inclined beams with twisted-shape sections. Front. Mech. Eng., 2020, 15(3): 374-389 DOI:10.1007/s11465-019-0580-8

登录浏览全文

4963

注册一个新账户 忘记密码

References

[1]

Lin S M. Dynamic analysis of rotating nonuniform Timoshenko beams with an elastically restrained root. Journal of Applied Mechanics, 1999, 66(3): 742–749

[2]

He Q, Xuan H J, Liu L L, et al. Perforation of aero-engine fan casing by a single rotating blade. Aerospace Science and Technology, 2013, 25(1): 234–241

[3]

Javdani S, Fabian M, Carlton J S, et al. Underwater free-vibration analysis of full-scale marine propeller using a fiber Bragg grating-based sensor system. IEEE Sensors Journal, 2016, 16(4): 946–953

[4]

Rezaei M M, Behzad M, Haddadpour H, et al. Development of a reduced order model for nonlinear analysis of the wind turbine blade dynamics. Renewable Energy, 2015, 76: 264–282

[5]

Rao J S, Carnegie W. Solution of the equations of motion of coupled-bending bending torsion vibrations of turbine blades by the method of Ritz–Galerkin. International Journal of Mechanical Sciences, 1970, 12(10): 875–882

[6]

Houbolt J C, Brooks G W. Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades. National Advisory Committee for Aeronautics, Technical Note 3905, 1957

[7]

Du H, Lim M K, Liew K M. A power series solution for vibration of a rotating Timoshenko beam. Journal of Sound and Vibration, 1994, 175(4): 505–523

[8]

Rao J S. Flexural vibration of pretwisted tapered cantilever blades. Journal of Engineering for Industry, 1972, 94(1): 343–346

[9]

Şakar G, Sabuncu M. Dynamic stability of a rotating asymmetric cross-section blade subjected to an axial periodic force. International Journal of Mechanical Sciences, 2003, 45(9): 1467–1482

[10]

Banerjee J R. Free vibration of centrifugally stiffened uniform and tapered beams using the dynamic stiffness method. Journal of Sound and Vibration, 2000, 233(5): 857–875

[11]

Zeng J, Ma H, Yu K, Rubbing response comparisons between single blade and flexible ring using different rubbing force models. International Journal of Mechanical Sciences, 2019, 164: 105164

[12]

Zeng J, Zhao C G, Ma H, Rubbing dynamic characteristics of the blisk-casing system with elastic supports. Aerospace Science and Technology, 2019, 95: 105481

[13]

Hodges D H, Dowell E H. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades. NASA Technical Report NASA-TN-D-7818, A-5711, 1974

[14]

Zhu T L. The vibrations of pre-twisted rotating Timoshenko beams by the Rayleigh–Ritz method. Computational Mechanics, 2011, 47(4): 395–408

[15]

Ma H, Xie F T, Nai H Q, Vibration characteristics analysis of rotating shrouded blades with impacts. Journal of Sound and Vibration, 2016, 378: 92–108

[16]

Xie F T, Ma H, Cui C, Vibration response comparison of twisted shrouded blades using different impact models. Journal of Sound and Vibration, 2017, 397: 171–191

[17]

Sinha S K. Combined torsional-bending-axial dynamics of a twisted rotating cantilever Timoshenko beam with contact-impact loads at the free end. Journal of Applied Mechanics, 2007, 74(3): 505–522

[18]

Yang X D, Wang S W, Zhang W, et al. Dynamic analysis of a rotating tapered cantilever Timoshenko beam based on the power series method. Applied Mathematics and Mechanics, 2017, 38(10): 1425–1438

[19]

Şakar G, Sabuncu M. Buckling and dynamic stability of a rotating pretwisted asymmetric cross-section blade subjected to an axial periodic force. Finite Elements in Analysis and Design, 2004, 40(11): 1399–1415

[20]

Sabuncu M, Evran K. Dynamic stability of a rotating pre-twisted asymmetric cross-section Timoshenko beam subjected to an axial periodic force. International Journal of Mechanical Sciences, 2006, 48(6): 579–590

[21]

Subrahmanyam K B, Kaza K R V, Brown G V, et al. Nonlinear bending-torsional vibration and stability of rotating, pretwisted, preconed blades including Coriolis effects. In: Proceedings of Workshop on Dynamics and Aeroelastic Stability Modeling of Rotor Systems. Atlanta: NASA, 1986, NASA-TM-87207

[22]

Sina S A, Haddadpour H. Axial–torsional vibrations of rotating pretwisted thin walled composite beams. International Journal of Mechanical Sciences, 2014, 80: 93–101

[23]

Adair D, Jaeger M. Vibration analysis of a uniform pre-twisted rotating Euler–Bernoulli beam using the modified Adomian decomposition method. Mathematics and Mechanics of Solids, 2018, 23(9): 1345–1363

[24]

Oh Y, Yoo H H. Vibration analysis of a rotating pre-twisted blade considering the coupling effects of stretching, bending, and torsion. Journal of Sound and Vibration, 2018, 431: 20–39

[25]

Lee J W, Lee J Y. Development of a transfer matrix method to obtain exact solutions for the dynamic characteristics of a twisted uniform beam. International Journal of Mechanical Sciences, 2016, 105: 215–226

[26]

Banerjee J R. Development of an exact dynamic stiffness matrix for free vibration analysis of a twisted Timoshenko beam. Journal of Sound and Vibration, 2004, 270(1–2): 379–401

[27]

Subrahmanyam K B, Kaza K R V. Vibration and buckling of rotating, pretwisted, preconed beams including Coriolis effects. Journal of Vibration and Acoustics, 1986, 108(2): 140–149

[28]

Hashemi S M, Richard M J. Natural frequencies of rotating uniform beams with Coriolis effects. Journal of Vibration and Acoustics, 2001, 123(4): 444–455

[29]

Banerjee J R, Kennedy D. Dynamic stiffness method for inplane free vibration of rotating beams including Coriolis effects. Journal of Sound and Vibration, 2014, 333(26): 7299–7312

[30]

Oh S Y, Song O, Librescu L. Effects of pretwist and presetting on coupled bending vibrations of rotating thin-walled composite beams. International Journal of Solids and Structures, 2003, 40(5): 1203–1224

[31]

Latalski J, Warminski J, Rega G. Bending–twisting vibrations of a rotating hub–thin-walled composite beam system. Mathematics and Mechanics of Solids, 2017, 22(6): 1303–1325

[32]

Ondra V, Titurus B. Free vibration analysis of a rotating pre-twisted beam subjected to tendon-induced axial loading. Journal of Sound and Vibration, 2019, 461: 114912

[33]

Zeng J, Chen K K, Ma H, Vibration response analysis of a cracked rotating compressor blade during run-up process. Mechanical Systems and Signal Processing, 2019, 118: 568–583

[34]

Sun Q, Ma H, Zhu Y P, Comparison of rubbing induced vibration responses using varying-thickness-twisted shell and solid-element blade models. Mechanical Systems and Signal Processing, 2018, 108: 1–20

[35]

Ma H, Wang D, Tai X Y, Vibration response analysis of blade-disk dovetail structure under blade tip rubbing condition. Journal of Vibration and Control, 2017, 23(2): 252–271

[36]

Lin S M. The instability and vibration of rotating beams with arbitrary pretwist and an elastically restrained root. Journal of Applied Mechanics, 2001, 68(6): 844–853

[37]

Lin S M, Wu C T, Lee S Y. Analysis of rotating nonuniform pretwisted beams with an elastically restrained root and a tip mass. International Journal of Mechanical Sciences, 2003, 45(4): 741–755

[38]

Lee S Y, Lin S M, Wu C T. Free vibration of a rotating non-uniform beam with arbitrary pretwist, an elastically restrained root and a tip mass. Journal of Sound and Vibration, 2004, 273(3): 477–492

[39]

Choi S T, Chou Y T. Vibration analysis of elastically supported turbomachinery blades by the modified differential quadrature method. Journal of Sound and Vibration, 2001, 240(5): 937–953

[40]

Bambill D V, Rossit C A, Rossi R E, Transverse free vibration of non uniform rotating Timoshenko beams with elastically clamped boundary conditions. Meccanica, 2013, 48(6): 1289–1311

[41]

Digilov R M, Abramovich H. The impact of root flexibility on the fundamental frequency of a restrained cantilever beam. International Journal of Mechanical Engineering Education, 2017, 45(2): 184–193

[42]

Hodges D H. Torsion of pretwisted beams due to axial loading. Journal of Applied Mechanics, 1980, 47(2): 393–397

[43]

Zeng J, Ma H, Yu K, Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation. Applied Mathematics and Mechanics, 2019, 40(8): 1053–1082

RIGHTS & PERMISSIONS

Higher Education Press

AI Summary AI Mindmap
PDF (2565KB)

3731

Accesses

0

Citation

Detail

Sections
Recommended

AI思维导图

/