Abstract
The phenomenon of vibration vector rotation caused by thermally induced unbalance changes, referred to as the “spiral vibration” (SV), is frequently observed in large rotating machinery. Since the SV is a consequence of an interaction between mechanical and thermal unbalance of the rotor, a set of standard rotordynamic equations must be extended by the additional thermal equation. For the case of rotor deformation caused by a hot spot on a slip ring of turbo-generator a new thermo-elastic model has been formulated. A solution for the thermal mode response of a simplified system has been derived analytically using the non-dimensional form of the thermal equation. This paper provides formulae for stability threshold and spiral period corresponding to the newly developed model of thermal excitation. The presented theoretical results have been adopted in more detailed numerical models and used to effectively extend stability margin of the SV in turbo-generator shaft trains.
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Notes
- 1.
It is assumed that \(p\) and \(q\) are very small numbers. Based on a comparison between simulation results and measured SV characteristics, estimated values for these parameters are in the range of 1e-5 and 1e-6. Consequently the circular frequency of vector rotation (see Eq. (11)) is much less than unity allowing to neglect the higher order derivatives of \(\varvec{\rho}_{\varvec{T}}\).
Abbreviations
- CCPP:
-
Combined cycle power plant
- HS:
-
Hot spot
- SSPT:
-
Single shaft power train
- SR:
-
Slip ring
- SV:
-
Spiral vibration
- \(\varvec{r} = x + jy\) :
-
Whirl (vibration vector) in stationary system
- \(\varvec{\rho}= u + jv\) :
-
Whirl (vibration vector) in rotating system
- \(\varvec{r}_{\varvec{T}} ,\varvec{ \rho }_{\varvec{T}}\) :
-
Thermal deflection of shaft (in stationary and rotating systems)
- \(p, q\) :
-
Dimensionless proportionality factors for added and eliminated heat
- \(p^{*} , q^{*}\) :
-
Proportionality factors for added and eliminated heat
- \(T_{S}\) :
-
Period of a spiral
- \(\varOmega\) :
-
Rotational speed of the shaft
- \(\eta =\Omega /\omega_{n}\) :
-
Normalized shaft angular speed
- \(\varepsilon\) :
-
Eccentricity of CG (Jeffcott rotor)
- k :
-
Linear shaft stiffness (Jeffcott rotor)
- m :
-
Concentrated mass of shaft (Jeffcott rotor)
- d :
-
Shaft damping (Jeffcott rotor)
- \(D = d/(2m\omega_{n} )\) :
-
Normalized shaft damping
- \(\omega_{n} = \surd (k/m)\) :
-
Natural frequency of undamped shaft (Jeffcott rotor)
- t :
-
Time
- \(z = \omega_{n} t\) :
-
Normalized time
- M :
-
Mass matrix
- D :
-
Damping matrix
- G :
-
Gyroscopic matrix
- K :
-
Stiffness matrix (rotor, support)
- \(\varvec{K}^{\varvec{R}}\) :
-
Stiffness matrix of a free-free rotor
- T :
-
Matrix transforming the thermal displacement in the location of HS into the thermal deformation of the whole shaft-line
- \(\varvec{r}_{{\varvec{T},\varvec{HS}}}\) :
-
Thermal deflection of shaft (in the location of HS)
- \(\varvec{r}_{{\varvec{HS}}}\) :
-
Total deflection of shaft (in the location of HS)
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Golebiowski, M., Nordmann, R., Knopf, E. (2015). A New Approach for Thermo-Elastic Equations to Predict Spiral Vibrations in Turbogenerator Shafts. In: Pennacchi, P. (eds) Proceedings of the 9th IFToMM International Conference on Rotor Dynamics. Mechanisms and Machine Science, vol 21. Springer, Cham. https://doi.org/10.1007/978-3-319-06590-8_186
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DOI: https://doi.org/10.1007/978-3-319-06590-8_186
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