Wind turbine blade with viscoelastic damping
Abstract
A wind turbine blade (60) damped by viscoelastic material (54, 54A-F) sandwiched between stiffer load-bearing sublayers (52A, 52B, 56A, 56B) in portions of the blade effective to damp oscillations (38) of the blade. The viscoelastic material may be located in one or more of: a forward portion (54A) of the shell, an aft portion (54D) of the shell, pressure and suction side end caps (54B) of an internal spar, internal webbing walls (54C, 54E), and a trailing edge core (54F).
- Inventors:
- Issue Date:
- Research Org.:
- SIEMENS ENERGY, INC. Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1338922
- Patent Number(s):
- 9541061
- Application Number:
- 14/195,935
- Assignee:
- SIEMENS ENERGY, INC. (Orlando, FL)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F02 - COMBUSTION ENGINES F02C - GAS-TURBINE PLANTS
F - MECHANICAL ENGINEERING F03 - MACHINES OR ENGINES FOR LIQUIDS F03D - WIND MOTORS
- DOE Contract Number:
- EE0005493
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2014 Mar 04
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 17 WIND ENERGY; 36 MATERIALS SCIENCE
Citation Formats
Sievers, Ryan A., and Mullings, Justin L. Wind turbine blade with viscoelastic damping. United States: N. p., 2017.
Web.
Sievers, Ryan A., & Mullings, Justin L. Wind turbine blade with viscoelastic damping. United States.
Sievers, Ryan A., and Mullings, Justin L. Tue .
"Wind turbine blade with viscoelastic damping". United States. https://www.osti.gov/servlets/purl/1338922.
@article{osti_1338922,
title = {Wind turbine blade with viscoelastic damping},
author = {Sievers, Ryan A. and Mullings, Justin L.},
abstractNote = {A wind turbine blade (60) damped by viscoelastic material (54, 54A-F) sandwiched between stiffer load-bearing sublayers (52A, 52B, 56A, 56B) in portions of the blade effective to damp oscillations (38) of the blade. The viscoelastic material may be located in one or more of: a forward portion (54A) of the shell, an aft portion (54D) of the shell, pressure and suction side end caps (54B) of an internal spar, internal webbing walls (54C, 54E), and a trailing edge core (54F).},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {1}
}
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