Innovations in the On-site Manufacturing of Tall Wind Turbine Towers
Transcript of Innovations in the On-site Manufacturing of Tall Wind Turbine Towers
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Innovations in the On-site Manufacturing of Tall Wind Turbine Towers
Andrew T. Myers, PhD, PE
Assistant Professor of Civil Engineering
Northeastern University
Mass Wind Working Group Meeting
September 30, 2015
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Outline
• Background
• Research Needs and Project Goals
• Large-scale Experiments
• Imperfections
• Strength
• Buckling characteristics
• Complementary GMNIA analyses
• Future Work
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Background
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• Wind generated-energy in the Great Plains among the cheapest energy sources in the country.
• Elsewhere, harvesting wind energy becomes economical only at higher elevations.
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Can
• Predominant wind tower design is a slender steel monopole with diameter-to-thickness (D/t) ratios, ~100-300.
• Utility-scale towers are tapered.
• Manufactured by “can-welding.”
Bolted
Flange
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Optimal Tower Base Diameter
Transportable Tower Base Diameter
• Great! Let’s make taller towers!
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Patent:US8720153…
• One innovative solution, patented by Keystone Tower Systems, is to make tapered tubes with automated spiral welding.
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Research Needs and Project Goals
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QC C
QC B
QC A
DC 71
80
90
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Ultimate Moment = 160 MN-m Damage Equiv. Moment = 40 MN-m (at 1e7 cycles; m = 4)
Base cross-section designed to EN 1993-1-6 for typical base loads of 140m, 3MW tower:
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Today, fatigue controlled
If free of constraints, shift to buckling controlled
QC C
QC B
QC A
DC 71
80
90
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Optimal Tower Base Diameter
Transportable Tower Base Diameter
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Need to understand buckling for flexure and high D/t
D/t = 397
D/t = 302
D/t = 222
QC C
QC B
QC A
DC 71
80
90
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Buckling of a wind tower
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Current State of Affairs • As steel tubular towers become taller with larger base
diameters, the buckling limit state becomes more important and tower sections become more slender.
• No AISC design equation for moment strength of very slender circular hollow sections (l > 0.45).
• Eurocode provides equation, but, at high slenderness, it is based on compression tests not bending.
• Insufficient test data to justify bending design equation.
• Buckling of circular hollow sections is highly imperfection sensitive.
• Eurocode’s GMNIA method is promising, but challenging.
• Need for large-scale tests, imperfection measurements and complementary GMNIA simulations.
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• Validate Eurocode buckling for:
• High D/t
• Flexure
• Imperfection field from new manufacturing process
• Develop GMNIA protocols to enable greater optimization.
• Establish basis for design in the U.S.
Project Goals
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Initial imperfection scan
(laser, full 3d)
Ultimate load testing in flexure
Load curve (moment v. rotation)
GMNIA FEA
Project Goals
Simultaneous surface scan
(laser, compression face)
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Large-scale Experiments
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Spec. #
Min D/t [-]
Max D/t [-]
Dmin [mm]
Dmax
[mm] Gauge
t [mm]
L [m]
α [-]
1 195 224 663 762 10 3.40 3.43 0.83°
2 127 139 815 892 -- 6.43 3.37 0.65°
3 235 260 812 897 10 3.45 3.38 0.76°
4 283 308 864 940 11 3.05 3.40 0.82°
5 283 308 864 940 11 3.05 3.38 0.82°
6 283 308 864 940 11 3.05 3.40 0.82°
7 316 350 965 1067 11 3.05 3.40 0.86°
8 316 350 965 1067 11 3.05 3.40 0.86°
9 316 350 965 1067 11 3.05 3.40 0.86°
10* 68 154 800 975 -- 6.35 3.40 0.90°
Test Matrix
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Overview
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• Specimens #1-4 and #6-7 finished
• Specimens #5, #8-10 will be tested this fall
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Spec. #
Min D/t [-]
Max D/t [-]
Dmin [mm]
Dmax
[mm] Gauge
t [mm]
L [m]
α [-]
1 195 224 663 762 10 3.40 3.43 0.83°
2 127 139 815 892 -- 6.43 3.37 0.65°
3 235 260 812 897 10 3.45 3.38 0.76°
4 283 308 864 940 11 3.05 3.40 0.82°
5 283 308 864 940 11 3.05 3.38 0.82°
6 283 308 864 940 11 3.05 3.40 0.82°
7 316 350 965 1067 11 3.05 3.40 0.86°
8 316 350 965 1067 11 3.05 3.40 0.86°
9 316 350 965 1067 11 3.05 3.40 0.86°
10* 68 154 800 975 -- 6.35 3.40 0.90°
Test Matrix
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Spec 2
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Spec. #
Min D/t [-]
Max D/t [-]
Dmin [mm]
Dmax
[mm] Gauge
t [mm]
L [m]
α [-]
1 195 224 663 762 10 3.40 3.43 0.83°
2 127 139 815 892 -- 6.43 3.37 0.65°
3 235 260 812 897 10 3.45 3.38 0.76°
4 283 308 864 940 11 3.05 3.40 0.82°
5 283 308 864 940 11 3.05 3.38 0.82°
6 283 308 864 940 11 3.05 3.40 0.82°
7 316 350 965 1067 11 3.05 3.40 0.86°
8 316 350 965 1067 11 3.05 3.40 0.86°
9 316 350 965 1067 11 3.05 3.40 0.86°
10* 68 154 800 975 -- 6.35 3.40 0.90° 24
Test Matrix
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Spec 10
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• Pure bending, pure compression and bending-compression
• 3300 kN-m max moment
• 10° max end rotation
• 3000 kN max tension, 2000 kN max compression
• Specimen welded to 100 mm thick end plates
Actuator
Actuator
Specimen
Pin
Slotted Pin
Baseplate
Baseplate
Crossbeam
Crossbeam
Dmin
Dmax
Cross weld Orientation
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Imperfections amplified 20x; Both specimens ~1m in diameter, ~3m long
Tapered spiral welded (Specimen #4)
Initial Imperfection Scans
Can welded (Specimen #10)
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Simultaneous Surface Scan
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Specimen 4 Results
I
II
III
End
Spec. #
Min D/t [-]
Max D/t [-]
Dmin [mm]
Dmax
[mm] Gauge
t [mm]
L [m]
α [-]
4 283 308 864 940 11 3.05 3.40 0.82°
• Eurocode QC strengths calculated for “equivalent” diameter
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Specimen 4 Results – Load Drop I • First test to buckle simultaneously at three different cross-sections.
Buckling initiated near the end with minimum diameter.
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Pre-buckling
Pre-test
Load drop I
Specimen 4 Results – Load Drop I
Dmax
Dmin
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I
II
III
Specimen 4 Results
End
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Specimen 4 Results – Load Drop II
• Additional buckling waves on bottom of the second and third sheets
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I
II
III
Specimen 4 Results
End
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Specimen 4 Results – Load Drop III
• Additional buckling waves on top of the fifth sheet
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I
II
III
Specimen 4 Results
End
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Specimen 4 Results – End
• Buckling pattern somewhat helical in reverse direction as weld
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GMNIA Analyses – Convergence Study • S4R elements in ABAQUS.
• Nonlinear collapse analysis with Rik’s Solver.
• Convergence study on shell element type, aspect ratio, size, orientation (aligned with helix vs normal) and loading (pure compression vs bending).
• Results showed convergence for S4R elements, 1:1 aspect ratio, element size = ~0.5 𝑅𝑡, elements oriented normally and bending.
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GMNIA Results – Specimen 4
• GMNIA results shown for S4R elements, 1:1 aspect ratio, element
size = ~0.5 𝑅𝑡, elements oriented normally, bending
• Measured imperfections
• Idealized boundary conditions
• Measured material properties (idealized as bilinear with
yield plateau)
• Contours of Von Mises stress
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GMNIA Results – Specimen 4
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Future Work
• More large-scale tests.
• Probabilistic assessment of initial imperfections.
• FEA sensitivity study of imperfections.
• Combining tests and FEA to develop design equations and FEA protocols for high slenderness steel tubes subject to flexure.
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Collaborators
• Eric Smith, Keystone Tower Systems
• Ben Schafer, JHU
• Angelina Jay, NEU
• Robert Rosa, NEU
• Shahab Torabian, JHU
• Abdullah Mahmoud, JHU
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Acknowledgements
• NEU STReSS Lab
• Funding by:
• NSF grant CMMI-1334122
• NSF SBIR and DOE SBIR
• Mass Clean Energy Center
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