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Title: 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 F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05B - INDEXING SCHEME RELATING TO MACHINES OR ENGINES OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, TO WIND MOTORS, TO NON-POSITIVE DISPLACEMENT PUMPS, AND TO GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY
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}
}