A dynamic model of the rotating shrouded blade is established, considering the shroud mass, the Coriolis force, and the centrifugal stiffening effect. And a macroslip model of dry friction with variable normal load is established to simulate the separation-contact-stick-slip state of the shroud. The Lagrangian equation is utilized to solve the differential motion equation, and the Galerkin method is used for discretization. The influence of shroud structure’s parameters such as rotational speed, contact angle, friction coefficient, clearance, and shroud position on the damping effect of the shroud is reviewed by means of amplitude-frequency response and energy through the Newmark-β numerical method. The results demonstrate that the damping ...
In order to study the effect of the dry friction damping structure on the localized vibration of mis...
This paper is aimed at modelling of friction effects in blade shrouding which are realized by means ...
Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant st...
The vibration characteristics of a bladed disk with the continuous ring type structure have been stu...
Vibration of a blade couple damped by a dry friction contact in the shroud is investigated by means ...
Actual trend in steam turbine design is to use blades with integral shrouds, for high pressure and i...
High-cycle fatigue is one of the most frequent reasons of failure for turbomachinery and in early de...
The damping potential of multiple friction contacts in a bladed disk is investigated. Friction conta...
Shroud devices which are typical cyclic symmetric structures are widely used to reduce the vibration...
Shrouds have been widely used to reduce the level of excessive vibration of blisks. However, complic...
The vibration dissipation mechanism of the rotating blade with a dovetail joint is studied in this p...
The nonlinear forced vibration responses of integrally shrouded turbine blade considering different ...
A dynamic model is proposed in this paper for analyzing the nonlinear characteristics of a flexible ...
This paper investigates the damping potential of strip dampers on a real turbine bladed disk. A 3D n...
This work focuses on efficient modelling and adaptive control of friction damping in bladed disks. T...
In order to study the effect of the dry friction damping structure on the localized vibration of mis...
This paper is aimed at modelling of friction effects in blade shrouding which are realized by means ...
Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant st...
The vibration characteristics of a bladed disk with the continuous ring type structure have been stu...
Vibration of a blade couple damped by a dry friction contact in the shroud is investigated by means ...
Actual trend in steam turbine design is to use blades with integral shrouds, for high pressure and i...
High-cycle fatigue is one of the most frequent reasons of failure for turbomachinery and in early de...
The damping potential of multiple friction contacts in a bladed disk is investigated. Friction conta...
Shroud devices which are typical cyclic symmetric structures are widely used to reduce the vibration...
Shrouds have been widely used to reduce the level of excessive vibration of blisks. However, complic...
The vibration dissipation mechanism of the rotating blade with a dovetail joint is studied in this p...
The nonlinear forced vibration responses of integrally shrouded turbine blade considering different ...
A dynamic model is proposed in this paper for analyzing the nonlinear characteristics of a flexible ...
This paper investigates the damping potential of strip dampers on a real turbine bladed disk. A 3D n...
This work focuses on efficient modelling and adaptive control of friction damping in bladed disks. T...
In order to study the effect of the dry friction damping structure on the localized vibration of mis...
This paper is aimed at modelling of friction effects in blade shrouding which are realized by means ...
Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant st...