Combined preliminary–detailed design of wind turbines
This paper is concerned with the holistic optimization of wind turbines. A multi-disciplinary optimization procedure is presented that marries the overall sizing of the machine in terms of rotor diameter and tower height (often termed “preliminary design”) with the detailed sizing of its aerodyn...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Copernicus Publications
2016-05-01
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Series: | Wind Energy Science |
Online Access: | https://www.wind-energ-sci.net/1/71/2016/wes-1-71-2016.pdf |
Summary: | This paper is concerned with the holistic optimization of wind turbines. A
multi-disciplinary optimization procedure is presented
that marries the overall sizing of the machine in terms of rotor diameter
and tower height (often termed “preliminary design”) with the
detailed sizing of its aerodynamic and structural
components. The proposed combined preliminary–detailed approach sizes the
overall machine while taking into full account the subtle and complicated
couplings that arise due to the mutual effects of aerodynamic and
structural choices. Since controls play a central role in
dictating performance and loads, control laws are also updated accordingly
during optimization. As part of the approach, rotor and tower are sized
simultaneously, even in this case capturing the mutual effects of one
component over the other due to the tip clearance constraint. The procedure, here driven by detailed models of the cost of energy, results in a complete aero-structural design of the machine, including its associated control
laws.
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The proposed methods are tested on the redesign of two wind turbines, a
2.2 MW onshore machine and a large 10 MW offshore one. In both cases, the
optimization leads to significant changes with respect to the initial
baseline configurations, with noticeable reductions in the cost of energy.
The novel procedures are also exercised on the design of
low-induction rotors for both considered wind turbines, showing that they
are typically not competitive with conventional high-efficiency rotors. |
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ISSN: | 2366-7443 2366-7451 |