NO20051543L - Rotorblad med stavformet demper - Google Patents

Rotorblad med stavformet demper

Info

Publication number
NO20051543L
NO20051543L NO20051543A NO20051543A NO20051543L NO 20051543 L NO20051543 L NO 20051543L NO 20051543 A NO20051543 A NO 20051543A NO 20051543 A NO20051543 A NO 20051543A NO 20051543 L NO20051543 L NO 20051543L
Authority
NO
Norway
Prior art keywords
foot
tip
rotor blade
edge surface
rod
Prior art date
Application number
NO20051543A
Other languages
English (en)
Norwegian (no)
Other versions
NO20051543D0 (no
Inventor
Raymond Surace
Tracy Propheter
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of NO20051543D0 publication Critical patent/NO20051543D0/no
Publication of NO20051543L publication Critical patent/NO20051543L/no

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fluid-Damping Devices (AREA)
  • Rotary Pumps (AREA)
  • Multiple-Way Valves (AREA)
NO20051543A 2004-05-27 2005-03-23 Rotorblad med stavformet demper NO20051543L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/855,184 US7217093B2 (en) 2004-05-27 2004-05-27 Rotor blade with a stick damper

Publications (2)

Publication Number Publication Date
NO20051543D0 NO20051543D0 (no) 2005-03-23
NO20051543L true NO20051543L (no) 2005-11-28

Family

ID=34940667

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20051543A NO20051543L (no) 2004-05-27 2005-03-23 Rotorblad med stavformet demper

Country Status (12)

Country Link
US (1) US7217093B2 (pl)
EP (1) EP1602801B1 (pl)
JP (1) JP2005337237A (pl)
KR (1) KR20060044732A (pl)
AT (1) ATE362036T1 (pl)
AU (1) AU2005201263A1 (pl)
CA (1) CA2501160A1 (pl)
DE (1) DE602005001085T2 (pl)
NO (1) NO20051543L (pl)
PL (1) PL1602801T3 (pl)
SG (1) SG117530A1 (pl)
TW (1) TW200538625A (pl)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7625178B2 (en) * 2006-08-30 2009-12-01 Honeywell International Inc. High effectiveness cooled turbine blade
US7736124B2 (en) * 2007-04-10 2010-06-15 General Electric Company Damper configured turbine blade
US8579593B2 (en) * 2009-11-06 2013-11-12 Siemens Energy, Inc. Damping element for reducing the vibration of an airfoil
JP5660883B2 (ja) 2010-12-22 2015-01-28 三菱日立パワーシステムズ株式会社 蒸気タービンの静翼、蒸気タービン
US9403208B2 (en) 2010-12-30 2016-08-02 United Technologies Corporation Method and casting core for forming a landing for welding a baffle inserted in an airfoil
US9249668B2 (en) 2012-04-24 2016-02-02 United Technologies Corporation Airfoil with break-way, free-floating damper member
US9470095B2 (en) 2012-04-24 2016-10-18 United Technologies Corporation Airfoil having internal lattice network
US9296039B2 (en) 2012-04-24 2016-03-29 United Technologies Corporation Gas turbine engine airfoil impingement cooling
US9404369B2 (en) 2012-04-24 2016-08-02 United Technologies Corporation Airfoil having minimum distance ribs
US9175570B2 (en) 2012-04-24 2015-11-03 United Technologies Corporation Airfoil including member connected by articulated joint
US9074482B2 (en) 2012-04-24 2015-07-07 United Technologies Corporation Airfoil support method and apparatus
US9243502B2 (en) 2012-04-24 2016-01-26 United Technologies Corporation Airfoil cooling enhancement and method of making the same
US9267380B2 (en) 2012-04-24 2016-02-23 United Technologies Corporation Airfoil including loose damper
US9181806B2 (en) 2012-04-24 2015-11-10 United Technologies Corporation Airfoil with powder damper
US8915718B2 (en) 2012-04-24 2014-12-23 United Technologies Corporation Airfoil including damper member
US9133712B2 (en) 2012-04-24 2015-09-15 United Technologies Corporation Blade having porous, abradable element
US9121288B2 (en) 2012-05-04 2015-09-01 Siemens Energy, Inc. Turbine blade with tuned damping structure
EP3097268B1 (en) * 2014-01-24 2019-04-24 United Technologies Corporation Blade for a gas turbine engine and corresponding method of damping
JP5766861B2 (ja) * 2014-09-10 2015-08-19 三菱日立パワーシステムズ株式会社 蒸気タービンの静翼、蒸気タービン
JP5805283B2 (ja) * 2014-09-10 2015-11-04 三菱日立パワーシステムズ株式会社 蒸気タービンの静翼、蒸気タービン
US10774653B2 (en) 2018-12-11 2020-09-15 Raytheon Technologies Corporation Composite gas turbine engine component with lattice structure
US11371358B2 (en) 2020-02-19 2022-06-28 General Electric Company Turbine damper
US11739645B2 (en) 2020-09-30 2023-08-29 General Electric Company Vibrational dampening elements
US11536144B2 (en) 2020-09-30 2022-12-27 General Electric Company Rotor blade damping structures
US11808166B1 (en) * 2021-08-19 2023-11-07 United States Of America As Represented By The Administrator Of Nasa Additively manufactured bladed-disk having blades with integral tuned mass absorbers
US12371998B2 (en) * 2023-06-29 2025-07-29 Ge Infrastructure Technology Llc Nested damper pin and vibration dampening system for turbine nozzle or blade

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB347964A (en) 1929-07-05 1931-05-07 British Thomson Houston Co Ltd Improvements in and relating to vibration damping devices particularly for turbines, propellers and the like
US2689107A (en) * 1949-08-13 1954-09-14 United Aircraft Corp Vibration damper for blades and vanes
GB2097479B (en) * 1981-04-24 1984-09-05 Rolls Royce Cooled vane for a gas turbine engine
US5407321A (en) * 1993-11-29 1995-04-18 United Technologies Corporation Damping means for hollow stator vane airfoils
US5820343A (en) * 1995-07-31 1998-10-13 United Technologies Corporation Airfoil vibration damping device
US5558497A (en) * 1995-07-31 1996-09-24 United Technologies Corporation Airfoil vibration damping device
GB9906450D0 (en) * 1999-03-19 1999-05-12 Rolls Royce Plc Aerofoil blade damper
US6929451B2 (en) * 2003-12-19 2005-08-16 United Technologies Corporation Cooled rotor blade with vibration damping device

Also Published As

Publication number Publication date
NO20051543D0 (no) 2005-03-23
ATE362036T1 (de) 2007-06-15
SG117530A1 (en) 2005-12-29
US7217093B2 (en) 2007-05-15
TW200538625A (en) 2005-12-01
KR20060044732A (ko) 2006-05-16
DE602005001085T2 (de) 2007-11-22
AU2005201263A1 (en) 2005-12-15
CA2501160A1 (en) 2005-11-27
JP2005337237A (ja) 2005-12-08
EP1602801A1 (en) 2005-12-07
DE602005001085D1 (de) 2007-06-21
US20050265843A1 (en) 2005-12-01
EP1602801B1 (en) 2007-05-09
PL1602801T3 (pl) 2007-09-28

Similar Documents

Publication Publication Date Title
NO20051543L (no) Rotorblad med stavformet demper
NO20050623L (no) Kjolt rotorblad med vibrasjonsdempningsanordning
ATE369094T1 (de) Verformbare zwischenwirbelprothese
DK1837147T3 (da) Træflækker
DE602006006194D1 (de) Flügelspitzenvorrichtung
ATE501769T1 (de) Skiprofil-kurve
AR055490A1 (es) Clavo endomedular destinado de fracturas de femur proximal
NO20080223L (no) Sparkelspade med forskjovet handtak
PE20201310A1 (es) Superficie de punta arqueada y montaje de hoja
AR057783A1 (es) Montaje de desgaste para excavadoras
BR0005937A (pt) Aerofólio de abaulamento curvado
DK1342009T3 (da) Vindmöllerotorvinge med kombineret lynreceptor og drænkanal samt lynreceptor med drænkanal
CO5640062A1 (es) Instrumentos y metodos para insertar un implante intervertebral
FR2903293B1 (fr) Vis a os
UY28709A1 (es) Derivados de prostaglandinas
MX2019000438A (es) Cubierta de labio para labio moldeado en implemento de trabajo.
ATE485009T1 (de) Orthopädisches implantat
AR073133A1 (es) Agente para el tratamiento de enfermedades pulmonares
BRPI0514470A (pt) 5-[3-(4-benziloxifeniltio)-fur-2-il]-imidazolin-2, 4-diona e análogos como inibidores de elastase macrofágica
FR3038343B1 (fr) Aube de turbine a bord de fuite ameliore
FR2864451B1 (fr) Ski
ATE321229T1 (de) Rückschlagventil
ATE377378T1 (de) Physiologische spekulum
FI20075837A0 (fi) Kiinnitysruuvi
WO2005079251A3 (en) Laryngoscope blade

Legal Events

Date Code Title Description
FC2A Withdrawal, rejection or dismissal of laid open patent application