Turbine blade with tuned damping structure

Campbell, Christian X.; Messmann, Stephen J.

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A - human necessities
A01 - agriculture
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Title: Turbine blade with tuned damping structure

Abstract

A turbine blade is provided comprising: a root; an airfoil comprising an external wall extending radially from the root and having a radially outermost portion; and a damping structure. The external wall may comprise first and second side walls joined together to define an inner cavity of the airfoil. The damping structure may be positioned within the airfoil inner cavity and coupled to the airfoil so as to define a tuned mass damper.

Inventors:: Campbell, Christian X.; Messmann, Stephen J.

Issue Date:: Tue Sep 01 00:00:00 EDT 2015

Research Org.:: Siemens Energy, Inc., Orlando, FL (United States)

Sponsoring Org.:: USDOE

OSTI Identifier:: 1213468

Patent Number(s):: 9121288

Application Number:: 13/464,108

Assignee:: Siemens Energy, Inc. (Orlando, FL)

Patent Classifications (CPCs):: F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES

F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

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F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F01D5/16 - for counteracting blade vibration
F01D5/20 - Specially-shaped blade tips to seal space between tips and stator {

F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
F05D2300/6033 - Ceramic matrix composites [CMC]

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DOE Contract Number:: FC26-05NT42644

Resource Type:: Patent

Resource Relation:: Patent File Date: 2012 May 04

Country of Publication:: United States

Language:: English

Subject:: 17 WIND ENERGY

Citation Formats


                    Campbell, Christian X., and Messmann, Stephen J. Turbine blade with tuned damping structure.  United States: N. p., 2015. 
        Web.

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                    Campbell, Christian X., & Messmann, Stephen J. Turbine blade with tuned damping structure.  United States.

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                    Campbell, Christian X., and Messmann, Stephen J. Tue .  
        "Turbine blade with tuned damping structure".  United States.  https://www.osti.gov/servlets/purl/1213468.

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@article{osti_1213468,

  title        = {Turbine blade with tuned damping structure},

  author       = {Campbell, Christian X. and Messmann, Stephen J.},

  abstractNote = {A turbine blade is provided comprising: a root; an airfoil comprising an external wall extending radially from the root and having a radially outermost portion; and a damping structure. The external wall may comprise first and second side walls joined together to define an inner cavity of the airfoil. The damping structure may be positioned within the airfoil inner cavity and coupled to the airfoil so as to define a tuned mass damper.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {Tue Sep 01 00:00:00 EDT 2015},

  month        = {Tue Sep 01 00:00:00 EDT 2015}

}

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Works referenced in this record:

Vibration Damping Device
patent, November 1931

Kimball, Arthur L.
US Patent Document 1833751
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/1833751

Vibration Damper for Blades and Vanes
patent, September 1954

Odeguard, Eugene A.
US Patent Document 2,689,107
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2689107

Vibration damped rotor blades for turbomachines
patent, July 1984

Fuller, John R. C.
US Patent Document 4,460,314
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4460314

Rotor blade for a gas turbine engine
patent, November 1984

Pask, George; Sadler, John; Coplin, John F.
US Patent Document 4,484,859
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4484859

Damped airfoil blade
patent, November 1992

Stoner, Alan W.; El-Aini, Yehia M.; Wiebe, David J.
US Patent Document 5,165,860
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5165860

Airfoil vibration damping device
patent, October 1998

Kraft, Robert J.; McClelland, Robert J.
US Patent Document 5,820,343
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5820343

Panel damped hybrid blade
patent, March 2000

Schilling, Jan Christopher; Cornell, Jay L.; Stevenson, Joseph T.
US Patent Document 6,039,542
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6039542

Gas turbine engine airfoil damper and method for production
patent, December 2000

Mannava, Seetharamaiah; Cowie, William D.; Yeaton, Robert L.
US Patent Document 6,155,789
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6155789

Aerofoil blade damper
patent, September 2001

Chin, Kevin
US Patent Document 6,283,707
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6283707

Methods and apparatus for damping rotor assembly vibrations
patent, October 2002

Crall, David William
US Patent Document 6,471,484
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6471484

Apparatus for passive damping of flexural blade vibration in turbo-machinery
patent, August 2003

von Flotow, Andreas H.
US Patent Document 6,607,359
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6607359

Component with internal damping
patent, July 2006

Powell, Christopher A.
US Patent Document 7,070,390
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7070390

Rotor blade with a stick damper
patent, May 2007

Propheter, Tracy A.; Surace, Raymond
US Patent Document 7,217,093
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7217093

Turbine blade with vibration damper
patent, September 2007

Garner, Chad
US Patent Document 7,270,517
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7270517

Composite filled gas turbine engine blade with gas film damper
patent, October 2007

Vetters, Daniel K.
US Patent Document 7,278,830
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7278830

Damper configured turbine blade
patent, June 2010

Bauer, Randall Charles; Garay, Gregory Terrence; Weaver, Matthew Mark
US Patent Document 7,736,124
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7736124

Vibration Damper
patent-application, September 2010

Miller, David
US Patent Application 12/693807; 20100232968
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100232968

Airfoil with Break-Way, Free-Floating Damper Member
patent-application, October 2013

Fisk, Benjamin T.; Propheter-Hinckley, Tracy A.; Dolansky, Gregory M.
US Patent Application 13/454183; 20130276455
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130276455

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Similar Records

Title: Turbine blade with tuned damping structure

Abstract

Citation Formats

Vibration Damping Device patent, November 1931

Vibration Damper for Blades and Vanes patent, September 1954

Vibration damped rotor blades for turbomachines patent, July 1984

Rotor blade for a gas turbine engine patent, November 1984

Damped airfoil blade patent, November 1992

Airfoil vibration damping device patent, October 1998

Panel damped hybrid blade patent, March 2000

Gas turbine engine airfoil damper and method for production patent, December 2000

Aerofoil blade damper patent, September 2001

Methods and apparatus for damping rotor assembly vibrations patent, October 2002

Apparatus for passive damping of flexural blade vibration in turbo-machinery patent, August 2003

Component with internal damping patent, July 2006

Rotor blade with a stick damper patent, May 2007

Turbine blade with vibration damper patent, September 2007

Composite filled gas turbine engine blade with gas film damper patent, October 2007

Damper configured turbine blade patent, June 2010

Vibration Damper patent-application, September 2010

Airfoil with Break-Way, Free-Floating Damper Member patent-application, October 2013

Vibration Damping Device
patent, November 1931

Vibration Damper for Blades and Vanes
patent, September 1954

Vibration damped rotor blades for turbomachines
patent, July 1984

Rotor blade for a gas turbine engine
patent, November 1984

Damped airfoil blade
patent, November 1992

Airfoil vibration damping device
patent, October 1998

Panel damped hybrid blade
patent, March 2000

Gas turbine engine airfoil damper and method for production
patent, December 2000

Aerofoil blade damper
patent, September 2001

Methods and apparatus for damping rotor assembly vibrations
patent, October 2002

Apparatus for passive damping of flexural blade vibration in turbo-machinery
patent, August 2003

Component with internal damping
patent, July 2006

Rotor blade with a stick damper
patent, May 2007

Turbine blade with vibration damper
patent, September 2007

Composite filled gas turbine engine blade with gas film damper
patent, October 2007

Damper configured turbine blade
patent, June 2010

Vibration Damper
patent-application, September 2010

Airfoil with Break-Way, Free-Floating Damper Member
patent-application, October 2013