Nothing Special   »   [go: up one dir, main page]

Rossi et al., 2021 - Google Patents

High efficiency active damping on a fan rotor blade in case of resonant vibrations by means of piezoelectric actuators

Rossi et al., 2021

Document ID
5858979006934289873
Author
Rossi A
Botta F
Giovannelli A
Belfiore N
Publication year
Publication venue
Turbo Expo: Power for Land, Sea, and Air

External Links

Snippet

Severe resonant vibration is one of the main roots of turbomachinery blades failure. Forced response issues arise when the blades work in non-uniform flow fields. As a result unsteady aerodynamic pressures occur on the surfaces of the blade. If the frequency of the …
Continue reading at asmedigitalcollection.asme.org (other versions)

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/26Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F04POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/671Measures to reduce the propulsor weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F04POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator

Similar Documents

Publication Publication Date Title
Chiang et al. An analysis system for blade forced response
Petrov Analysis of flutter-induced limit cycle oscillations in gas-turbine structures with friction, gap, and other nonlinear contact interfaces
Rossi et al. A novel approach to reduce fan rotor blades stress in case of resonance due to inlet flow distortion by means of piezoelectric actuators
Im et al. Detached eddy simulation of transonic rotor stall flutter using a fully coupled fluid-structure interaction
Колодяжна et al. Aeroelastic Characteristics of Rotor Blades of Last Stage of a Powerful Steam Turbine
Rossi et al. High efficiency active damping on a fan rotor blade in case of resonant vibrations by means of piezoelectric actuators
Stapelfeldt Advanced methods for multi-row forced response and flutter computations
Cheng et al. Prediction of stall inception in multi-stage compressors based on an eigenvalue approach
Fleeter et al. The Time-Variant Aerodynamic Response of a Stator Row Including the Effects of Airfoil Camber
Blocher et al. Time-Linearized Forced Response Analysis of a Counter Rotating Fan: Part I—Theoretical Concept of a Fully Time-Linear Forced Response Analysis
Hauptmann et al. Aerodynamic excitation analysis for variable tip gap
Peng Tip running clearances effects on tip vortices induced axial compressor rotor flutter
Tong et al. High fidelity transient forced response analysis of mistuned bladed disks under complex excitation and variable rotation speeds
Rzadkowski et al. Numerical Modelling of fluid-structure interaction in a turbine stage for 3D viscous flow in nominal and off-design regimes
Liu et al. Improving the aero-elastic stability of bladed disks through parallel piezoelectric network
Kaneko et al. Effect of material damping of steam turbine vane on flutter suppression
Guerin et al. Thermomechanical component mode synthesis for blade casing interaction prediction
Li et al. Investigations on Unsteady Flow Excitation and Mechanical Performance of Last Turbine Stage Long Blade Using Fluid-Structure Interaction Method
Hsu A Study on Fluid Self‐Excited Flutter and Forced Response of Turbomachinery Rotor Blade
Kang et al. Rig Testing of the Operability of a Transonic Compressor Blade of an Industrial Gas Turbine
Breard et al. A non-linear integrated aeroelasticity method for the prediction of turbine forced response with friction dampers
Zhai et al. Aeroelastic Stability Assessment of an Industrial Compressor Blade Including Mistuning Effects
Berthillier et al. A numerical method for the prediction of bladed disk forced response
Rzadkowski et al. The Unsteady low-frequency aerodynamic forces acting on rotor blades in the first two stages of a jet engine axial compressor in the case of a bird strike
Биков et al. Effect of Blade Material of Steam Turbine Rotor on Aeroelastic Characteristics