Abstract. Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant stresses is often unfeasible. A possible solution is to add an external source of damping, in the form of dry friction devices such as the under-platform damper. The relative movement between the blades causes possible slip between damper and blade surfaces. Due to the nonlinear nature of dry friction, dynamic analysis of structures constrained through frictional contacts is dffcult, commercial finite element codes using time step integration are not suitable given the large computation times. For this reason, ad hoc numerical codes have been developed in the frequency domain. Some authors [1{4] prefer a separate routine in order to c...
Friction dampers are commonly included into turbine designs to limit the turbine blades resonant vi...
In the machinery structures with joints the contact pressures at contact interfaces are usually high...
The complex architecture of aircraft engines requires demanding computational efforts to take into a...
Abstract. Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large r...
Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant st...
A crucial part of building reliable models for the design of under-platform dampers for turbine blad...
International audienceHigh-cycle fatigue caused by large resonance stresses remains one of the most ...
Dry friction devices such as underplatform dampers are commonly included in turbine bladed disks des...
Dry friction devices such as underplatform dampers are commonly included in turbine bladed disks des...
A two-dimensional microslip friction model with normal load variation induced by normal motion is pr...
Underplatform dampers are widely used to dissipate vibration energy and to further prevent high cycl...
Friction damping is one of the most exploited systems of passive control of the vibration of mechani...
Dry friction dampers are widely used to reduce vibration. The forced vibration response of a simplif...
Friction damping is one of the most exploited systems of passive control of vibration of mechanical ...
Underplatform dampers (UPDs) are widely used as a source of friction damping and are frequently inco...
Friction dampers are commonly included into turbine designs to limit the turbine blades resonant vi...
In the machinery structures with joints the contact pressures at contact interfaces are usually high...
The complex architecture of aircraft engines requires demanding computational efforts to take into a...
Abstract. Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large r...
Detuning of gas turbine blades in order to avoid high cycle fatigue failure due to large resonant st...
A crucial part of building reliable models for the design of under-platform dampers for turbine blad...
International audienceHigh-cycle fatigue caused by large resonance stresses remains one of the most ...
Dry friction devices such as underplatform dampers are commonly included in turbine bladed disks des...
Dry friction devices such as underplatform dampers are commonly included in turbine bladed disks des...
A two-dimensional microslip friction model with normal load variation induced by normal motion is pr...
Underplatform dampers are widely used to dissipate vibration energy and to further prevent high cycl...
Friction damping is one of the most exploited systems of passive control of the vibration of mechani...
Dry friction dampers are widely used to reduce vibration. The forced vibration response of a simplif...
Friction damping is one of the most exploited systems of passive control of vibration of mechanical ...
Underplatform dampers (UPDs) are widely used as a source of friction damping and are frequently inco...
Friction dampers are commonly included into turbine designs to limit the turbine blades resonant vi...
In the machinery structures with joints the contact pressures at contact interfaces are usually high...
The complex architecture of aircraft engines requires demanding computational efforts to take into a...