desain turbine
TRANSCRIPT
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AAE 415 Aerodynamic Design
Final Project Presentation
Large Horizontal-Axis
Wind Turbine DesignTed Light
Jeff Robinson
December 13, 2003
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Outline
Background
Wind Energy & History
Types of Wind Turbines
Wind Turbine Aerodynamics
Design Process
Starting Point and Analysis Method
Results
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Wind Energy & History
Wind energy has been used
for thousands of years, for
sailing, pumping water,
grinding grain, etc.
In the early 1900s, windturbines were used to
produce direct electric
current to small areas
Oil Crisis of 1970s renewedinterest in wind turbines as a
cheap, clean, unlimited
source of energy
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Types of Wind Turbines
Darrius VerticalAxis Wind Turbine
Large HorizontalAxis Wind Turbine
Traditional Windmill
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Airfoil Aerodynamics
Wind = V0
Rotation = r*W
Relative Wind = W a
Wind Speed and Turbine Rotation must be
combined to find total velocity that airfoil sectionssee
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Desired Airfoil Qualities
For a fixed-pitch, constant speed machine,
recommended airfoil qualities at 0.75R are:
High L/D
Low clmax near tip reduces tendency to
overpower generator in high wind speeds
Insensitive to surface roughness (bugs, birds,
bullets)
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Design Process
CMARC used to analyze designs
Existing wind turbine with known geometry
and performance modeled for baseline
comparison
Assumed constant velocity generator
(Power) = (Moment)*(Rotation Rate)
Variation and Analysis of Designs
Geometric parameters modified
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Analysis Strategy
Start with an existing wind turbine, then
modify its geometry
Geometry varied
Airfoil section
Twist distribution
Chord distribution
Rotational rate, number of blades and
span were held constant
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Mod-2 Wind Turbine
Manufactured by Boeing in late 1970s
Development sponsored by NASA
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Mod-2 Wind Turbine Specifications
3.45 m 1.43 m
13.7 m
45.7 m
Diameter = 91.4 m
No. of Blades = 2 Average Wind Speed = 12.5 m/s
Rotation Rate = 17.5 rpm
Airfoil: NACA 23024
Power Output = 2.5 MW
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CMARC Inputs
Rotation rate about x-axis set to that of
Mod-2 wind turbine (17.5 rpm)
Many wind turbines are constant speed
Wind Speed set to local average wind
speed for Mod-2 (12.5 m/s)
Baseline geometry emulated Mod-2
geometry, then varied
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Results
r/R (1) (2) (3)
0 15 14 10
0.25 11.4 11.4 8
0.5 5.7 7 6
0.75 3.8 3.8 4
1 2.85 2.85 2
Chord Changes
r/R (1) (2) (3)
0 6.1 6.0 5.5
0.25 66.7 27.8 83.5
0.5 83.4 49.5 89
0.75 93.8 71.3 90
1 111.6 93.0 92
Twist Changes (values in deg from wind axis)
Mod-2 Baseline Model 5816 ---
Mod-A Airfoil Changed to NACA 651-012 5516 -12%
Mod-B Airfoil Changed to NACA 65-410 6179 15%
Mod-C Airfoil Changed to Althaus AH 93-W-145 2551 -131%
Mod-D Chord Change (1) from Mod-B with no sweep 8914 124%
Mod-E Chord Change (2) from Mod-B with no sweep 8442 105%
Mod-F Chord Change (3) from Mod-B with no sweep 7872 82%
Mod-G Chord Change (3) from Mod-B with sweep 9380 143%
Mod-H Twist Change (1) from Mod-G 10367 182%
Mod-I Twist Change (2) from Mod-G 7849 81%
Mod-J Twist Change (3) from Mod-G 7735 77%
Mod-2 Rating Published Power Rating 2500
Model # DescriptionPower (kW)
Dfrom
Baseline
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Results
Leading Edge
Root Section
Blade Tip
Airfoil NACA 65-410
r/R Chord (m) Twist (deg)0 10 6.1
0.25 8 66.7
0.5 6 83.4
0.75 4 93.8
1 2 111.6
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Cp Distribution
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Wake
for
Best
Blade
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Results
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Questions?