Abstract
The influence of blade vibration on the nonlinear characteristics of rotor–bearing system is non-ignorable in estimating system performance. The extensive studies simplify the rotor system as lumped mass points. The influence of shaft’s bending and shear and the flexibility are usually ignored. The present paper is aim to analyze the nonlinear dynamic behavior of a continuum model. The continuum model of flexible blade–rotor–bearing coupling system is established, simplifying the shaft as Timoshenko beam. The Lagrange method is utilized to derive the differential equation of motion of system. Then, the nonlinear equations of coupling system are numerically solved using the Newmark-\(\upbeta \) method. The results obtained through the proposed model are compared with the rotor–bearing system without the blades. The effect of several parameters such as rotational speed, the damping coefficient and the length of blade on the nonlinear dynamics of rotor system have been investigated. Inclusive of the analysis methods of bifurcation diagram, three-dimensional spectral plots, time-base analysis, Poincare maps and spectral plots are used to analyze the behavior of the coupling system under different operating conditions, which exhibits rich dynamic behavior of the system.
Similar content being viewed by others
Abbreviations
- \(\rho _\mathrm{s}\) :
-
Shaft mass density
- \(L_\mathrm{s}\) :
-
Shaft length
- \(A_\mathrm{s}\) :
-
Cross-sectional area of the shaft
- \(E_\mathrm{s}\) :
-
Young’s modulus of shaft
- \(I_\mathrm{s}\) :
-
Cross-sectional area moment of inertia of shaft
- \(G_\mathrm{s}\) :
-
Shear elastic modulus of shaft
- \(J_\mathrm{p}\) :
-
Shaft’s polar moment of inertia
- \(J_\mathrm{d}\) :
-
Shaft’s cross-sectional moment of inertia
- \(J_\mathrm{dz}\) :
-
Disk’s cross-sectional moment of inertia
- \(J_\mathrm{z}\) :
-
Disk’s polar moment of inertia
- \(\rho _\mathrm{b}\) :
-
Blade mass density
- \(L_\mathrm{b}\) :
-
Blade length
- \(A_\mathrm{b}\) :
-
Cross-sectional area of the blade
- \(E_\mathrm{b}\) :
-
Young’s modulus of blade
- \(I_\mathrm{b}\) :
-
Cross-sectional area moment of inertia of blade
- x:
-
Shaft’s transverse displacements with respect to the X-axis
- y:
-
Shaft’s transverse displacements with respect to the Y-axis
- \(\theta _x,\theta _y\) :
-
Bending angle of shaft at arbitrary position
- u :
-
Blade displacements with respect to the \(x_\mathrm{b}\)-axis
- v :
-
Blade displacements with respect to the \(y_\mathrm{b}\)-axis
- w :
-
Blade displacements with respect to the \(z_\mathrm{b}\)-axis
- \({{\varvec{X}}}\) :
-
The mode shape vector of the bending shaft respect to the X-axis
- \({{\varvec{Y}}}\) :
-
The mode shape vector of the bending shaft respect to the Y-axis
- \({\varvec{\varPhi }}\) :
-
The mode shape vector of the shaft torsion
- \({\varvec{\varPsi }}\) :
-
The mode shape vector of the blade axial
- \({{\varvec{V}}}\) :
-
The mode shape vector of the blade bending direction
- \({\varvec{\eta }}, {\varvec{\xi }},{{\varvec{q}}}_{{{\varvec{u}}}} , {{\varvec{q}}}_{{{\varvec{v}}}}\) :
-
Generalized vector
- \(\dot{\phi }\) :
-
Rotational speed
- \(()_\mathrm{b}\) :
-
Blade
- \(()_\mathrm{d}\) :
-
Disk
- \(()_\mathrm{s}\) :
-
Shaft
- \(()_\mathrm{T}\) :
-
Shaft torsion
References
Taplak, H., Erkaya, S., İbrahim, Uzmay: Experimental analysis on fault detection for a direct coupled rotor–bearing system. Measurement 46(1), 336–344 (2013)
Santos, I.F., Saracho, C.M., Smith, J.T., et al.: Contribution to experimental validation of linear and non-linear dynamic models for representing rotor–blade parametric coupled vibrations. J. Sound Vib. 271(3–5), 883–904 (2004)
Shen, X.Y., Mei, Z.: Numerical and experimental analysis of nonlinear dynamics of rotor–bearing–seal system. Nonlinear Dyn. 53(1–2), 31–44 (2008)
Yan, S., Dowell, E.H., Lin, B.: Effects of nonlinear damping suspension on nonperiodic motions of a flexible rotor in journal bearings. Nonlinear Dyn. 778(2), 1435–1450 (2014)
Qin, Z.Y., Han, Q.K., Chu, F.L.: Analytical model of bolted disk–drum joints and its application to dynamic analysis of jointed rotor. ARCHIVE Proc. Inst. Mech. Eng. C J. Mech. Eng. Sci. 228(4), 646–663 (2014)
Qin, Z., Han, Q., Chu, F.: Bolt loosening at rotating joint interface and its influence on rotor dynamics. Eng. Fail. Anal. 59, 456–466 (2015)
Castro, H.F.D., Cavalca, K.L., Nordmann, R.: Whirl and whip instabilities in rotor–bearing system considering a nonlinear force model. J. Sound Vib. 317(1–2), 273–293 (2008)
Chang-Jian, C.W., Chen, C.K.: Chaotic response and bifurcation analysis of a flexible rotor supported by porous and non-porous bearings with nonlinear suspension. Nonlinear Anal. Real World Appl. 10(2), 1114–1138 (2009)
Laha, S.K., Kakoty, S.K.: Non-linear dynamic analysis of a flexible rotor supported on porous oil journal bearings. Commun. Nonlinear Sci. Numer. Simul. 16(16), 1617–1631 (2011)
Yang, L.H., Wang, W.M., Zhao, S.Q., et al.: A new nonlinear dynamic analysis method of rotor system supported by oil-film journal bearings. Appl. Math. Model. 38(21–22), 5239–5255 (2014)
Jing, J.P., Meng, G., Yi, S., et al.: On the non-linear dynamic behavior of a rotor–bearing system. J. Sound Vib. 274(3–5), 1031–1044 (2002)
Jing, J.P., Meng, G., Sun, Y., et al.: On the oil-whipping of a rotor–bearing system by a continuum model. Appl. Math. Model. 29(5), 461–475 (2005)
Meybodi, R.R., Mohammadi, A.K., Bakhtiari-Nejad, F.: Numerical analysis of a rigid rotor supported by aerodynamic four-lobe journal bearing system with mass unbalance. Commun. Nonlinear Sci. Numer. Simul. 17(1), 454–471 (2012)
Li, W., Yang, Y., Sheng, D., et al.: A novel nonlinear model of rotor/bearing/seal system and numerical analysis. Mech. Mach. Theory 46(5), 618–631 (2011)
Cheng, M., Meng, G., Jing, J.: Numerical and experimental study of a rotor–bearing–seal system. Mech. Mach. Theory 42(8), 1043–1057 (2007)
Phadatare, H.P., Pratiher, B.: Nonlinear frequencies and unbalanced response analysis of high speed rotor–bearing systems. Proc. Eng. 144, 801–809 (2016)
Xiang, L., Hu, A., Hou, L., et al.: Nonlinear coupled dynamics of an asymmetric double-disc rotor–bearing system under rub-impact and oil-film forces. Appl. Math. Model. 40(7–8), 4505–4523 (2015)
Hu, A., Hou, L., Xiang, L.: Dynamic simulation and experimental study of an asymmetric double-disk rotor–bearing system with rub-impact and oil-film instability. Nonlinear Dyn. 84(2), 641–659 (2015)
Chang-Jian, C.W., Chen, C.K.: Chaos of rub-impact rotor supported by bearings with nonlinear suspension. Tribol. Int. 42(3), 426–439 (2009)
Chu, F., Zhang, Z.: Periodic, quasi-periodic and chaotic vibrations of a rub-impact rotor system supported on oil film bearings. Int. J. Eng. Sci. 35(10–11), 963–973 (1997)
Chang-Jian, C.W., Chen, C.K.: Non-linear dynamic analysis of rub-impact rotor supported by turbulent journal bearings with non-linear suspension. Int. J. Mech. Sci. 50(6), 1090–1113 (2008)
Chang-Jian, C.W., Chen, C.K.: Couple stress fluid improve rub-impact rotor–bearing system. Nonlinear Dyn. Anal. Appl. Math. Model. 34(7), 1763–1778 (2010)
Ping, L.Z., Gang, L.Y., Liang, Y.H., et al.: Nonlinear dynamic study of the elastic rotor–bearing system with rub-impact fault. J. Northeast. Univ. 23(10), 980–983 (2002)
Han, F., Guo, X.L., Gao, H.Y.: Research on coupled bending and torsion vibration of blade–rotor–bearing system with nonlinear oil-film force. Eng. Mech. 30(4), 355–359 (2013)
Wang, L., Cao, D.Q., Huang, W.: Nonlinear coupled dynamics of flexible blade–rotor–bearing systems. Tribol. Int. 43, 759–778 (2010)
Wang, L., Cao, D.Q., Huang, W.: Nonlinear dynamic behavior of a blade–shaft–bearing system. Chin. J. Appl. Mech. 24(2), 169–174 (2007)
Wang, L., Cao, D.Q., Huang, W.: Effect of the blade vibration on the dynamical behaviors of a rotor–bearing system. J. Harbin Eng. Univ. 28(3), 320–325 (2007)
Acknowledgements
The project is supported by the China Natural Science Funds (No. 51575093), Natural Science Funds of Liaoning Province (No. 2015020153)
Author information
Authors and Affiliations
Corresponding author
Ethics declarations
Conflict of interest
The authors declare that there is no conflict of interests regarding the publication of this article.
Appendices
Appendix 1: Vectors and matrices related to the rotor system
-
(1)
Expression of discrete kinetic energy of shaft can be shown as follows
$$\begin{aligned} T_{\mathrm{s}}= & {} \int _0^{L_{\mathrm{s}} } \left[ \frac{1}{2}\rho A(\dot{{\varvec{\eta }}}^{\mathrm{T}}(t){{\varvec{X}}}^{\mathrm{T}}(z){{\varvec{X}}}(z)\dot{{\varvec{\eta }}}(t)\right. \nonumber \\&+\dot{{\varvec{\xi }}}^{\mathrm{T}}(t){{\varvec{Y}}}^{\mathrm{T}}(z){{\varvec{Y}}}(z)\dot{{\varvec{\xi }}}(t)) +\frac{1}{2}J_{\mathrm{p}} \dot{\phi }^{2} \nonumber \\&+\frac{1}{2}J_{\mathrm{d}} \left( \left[ {{\varvec{X}}}^{'}(z)\dot{{\varvec{\eta }}}(t)+\frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z)\dot{{\varvec{\eta }}}(t)\right] ^{\mathrm{T}}\left[ {{\varvec{X}}}^{'}(z)\dot{{\varvec{\eta }}}(t)\right. \right. \nonumber \\&\left. \left. +\frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z)\dot{{\varvec{\eta }}}(t)\right] \right) \nonumber \\&+\frac{1}{2}J_{\mathrm{d}} \left[ {{\varvec{Y}}}^{'}(z)\dot{{\varvec{\xi }}}(t)+\frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z)\dot{{\varvec{\xi }}}(t)\right] ^{\mathrm{T}}\left[ {{\varvec{Y}}}^{'}(z)\dot{{\varvec{\xi }}}(t)\right. \nonumber \\&\left. \left. +\frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z)\dot{{\varvec{\xi }}}(t)\right] \right) \nonumber \\&+\frac{1}{2}J_{\mathrm{p}} \dot{\phi }\left( \left[ {{\varvec{X}}}^{'}(z)\dot{{\varvec{\eta }}}(t)+\frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z)\dot{{\varvec{\eta }}}(t)\right] ^{\mathrm{T}}\left[ {{\varvec{Y}}}^{'}(z){\varvec{\xi }}(t)\right. \right. \nonumber \\&\left. \left. +\frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z){\varvec{\xi }}(t)\right] \right) \nonumber \\&-\frac{1}{2}J_{\mathrm{p}} \dot{\phi }\left( \left[ {{\varvec{X}}}^{'}(z){\varvec{\eta }}(t)+\frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z){\varvec{\eta }}(t)\right] ^{\mathrm{T}}\left[ {{\varvec{Y}}}^{'}(z)\dot{{\varvec{\xi }}}(t)\right. \right. \nonumber \\&\left. \left. +\frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z)\dot{{\varvec{\xi }}}(t)\right] \right) \nonumber \\&+\frac{1}{2}I_{\mathrm{s}} \int _0^{L_{\mathrm{s}} } {\dot{{{\varvec{q}}}}_{\varvec{\theta }}^{{\varvec{T}}}} {\varvec{\varPhi }}^{{{\varvec{T}}}}{\varvec{\varPhi }} \dot{{{\varvec{q}}}}_{\varvec{\theta }} \hbox {d}z \end{aligned}$$(33) -
(2)
Expression of discrete kinetic energy of disk can be expressed as
$$\begin{aligned} T_{\mathrm{d}}= & {} \frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)m_{\mathrm{d}} {{\varvec{X}}}^{\mathrm{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\eta }}}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\xi }}}^{\mathrm{T}}(t)m_{\mathrm{d}} {{\varvec{Y}}}^{\mathrm{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}\left( {z_{\mathrm{d}}} \right) \dot{{\varvec{\xi }}}(t) \nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_\mathrm{dz} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\eta }}}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_{\mathrm{dz}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\eta }}}(t) \nonumber \\&+\frac{1}{2}\dot{{\varvec{\xi }}}^{\mathrm{T}}(t)J_{\mathrm{dz}} {{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\xi }}}^{\mathrm{T}}(t)J_{\mathrm{dz}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t) \nonumber \\&+\frac{1}{2}\dot{{\varvec{\xi }}}^{\mathrm{T}}(t)J_{\mathrm{dz}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\xi }}}^{\mathrm{T}}(t)J_{\hbox {dz}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t) \nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_{\mathrm{p}} \dot{\phi }{{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) {\varvec{\xi }}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_{\mathrm{z}} \dot{\phi }\frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) {\varvec{\xi }}(t) \nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi }\frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) {\varvec{\xi }}(t)\nonumber \\&+\frac{1}{2}\dot{{\varvec{\eta }}}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi }\left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}}} \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) {\varvec{\xi }}(t) \nonumber \\&-\frac{1}{2}{\varvec{\eta }}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi } {{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t)\nonumber \\&-\frac{1}{2}{\varvec{\eta }}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi }\frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t) \nonumber \\&-\frac{1}{2}{\varvec{\eta }}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi }\frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t)\nonumber \\&-\frac{1}{2}{\varvec{\eta }}^{\mathrm{T}}(t)J_\mathrm{z} \dot{\phi }\left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }}}(t)\nonumber \\ \end{aligned}$$(34) -
(3)
Expression of discrete potential energy of shaft can be written as
$$\begin{aligned} U_{\mathrm{s}}= & {} \frac{1}{2}\int _0^{L_\mathrm{s} } \left\{ EI([{{\varvec{X}}}^{''}(z){\varvec{\eta }}(t)]^{\mathrm{T}}[{{\varvec{X}}}^{''}(z){\varvec{\eta }}(t)]\right. \nonumber \\&\left. +[{{\varvec{Y}}}^{''}(z){\varvec{\xi }}(t)]^{\mathrm{T}}[{{\varvec{Y}}}^{''}(z){\varvec{\xi }}(t)]) \right. \nonumber \\&\left. +\kappa GA\left( \left[ \frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z){\varvec{\eta }}(t)\right] ^{\mathrm{T}}\left[ \frac{EI}{\kappa AG}{{\varvec{X}}}^{'''}(z){\varvec{\eta }}(t)\right] \right. \right. \nonumber \\&\left. \left. +\left[ \frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z){\varvec{\xi }}(t)\right] ^{\mathrm{T}}\left[ \frac{EI}{\kappa AG}{{\varvec{Y}}}^{'''}(z){\varvec{\xi }}(t)\right] \right) \right\} \hbox {d}z \nonumber \\= & {} \frac{1}{2}\int _0^{L_\mathrm{s} } \left\{ {{\varvec{q}}}_{\varvec{\theta }}^{\mathrm{T}} G_\mathrm{s} J_\mathrm{s} {\Phi }'^{\mathrm{T}}{\Phi }'{{\varvec{q}}}_\theta +{\varvec{\eta }}^{\mathrm{T}}(t)EI{{\varvec{X}}}^{{''}^{\mathrm{T}}}(z){{\varvec{X}}}^{''}(z){\varvec{\eta }}(t)\right. \nonumber \\&\left. +{\varvec{\xi }}^{\mathrm{T}}(t)EI{{\varvec{Y}}}^{{''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{''}(z){\varvec{\xi }}(t) \right. \nonumber \\&\left. +{\varvec{\eta }}^{\mathrm{T}}(t)\frac{(EI)^{2}}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z){\varvec{\eta }}(t)\right. \nonumber \\&\left. +{\varvec{\xi }}^{\mathrm{T}}(t)\frac{(EI)^{2}}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z){\varvec{\xi }}(t) \right\} \hbox {d}z \end{aligned}$$(35) -
(4)
The specific meaning of each parameter in the vibration differential equation of rotor
$$\begin{aligned} {{\varvec{M}}}_{\mathrm{r}}= & {} \left[ {{\begin{array}{ccc} \mathbf{M}_{\mathrm{s}1} +\mathbf{M}_{\mathrm{d}1} &{} {\mathbf{0}}&{} {\mathbf{0}} \\ {\mathbf{0}}&{} \mathbf{M}_{\mathrm{s}2} +{\mathbf{M}}_{\mathrm{d}2} &{} {\mathbf{0}} \\ {\mathbf{0}}&{} {\mathbf{0}}&{} {{\mathbf{M}}_{\varvec{\uptheta }} } \\ \end{array} }} \right] \nonumber \\ {{\varvec{C}}}_{\mathrm{r}}= & {} \left[ {{\begin{array}{ccc} {{{\varvec{C}}}_{\mathrm{s}1} +{{\varvec{C}}}_{\mathrm{d}1} }&{} 0&{} 0 \\ 0&{} {{{\varvec{C}}}_{\mathrm{s}2} +C_{\mathrm{d}2} }&{} 0 \\ 0&{} 0&{} {{{\varvec{C}}}_{\varvec{\uptheta }} } \\ \end{array} }} \right] \nonumber \\ {{\varvec{G}}}_{\mathrm{r}}= & {} \left[ {{\begin{array}{ccc} 0&{} {{\mathbf{G}}_{\mathrm{s}1} +{\mathbf{G}}_{\mathrm{d}1} }&{} 0 \\ {{\mathbf{G}}_{\mathrm{s}2} +{\mathbf{G}}_{\mathrm{d}2} }&{} 0&{} 0 \\ 0&{} 0&{} 0 \\ \end{array} }} \right] \nonumber \\ {{\varvec{K}}}_{\mathrm{r}}= & {} \left[ {{\begin{array}{ccc} {{\mathbf{K}}_{\mathrm{s}1} }&{} 0&{} 0 \\ 0&{} {{\mathbf{K}}_{\mathrm{s}2} }&{} 0 \\ 0&{} 0&{} {{\mathbf{K}}_{\varvec{\uptheta }} } \\ \end{array} }} \right] \nonumber \\ {{\varvec{M}}}_{\mathrm{s}1}= & {} \int _0^{L_{\mathrm{s}} } [\rho A{{\varvec{X}}}^{\mathrm{T}}(z){{\varvec{X}}}(z)+J_{\mathrm{d}}{{\varvec{X}}}^{{'}^{\mathrm{T}}}(z){{\varvec{X}}}^{'}(z)\nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z) \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'}(z)\nonumber \\&+J_{\mathrm{d}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z)]\hbox {d}z \end{aligned}$$(36)$$\begin{aligned} {{\varvec{M}}}_{\mathrm{s}2}= & {} \int _0^{L_{\mathrm{s}} } \left[ \rho A{{\varvec{Y}}}^{\mathrm{T}}(z){{\varvec{Y}}}(z)+J_{\mathrm{d}}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'}(z)\right. \nonumber \\&\left. +J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z)\right] \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'}(z)\nonumber \\&+J_{\mathrm{d}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z)\hbox {d}z \end{aligned}$$(37)$$\begin{aligned} {M}_\theta= & {} I_{\mathrm{s}} \int _0^{L_{\mathrm{s}}} {{\varvec{\varPhi }}^{\mathrm{T}}{\varvec{\varPhi }}} \hbox {d}z \end{aligned}$$(38)$$\begin{aligned} {{\varvec{G}}}_{\mathrm{s}1}= & {} \int _0^{L_{\mathrm{s}} } \left[ J_{\mathrm{p}} {{\varvec{X}}}^{{'}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'}(z)\right. \nonumber \\&\left. +J_{\mathrm{p}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z)\right. \nonumber \\&\left. +J_{\mathrm{p}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'}(z)\right. \nonumber \\&\left. +J_{\mathrm{p}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z)\right] \hbox {d}z \end{aligned}$$(39)$$\begin{aligned} {{\varvec{G}}}_{\mathrm{s}2}= & {} \int _0^{L_{\mathrm{s}} } \left[ -J_{\mathrm{p}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z)\right. \nonumber \\&\left. -J_{\mathrm{p}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'}(z)\right. \nonumber \\&\left. -J_{\mathrm{p}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z)\right. \nonumber \\&\left. -J_{\mathrm{p}} {{\varvec{Y}}}^{{'}^{\mathrm{T}}}(z){{\varvec{X}}}^{'}(z)\right] \hbox {d}z \end{aligned}$$(40)$$\begin{aligned} {{\varvec{M}}}_{\mathrm{d}1}= & {} m_{\mathrm{d}} {{\varvec{X}}}^{\mathrm{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}\left( {z_{\mathrm{d}} } \right) +J_{\mathrm{d}} {{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \left( \frac{EI}{\kappa AG}\right) ^{{2}}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) \end{aligned}$$(41)$$\begin{aligned} {{\varvec{M}}}_{\mathrm{d}2}= & {} m_{\mathrm{d}} {{\varvec{Y}}}^{\mathrm{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}\left( {z_{\mathrm{d}} } \right) +J_{\mathrm{d}} {{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{d}} \left( \frac{EI}{\kappa AG}\right) ^{\hbox {2}}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \end{aligned}$$(42)$$\begin{aligned} {{\varvec{G}}}_{\mathrm{d}1}= & {} J_{\mathrm{z}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{z}} \left( \frac{EI}{\kappa AG}\right) ^{{2}}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_\mathrm{z} {{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&+J_{\mathrm{z}} \frac{EI}{\kappa AG}{{\varvec{X}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{'''}\left( {z_{\mathrm{d}} } \right) \end{aligned}$$(43)$$\begin{aligned} {{\varvec{G}}}_{\mathrm{d}2}= & {} -J_{\mathrm{z}} \left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) \nonumber \\&-J_{\mathrm{z}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) \nonumber \\&-J_{\mathrm{z}} \frac{EI}{\kappa AG}{{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) \nonumber \\&-J_{\mathrm{z}} {{\varvec{Y}}}^{{'}^{\mathrm{T}}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) \end{aligned}$$(44)$$\begin{aligned} {{\varvec{K}}}_{\mathrm{s}1}= & {} \int _0^{L_{\mathrm{s}} } \left[ EI{{\varvec{X}}}^{{''}^{\mathrm{T}}}(z){{\varvec{X}}}^{''}(z)\right. \nonumber \\&\left. +\left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{X}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{X}}}^{'''}(z)\right] \hbox {d}z \end{aligned}$$(45)$$\begin{aligned} {{\varvec{K}}}_{\mathrm{s}2}= & {} \int _0^{L_{\mathrm{s}} } \left[ EI{{\varvec{Y}}}^{{''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{''}(z)\right. \nonumber \\&\left. +\left( \frac{EI}{\kappa AG}\right) ^{2}{{\varvec{Y}}}^{{'''}^{\mathrm{T}}}(z){{\varvec{Y}}}^{'''}(z)\right] \hbox {d}z \end{aligned}$$(46)$$\begin{aligned} {{\varvec{K}}}_{\varvec{\theta }}= & {} G_{\mathrm{s}} J_{\mathrm{s}} \int _0^{L_{\mathrm{s}} } {\varvec{\varPhi }}{{'}^{\mathrm{T}}}{\varvec{\varPhi }}^{'} \hbox {d}z \end{aligned}$$(47)
Appendix 2: Vectors and matrices related to the blade
-
(1)
Expression of discrete kinetic energy of \(i^{\mathrm{th}}\) blade can be shown as follows
$$\begin{aligned} T_{\mathrm{b}}= & {} \frac{1}{2}\rho _{\mathrm{b}} A_{\mathrm{b}} \int _0^{L_{\mathrm{b}} } {\dot{{\varvec{\eta }}}^{\mathbf{T}}{{\varvec{X}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{X}}}\left( {z{ }_{\mathrm{d}}} \right) \dot{{\varvec{\eta }}}} \nonumber \\&+\dot{{\varvec{\xi }}}^{\mathbf{T}}{{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) \dot{{\varvec{\xi }} }+\dot{{{\varvec{q}}}}_\mathbf{u}^{\mathbf{T}} {\varvec{\varPsi }}^{\mathbf{T}}{\varvec{\varPsi }} \dot{{{\varvec{q}}}}_\mathbf{u}\nonumber \\&+\dot{{{\varvec{q}}}}_\mathbf{u}^{\mathbf{T}} {\varvec{\varPsi }} ^{\mathbf{T}}{\varvec{\varPsi }} \dot{{{\varvec{q}}}}_{{{\varvec{u}}}} +\dot{{{\varvec{q}}}}_\mathbf{v}^{\mathbf{T}} {{\varvec{V}}}^{\mathbf{T}}{{\varvec{V}}}\dot{{{\varvec{q}}}}_\mathbf{v}\nonumber \\&+\dot{{{\varvec{q}}}}_{\varvec{\uptheta }}^{\mathbf{T}} \left( {R+x} \right) ^{2}{\varvec{\varPhi }}^{\mathbf{T}}{\varvec{\varPhi }} \dot{{{\varvec{q}}}}_{\varvec{\theta }} +{{\varvec{q}}}_\mathbf{u}^{\mathbf{T}} \dot{\psi }^{2}{\varvec{\varPsi }}^{\mathbf{T}}{\varvec{\varPsi }} {{\varvec{q}}}_{{{\varvec{u}}}} \nonumber \\&+{{\varvec{q}}}_{{\varvec{v}}}^{\mathbf{T}} \dot{\psi }^{2}{{\varvec{V}}}^{\mathbf{T}}{{\varvec{V}}}{{\varvec{q}}}_\mathbf{v} +{{\varvec{q}}}_{\varvec{\theta }}^{\mathbf{T}} \left( {R+x} \right) ^{2}\dot{\psi }^{2}{\varvec{\varPhi }}^{\mathbf{T}}{\varvec{\varPhi }} {{\varvec{q}}}_{\varvec{\theta }}\nonumber \\&-2\dot{{\varvec{\eta }}}^{\mathbf{T}}{{\varvec{X}}}^{\mathbf{T}}{{\varvec{V}}}\sin \psi \dot{{{\varvec{q}}}}_{{{\varvec{v}}}} \nonumber \\&+2\dot{{{\varvec{q}}}}_{\mathbf{v}}^{\mathbf{T}} \left( {R+x} \right) {{\varvec{V}}}^{\mathbf{T}}{\varvec{\varPhi }} \dot{{\varvec{q}}}_{\varvec{\theta }} +2\dot{{\varvec{\eta }}}^{\mathbf{T}}{{\varvec{X}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPsi }} \cos \psi \dot{{{\varvec{q}}}}_{{\varvec{u}}}\nonumber \\&+2\dot{{\varvec{\xi }}}^{\mathbf{T}}{{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPsi }} \sin \psi \dot{{{\varvec{q}}}}_{{\varvec{u}}}\nonumber \\&-2\dot{{\varvec{\eta }}}^{\mathbf{T}}\left( {R+x} \right) {{\varvec{X}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPhi }} \sin \psi \dot{{{\varvec{q}}}}_{\varvec{\theta }} \nonumber \\&+2\dot{{\varvec{\xi }}}^{\mathbf{T}}\left( {R+x} \right) {{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPhi }} \cos \psi \dot{{{\varvec{q}}}}_{\varvec{\theta }} \nonumber \\&+\dot{{\varvec{\eta }}}^{\mathbf{T}}\left( {R+x} \right) ^{2}\left\{ \left[ {{{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) +\frac{EI}{\kappa GA}{{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) } \right] ^{\mathrm{T}}\right. \nonumber \\&\left. \left[ {{{\varvec{X}}}^{'}\left( {z_{\mathrm{d}} } \right) +\frac{EI}{\kappa GA}{{\varvec{X}}}^{'''}\left( {z_{\mathrm{d}} } \right) } \right] \right\} \dot{{\varvec{\eta }}}\nonumber \\&-2\dot{{{\varvec{q}}}}_\mathbf{u}^{\mathbf{T}} \dot{\psi }{\varvec{\varPsi }}^{\mathbf{T}}{{\varvec{V}}}{{\varvec{q}}}_{{\varvec{v}}} +2\dot{{{\varvec{q}}}}_{{\varvec{v}}}^\mathbf{T} \dot{\psi }{{\varvec{V}}}^{\mathbf{T}}{\varvec{\varPsi }} {{\varvec{q}}}_{{\varvec{u}}}\nonumber \\&-2\dot{{\varvec{\eta }}}^{\mathbf{T}}\dot{\psi }{{\varvec{X}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPsi }} \sin \psi {{\varvec{q}}}_{{\varvec{u}}} \nonumber \\&-2\dot{{\varvec{\eta }}}^{\mathbf{T}}\dot{\psi }{{\varvec{X}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{V}}}\,\cos \psi {{\varvec{q}}}_{{\varvec{v}}} \nonumber \\&+2\dot{{\varvec{\xi }}}^{\mathbf{T}}\dot{\psi }{{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPsi }} \cos {\psi } {{\varvec{q}}}_{{\varvec{u}}} -2\dot{{\varvec{\xi }}}^{\mathbf{T}}\dot{\psi }{{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{V}}}\sin \psi {{\varvec{q}}}_{{\varvec{v}}}\nonumber \\&-2\dot{{\varvec{\eta }}}^{\mathbf{T}}\dot{\psi }\left( {R+x} \right) {{\varvec{X}}}^{\mathbf{T}}{\varvec{\varPhi }} \cos {\psi } {{\varvec{q}}}_{\varvec{\theta }}\nonumber \\&-2\dot{{\varvec{\xi }}}^{\mathbf{T}}\dot{\psi }\left( {R+x} \right) {{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {\varvec{\varPhi }} \sin \psi {{\varvec{q}}}_{\varvec{\theta }}\nonumber \\&+4\dot{{{\varvec{q}}}}_{\varvec{\theta }}^{\mathbf{T}} \dot{\psi }\left( {R+x} \right) {\varvec{\varPhi }} ^{\mathbf{T}}{\varvec{\varPsi }} {{\varvec{q}}}_{{\varvec{u}}} +2\dot{{\varvec{\xi }}}^{\mathbf{T}}{{\varvec{Y}}}^{\mathbf{T}}\left( {z_{\mathrm{d}} } \right) {{\varvec{V}}}\,\cos \psi \dot{{{\varvec{q}}}}_{{\varvec{v}}}\nonumber \\ \end{aligned}$$(48) -
(2)
Expression of discrete kinetic energy of \(i^{th}\) blade can be expressed as
$$\begin{aligned} U_{\mathrm{b}}= & {} \frac{1}{2}E_{\mathrm{b}} A_{\mathrm{b}} \int _0^{L_{\mathrm{b}} } {{{\varvec{q}}}_{\mathrm{u}}^{\mathbf{T}} {\varvec{\varPsi }}^{{'}^{\mathbf{T}}}{\varvec{\varPsi }}^{'}{{\varvec{q}}}_{{\varvec{u}}} \hbox {d}x} \nonumber \\&+\frac{1}{2}E_{\mathrm{b}} I_{\mathrm{b}} \int _0^{L_{\mathrm{b}} } {{{\varvec{q}}}_{{\varvec{v}}}^{\mathbf{T}} {{\varvec{V}}}^{{''}^{\mathbf{T}}}{{\varvec{V}}}^{''}{{\varvec{q}}}_{{\varvec{v}}} } \hbox {d}x \nonumber \\&+\frac{1}{4}{{\varvec{q}}}_{{\varvec{v}}}^{\mathbf{T}} \rho _{\mathrm{b}} A_{\mathrm{b}} \dot{\psi }^{2}\int _0^{L_{\mathrm{b}} } \left[ L_{\mathrm{b}}^2 -x^{2}\right. \nonumber \\&\left. +2R\left( {L_{\mathrm{b}} -x} \right) \right] {{\varvec{V}}}^{{'}^{\mathbf{T}}}{{\varvec{V}}}^{'} \hbox {d}x{{\varvec{q}}}_{{\varvec{v}}} \end{aligned}$$(49) -
(3)
The specific meaning of each transformation matrix of blade can be obtained as following
$$\begin{aligned} {{\varvec{A}}}_\mathbf{0}= & {} \left[ {{\begin{array}{ccc} {\cos \theta _{\mathrm{T}} }&{} {-\sin \theta _{\mathrm{T}} }&{} 0 \\ {\sin \theta _{\mathrm{T}} }&{} {\cos \theta _{\mathrm{T}} }&{} 0 \\ 0&{} 0&{} 1 \\ \end{array} }} \right] \\ {{\varvec{A}}}_\mathbf{1}= & {} \left[ {{\begin{array}{ccc} {\cos \psi }&{} {-\sin \psi }&{} 0 \\ {\sin \psi }&{} {\cos \psi }&{} 0 \\ 0&{} 0&{} 1 \\ \end{array} }} \right] \\ {{\varvec{A}}}_\mathbf{2}= & {} \left[ {{\begin{array}{ccc} 1&{} 0&{} 0 \\ 0&{} {\cos \theta _y }&{} {-\sin \theta _y } \\ 0&{} {\sin \theta _y }&{} {\cos \theta _y } \\ \end{array} }} \right] \\ {{\varvec{A}}}_3= & {} \left[ {{\begin{array}{ccc} {\cos \theta _x }&{} 0&{} {\sin \theta _x } \\ 0&{} 1&{} 0 \\ {-\sin \theta _x }&{} 0&{} {\cos \theta _x } \\ \end{array} }} \right] \end{aligned}$$
where \(\psi =\Omega t+\left( {i-1} \right) {2\pi }/{N_{\mathrm{b}} }\), and \(\left( {i-1} \right) {2\pi }/{N_{\mathrm{b}}}\) indicates the position of the \(i^{\mathrm{th}}\) blade in the blade; \(N_{\mathrm{b}}\) is the number of blades, \(\theta _{\mathrm{T}}\) is the twist angle at disk hub, \(\theta _x\) and \(\theta _y\) are swinging angles of disk.
Appendix 3: Vectors and matrices related to the rotor–blade coupling system
-
(1)
\(q_{\mathrm{rb}}\) is generalized coordinate vector of rotor–blade coupling system.
$$\begin{aligned} q_{\mathrm{rb}} =\left[ {q_{\mathrm{r}} }\quad {q_\theta }\quad {q_{\mathrm{b}} } \right] ^{\mathrm{T}} \end{aligned}$$(50)where \(q_{\mathrm{r}}\) and \(q_\theta \) are vectors of translational and torsional degrees of freedom of rotor; \(q_{\mathrm{b}} \) is the vector of degrees of freedom of blade.
-
(2)
\(M_{\mathrm{rb}}\) is mass matrix of rotor–blade coupling system.
$$\begin{aligned} M_{\mathrm{rb}} =\left[ {{\begin{array}{ccc} {M_{\mathrm{r}} }&{} 0&{} {M_{\mathrm{sb}} } \\ 0&{} {M_\theta }&{} {M_{\theta \mathrm{b}} } \\ {M_{\mathrm{sb}}^\mathrm{T} }&{} M_{{\uptheta }\mathrm{b}}^{\mathrm{T}} &{} {M_{\mathrm{b}} } \\ \end{array} }} \right] \end{aligned}$$(51)where \(M_{\mathrm{r}}\) and \(M_\theta \) are vectors of translational and torsional mass matrix of rotor; \(M_{\mathrm{b}}\) is the vector of mass matrix of blade; \(M_{\theta \mathrm{b}}\) and \(M_{\mathrm{sb}}\) are coupling mass matrix of system.
-
(3)
\(C_{\mathrm{rb}}\) is damping matrix of rotor–blade system(including proportional damping and gyro matrix)
$$\begin{aligned} C_{\mathrm{rb}} =\left[ {{\begin{array}{ccc} {C_{\mathrm{r}} }&{} {C_{\mathrm{s}\theta } }&{} {C_{\mathrm{sb}} } \\ {C_{\mathrm{s}\theta }^{\mathrm{T}} }&{} {C_\theta }&{} {C_{\theta \mathrm{b}} } \\ {C_{\mathrm{sb}}^{\mathrm{T}} }&{} {C_{\theta \mathrm{b}}^{\mathrm{T}} }&{} {C_{\mathrm{b}} } \\ \end{array} }} \right] \end{aligned}$$(52)where \(C_{\mathrm{r}}\) and \(C_\theta \) are vectors of translational and torsional damping matrix of rotor; \(C_{\mathrm{b}}\) is the vector of damping matrix of blade; \(C_{\mathrm{s}\theta }\), \(C_{\mathrm{sb}}\) and \(C_{\theta \mathrm{b}}\) are coupling damping matrix of system.
-
(4)
\(K_{\mathrm{rb}}\) is stiffness matrix of rotor–blade coupling system
$$\begin{aligned} K_{\mathrm{rb}} =\left[ {{\begin{array}{ccc} {K_{\mathrm{r}} }&{} 0&{} 0 \\ 0&{} {K_\theta }&{} 0 \\ 0&{} 0&{} {K_{\mathrm{b}} } \\ \end{array} }} \right] \end{aligned}$$(53)
where \(K_{\mathrm{r}}\) and \(K_\theta \) are vectors of translational and torsional stiffness matrices of rotor; \(K_{\mathrm{b}}\) is the vector of stiffness matrix of blade.
Rights and permissions
About this article
Cite this article
Li, C., She, H., Tang, Q. et al. The effect of blade vibration on the nonlinear characteristics of rotor–bearing system supported by nonlinear suspension. Nonlinear Dyn 89, 987–1010 (2017). https://doi.org/10.1007/s11071-017-3496-z
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11071-017-3496-z