Ventilation Fan Aeroelastic Analysis

Slides:



Advertisements
Similar presentations
Pipe fluid-elastics. Fluid-elasticity of a fluid-conveying pipe
Advertisements

FIGURE 5.1 Potentiometric displacement sensor.
LINFLOW 1.4 The Company.
In this work the question was, why did the fan fail in fatigue during
Local Customization Chapter 2. Local Customization 2-2 Objectives Customization Considerations Types of Data Elements Location for Locally Defined Data.
Acoustic-Structural Interaction in a Tuning Fork
Control calculations Heat Engines & Boilers.
1 PowerPoint Objective 4: Creating Charts and Tables Microsoft Office Specialist 2010 Certification Prep Story/Walls.
Chapter 3 Logic Gates.
ECE201 Lect-41 Sinusoids (8.1); Phasors (8.3); Complex Numbers (Appendix) Dr. Holbert January 30, 2006.
1 / 13 Vibration analysis and noise reduction of the swinging unit Magyar Bálint (BME) A C R O B O T E R 3rd OSB meeting Reading, / 11 / 2007 Vibration.
Click Here to Begin. 1. The candle is _______ the present. on between over under.
EWEA Annual Event 2013 Vienna February, 4-7, 2013
Absorptive Muffler with Shells
DISPLACEMENT TRANSMISSIBILITY IN BASE EXCITATION
Flow Disturbance of Flow due to Bends and Obstacles, etc. Time Transients and Spatial Distribution of Fluid Force on Structure Surface FLAVOR-3D: 3-D Fluid.
Aeroelasticity : Complexities and Challenges in Rotary–Wing Vehicles
ASME 2002, Reno, January VIBRATIONS OF A THREE-BLADED WIND TURBINE ROTOR DUE TO CLASSICAL FLUTTER Morten Hartvig Hansen Wind Energy Department Risø.
SIEMENS, MUELHEIM 1 1 Fluid-Structure Interaction for Combustion Systems Artur Pozarlik Jim Kok FLUISTCOM SIEMENS, MUELHEIM, 14 JUNE 2006.
Basic bluff-body aerodynamics I
Simulating an Insect-Scale Flapping Wing Air Vehicle
Mechanical Vibrations Jeff Rhoads and Terry Ballinger MSU 2006.
Mechanical Vibrations
Aeroelastic Stability and Control of Large Wind Turbines
Design of Wind Turbines P M V Subbarao Professor Mechanical Engineering Department Selection of Optimal Geometrical & Kinematic Variables ….
Design Process Supporting LWST 1.Deeper understanding of technical terms and issues 2.Linkage to enabling research projects and 3.Impact on design optimization.
Study of Oscillating Blades from Stable to Stalled Conditions 1 CFD Lab, Department of Aerospace Engineering, University of Glasgow 2 Volvo Aero Corporation.
Tobias—July, 2015 Benjamin John Tobias Princeton Plasma Physics Laboratory with M. Chen 1, C.W. Domier 1, R. Fitzpatrick 2, B.A. Grierson 3, N.C. Luhmann,
Turbomachinery Lecture 5a Airfoil, Cascade Nomenclature
Buckling of Slender Columns ( )
A Survey of Aeroacoustic Considerations in Wind Turbines Robert Scott AE 6060.
ANALYSIS OF LATHE VIBRATION INFLUENCE ON BLANK ROUGHNESS TALLINN UNIVERSITY OF TECHNOLOGY Ph.D Gennady Aryassov, M. Sc. Tauno Otto, M. Sc. Svetlana Gromova.
Kamila Součková Cutting the Air 2.. Task When a piece of thread (e.g., nylon) is whirled around with a small mass attached to its free end, a distinct.
3 th International Symposium on Integrating CFD and Experiments in Aerodynamics U.S. Air Force Academy, CO, USA June 20-21, 2007 Integration of CFD and.
Along-wind dynamic response
Aeroelastic effects Wind loading and structural response Lecture 14 Dr. J.D. Holmes.
Fluid Dynamics How does conservation of mass apply in a fluid? How does conservation of energy apply in a fluid? What is laminar flow? What is turbulence.
ASCE Wind Loads SESSION 1-2 Wind Engineering Theory: Bluff Body Aerodynamics.
Modal Dynamics of Wind Turbines with Anisotropic Rotors Peter F
1 MIDTERM EXAM REVIEW. 2 m 081.SLDASM REVIEW Excitation force 50N normal to face k=10000N/m m=6.66kg Modal damping 5%
Modal Analysis-hw-04 The schematic diagram of a large cannon is shown below. When the gun is fired, high-pressure gases accelerate the projectile inside.
Bird Strike on Jet Fan. Introduction Modelling of Bird Strike using EUROPLEXUS Full Lagrangian Approach Bird modelled by SPH elements (porous gelatine.
J.Cugnoni, LMAF/EPFL,  Goal: ◦ extract natural resonnance frequencies and eigen modes of a structure  Problem statement ◦ Dynamics equations (free.
BASICS OF DYNAMICS AND ASEISMIC DESIGN
Dynamics DYSTIFF s.r.o., Olomouc. Vertical pump - Variable speed of rotation - High level of vibration - Two eigenfrequencies in speed range.
UNDER THE GUIDANCE OF DR. P. V. MOHANRAM MR. C. SHANMUGAM ANALYSIS AND ISOLATION OF VIBRATION CHARACTERISTICS IN RECIPROCATING COMPRESSOR by N. Gopiselvam.
Date of download: 6/20/2016 Copyright © ASME. All rights reserved.
1 Turbopower Program Conference April 14-15, 2010, Linköping Compressor Technology WP1 Aero Forcing Florian Fruth, KTH
Date of download: 6/23/2016 Copyright © ASME. All rights reserved. From: Computational Fluid Dynamics Investigation of Turbulent Flow Inside a Rotary Double.
Date of download: 6/26/2016 Copyright © ASME. All rights reserved. Flutter of Variations on a 5 MW Swept Wind Turbine Blade 1 J. Sol. Energy Eng. 2016;138(2):
Aerodynamic Damping (WP2)
AAE 556 Aeroelasticity Lecture 28, 29,30-Unsteady aerodynamics 1 Purdue Aeroelasticity.
Tacoma Narrows Bridge Collapse
The information contained in this document is Volvo Aero Corporation Proprietary Information and it shall not – either in its original or in any modified.
Mechanical Vibrations
Short introduction to aeroelasticity
INVESTIGATION OF IDLING INSTABILITIES IN WIND TURBINE SIMULATIONS
Identifying the “wavemaker” of fluid/structure instabilities
Date of download: 10/22/2017 Copyright © ASME. All rights reserved.
AAE 556 Aeroelasticity Lectures 22, 23
Project COMP10: Designing for Blade Aeromechanical Integrity
Dynamic analysis of wind turbines subjected to Ice loads
Modeling tools for Rotordynamics and Bearings Tribodays 2017, Älvkarleby Niklas Rom, PhD © Copyright 2016 COMSOL. Any of.
Purdue Aeroelasticity
Date of download: 1/3/2018 Copyright © ASME. All rights reserved.
Vortex Induced Vibration in Centrifugal pump ( case study)
Purdue Aeroelasticity
ME321 Kinematics and Dynamics of Machines
Principles of Dynamics
Presentation transcript:

Ventilation Fan Aeroelastic Analysis Rotating Fan Stability Analysis. (Courtesy of FläktWoods AB, Sweden) LINFLOW 1.4

Ventilation Fan Modeling in LINFLOW Rotating Fan Stability Analysis. Twin blade fan model: Rotating at 987 rpm Inner radius 0.68 m Outer radius 1.02 m LINFLOW 1.4

Steady Flow Analysis of Rotating Fan Absolute Velocity Contours. LINFLOW 1.4

Structural Dynamic Analysis Rotating Fan Eigenmode table Structural model included fan blades + hub. Stability analysis was performed using the 8-10 first structural modes with the lowest natural frequencies. Structural model used LINFLOW 1.4

Ventilation Fan Aeroelastic Stability Analysis Aeroelastic Eigenfrequency Diagram Aeroelastic Damping Diagram One mode showed increasing damping requirements with increasing load, Which? LINFLOW 1.4

Ventilation Fan Stability Analysis Evaluation Unstable Mode Shape LINFLOW predicted an unstable 3.rd mode with a frequency of 382.6 Hz Measurements at full load later show that a maximum amplitude of vibration existed at 389 Hz LINFLOW 1.4

Ventilation Fan Experimental Response Evaluation Measurements at full load show that a maximum amplitude of vibration existed at 389 Hz 2 1 8 3 Measured frequency response diagram. LINFLOW 1.4

Ventilation Fan Unstable Mode Animation (Click on Picture for Animation) LINFLOW 1.4

Aeroelastic Instability Alleviation Can aeroelastic instabilities be eliminated or is it possible to raise the critical velocity? Yes,… … eliminate the source of elastic, inertial, and/or aerodynamic coupling. How? “Mass balance”-- add or redistributed mass to move the c.g. forward. Modify the vibration characteristics Increase spread between frequencies Avoid frequency rations of one or integer multiples Increase structural damping Eliminate sources of fluid-dynamic “forcing” such as vortex shedding or turbulence from wakes etc. LINFLOW 1.4

New Improved Ventilation Fan Geometry Aeroelastic improvements of the fan design Damping requirements for all aeroelastic modes now drop with increasing loading LINFLOW 1.4

New Ventilation Fan, Experimental Evaluation Measurements at full load on the aeroelasticly improved design show more then one order of magnitude lower stress levels on the fan surface. Measured frequency response diagram. (Return) LINFLOW 1.4