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Aeroelastic Renewable Energy System

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Flutter cut-in speed. Vibration frequency. Quantitative tri-axial force measurements ... Angular vs. Linear Magnet Model. Max Displacement (16 deg, 15mm) ... – PowerPoint PPT presentation

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Title: Aeroelastic Renewable Energy System


1
Aeroelastic Renewable Energy System
David Chesnutt, Adam Cofield, Dylan Henderson,
Jocelyn Sielski, Brian Spears, Sharleen Teal,
Nick Thiessen
1
2
AerodynamicsPrevious Work
  • Non-dimensional analysis completed
  • Compared different mathematical approaches to
    model AED system
  • Selected mathematical approach - Theodorsen
    Flutter Theory
  • Program writing started
  • Wind tunnel testing performed to qualitatively
    observe operational characteristics of AED and
    flutter frequency using triaxial load sensor

3
AerodynamicsCurrent Model
4
Aerodynamics Completed Testing
  • Purpose
  • Relationship between tension and flutter
    speed/frequency
  • Inputs
  • Nylon Fabric Belt (1x14)
  • Tested at 3 tensions (4.9N, 9.8N, 19.6N)
  • Outputs
  • Flutter cut-in speeds
  • Vibration frequency

Testing Assembly CAD Model
4
5
Aerodynamics Future Testing
  • Purpose
  • Obtain displacement functions
  • Calculate stresses and fatigue
  • Inputs
  • Steel foil belt (1x14)
  • Belt tension
  • Magnet Placement
  • Outputs
  • Flutter cut-in speed
  • Vibration frequency
  • Quantitative tri-axial force measurements

Testing Assembly Mounted in Wind Tunnel
5
6
AerodynamicsWork This Semester
  • Complete flutter program.
  • Test AED in wind tunnel to match analytical and
    theoretical results.
  • Incorporate magnetic forces into program.
  • Re-test AED in wind tunnel.

7
Power Conditioning System
  • Circuitry model follows forever flashlight

NightStar Physics Guide
http//www.foreverflashlights.com/micro_forever_fl
ashlights.htm
8
ElectromechanicsPrevious Work
  • Faction Aerodynamic force on belt
  • Freaction FbeltFcoil,1 Fcoil,2
  • Use Newtons Second Law of Motion to establish
    link between Lorentz forces and aerodynamic
    forces
  • Equation shows relationship between induced
    voltage and circuit current
  • Current is needed to find Lorentz Forces

9
ElectromechanicsPrevious Work
  • Developed magnetic circuit diagram to help
    determine flux through coils
  • Not adequate for complex system
  • Would require too many assumptions

10
ElectromechanicsPrevious Work
  • Linked cores increases magnetic flux between
    coils
  • Should increase change in flux through coils
  • Greater flux change is proportional to induced
    voltage and power increases

11
Angular vs. Linear Magnet Model
  • Small Displacement (4 deg, 3.75mm)

Note Difference in Analytical Models
12
Angular vs. Linear Magnet Model
  • Medium Displacement (8 deg, 7.5mm)

Note Difference in Analytical Models
13
Angular vs. Linear Magnet Model
  • Large Displacement (12 deg, 11.25mm)

Note Difference in Analytical Models
14
Angular vs. Linear Magnet Model
  • Max Displacement (16 deg, 15mm)

Note Difference in Analytical Models
15
Parameters
  • Belt Material Parameters
  • Density, MOE
  • Belt Configuration Parameters
  • Length, Width, Thickness, Mag. Placement, Tension
  • Power Generation Parameters
  • Coil/Core Parameters, Gap, Magnet Parameters

16
Parameters Optimization and Selection
  • Two or three parameters will be chosen for
    optimization
  • All other parameters will be selected by
    mathematical method and/or available materials
  • Final prototype design will also dictate
    selection to some extent

17
Parameters Likely Selections
  • Most likely to be selected mathematically or due
    to availability
  • Belt material
  • Belt length
  • Coil/core
  • Magnet parameters
  • Most likely to remain variable
  • Belt width
  • Thickness
  • Tension
  • Magnet placement
  • Magnet gap

Goal Narrow parameters down just to belt width,
tension, and gap
18
Timeline Spring 2009
19
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