NO20044661L - Dobbelretensjon-skovlarm - Google Patents

Dobbelretensjon-skovlarm

Info

Publication number
NO20044661L
NO20044661L NO20044661A NO20044661A NO20044661L NO 20044661 L NO20044661 L NO 20044661L NO 20044661 A NO20044661 A NO 20044661A NO 20044661 A NO20044661 A NO 20044661A NO 20044661 L NO20044661 L NO 20044661L
Authority
NO
Norway
Prior art keywords
vane
surge
fastener
skovlarm
dobbelretensjon
Prior art date
Application number
NO20044661A
Other languages
English (en)
Other versions
NO20044661D0 (no
Inventor
Phillip E Alexander
David O Kies
Joshua D Drumbaugh
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 NO20044661D0 publication Critical patent/NO20044661D0/no
Publication of NO20044661L publication Critical patent/NO20044661L/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • 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
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79—Bearing, support or actuation arrangements therefor
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Det beskrives en variabel skovlarm (48) med dobbelt retensjonsevne for å sikre at skovler i en gassturbinmotor (20) forblir forbundet til skovlarmen (48) selv under "surgebelastninger" eller en forhåndsbelastning på festeanordningen (112),. eller hele festeanordningen (112) tapes. Den variable skovlarm tilveiebringer videre en "surgesliss" (80) for å lette rotasjon av skovlen (42) selv når skovlen (42) opererer under "surgebetingelser" eller andre særlig høye trykkbetingelser.
NO20044661A 2004-02-04 2004-10-28 Dobbelretensjon-skovlarm NO20044661L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/771,884 US7011494B2 (en) 2004-02-04 2004-02-04 Dual retention vane arm

Publications (2)

Publication Number Publication Date
NO20044661D0 NO20044661D0 (no) 2004-10-28
NO20044661L true NO20044661L (no) 2005-08-05

Family

ID=34679372

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20044661A NO20044661L (no) 2004-02-04 2004-10-28 Dobbelretensjon-skovlarm

Country Status (5)

Country Link
US (1) US7011494B2 (no)
EP (1) EP1561906B1 (no)
AU (1) AU2004226998A1 (no)
CA (1) CA2486587A1 (no)
NO (1) NO20044661L (no)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7871242B2 (en) * 2007-05-31 2011-01-18 United Technologies Corporation Single actuator controlled rotational flow balance system
US8202043B2 (en) * 2007-10-15 2012-06-19 United Technologies Corp. Gas turbine engines and related systems involving variable vanes
US8033782B2 (en) * 2008-01-16 2011-10-11 Elliott Company Method to prevent brinelling wear of slot and pin assembly
US8215902B2 (en) * 2008-10-15 2012-07-10 United Technologies Corporation Scalable high pressure compressor variable vane actuation arm
US8414248B2 (en) 2008-12-30 2013-04-09 Rolls-Royce Corporation Variable geometry vane
US8864450B2 (en) * 2011-02-01 2014-10-21 United Technologies Corporation Gas turbine engine synchronizing ring bumper
US8915703B2 (en) * 2011-07-28 2014-12-23 United Technologies Corporation Internally actuated inlet guide vane for fan section
US10030533B2 (en) * 2012-09-21 2018-07-24 United Technologies Corporation Flanged bushing for variable vane
US8783119B2 (en) 2012-09-26 2014-07-22 United Technologies Corporation Vane arm testing rig
US10132179B2 (en) * 2012-09-28 2018-11-20 United Technologies Corporation Alignment tool for use in a gas turbine engine
WO2014113010A1 (en) * 2013-01-17 2014-07-24 United Technologies Corporation Vane lever arm for a variable area vane arrangement
WO2014116216A1 (en) * 2013-01-24 2014-07-31 United Technologies Corporation Gas turbine engine component with angled aperture impingement
US10208618B2 (en) * 2013-02-04 2019-02-19 United Technologies Corporation Vane arm having a claw
US9988926B2 (en) 2013-03-13 2018-06-05 United Technologies Corporation Machined vane arm of a variable vane actuation system
EP3036407B1 (en) * 2013-08-22 2020-11-11 United Technologies Corporation Vane arm assembly
US9644491B2 (en) 2014-06-13 2017-05-09 Pratt & Whitney Canada Corp. Single bolting flange arrangement for variable guide vane connection
US10563670B2 (en) * 2016-07-29 2020-02-18 Rolls-Royce Corporation Vane actuation system for a gas turbine engine
DE102016224523A1 (de) * 2016-12-08 2018-06-14 MTU Aero Engines AG Leitschaufelverstellung mit seitlich montiertem Verstellhebel
US10502091B2 (en) * 2016-12-12 2019-12-10 United Technologies Corporation Sync ring assembly and associated clevis including a rib
US10815818B2 (en) * 2017-07-18 2020-10-27 Raytheon Technologies Corporation Variable-pitch vane assembly
US10590795B2 (en) * 2017-10-17 2020-03-17 United Technologies Corporation Vane arm with tri-wedge circular pocket
US10830155B2 (en) 2018-02-08 2020-11-10 Raytheon Technologies Corporation Variable vane arm retention feature
DE102018202119A1 (de) 2018-02-12 2019-08-14 MTU Aero Engines AG Hebelanbindung einer Leitschaufelverstellung für Strömungsmaschinen
US10837309B2 (en) 2019-04-09 2020-11-17 Raytheon Technologies Corporation Retention clip for variable vane arm
US11391174B2 (en) * 2019-09-17 2022-07-19 Raytheon Technologies Corporation Vane arm clip for variable stator vanes
US11680494B2 (en) * 2020-02-14 2023-06-20 Raytheon Technologies Corporation Vane arm torque transfer plate
DE202023106055U1 (de) 2023-10-19 2023-11-30 MTU Aero Engines AG Hebelanbindung einer Leitschaufelverstellung für Strömungsmaschinen
DE202023106491U1 (de) 2023-11-07 2023-12-13 MTU Aero Engines AG Hebelanbindung einer Leitschaufelverstellung für eine Strömungsmaschine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1425074A (fr) * 1965-02-22 1966-01-14 Kolomensky Teplovozostroitelny Appareil directeur réglable pour turbine radiale
US4050844A (en) * 1976-06-01 1977-09-27 United Technologies Corporation Connection between vane arm and unison ring in variable area stator ring
US4668165A (en) * 1986-03-27 1987-05-26 The United States Of America As Represented By The Secretary Of The Air Force Super gripper variable vane arm
US4755104A (en) * 1986-04-29 1988-07-05 United Technologies Corporation Stator vane linkage
US4767264A (en) * 1986-10-31 1988-08-30 United Technologies Corporation Vane lever arm construction
US4897021A (en) * 1988-06-02 1990-01-30 United Technologies Corporation Stator vane asssembly for an axial flow rotary machine
US4979874A (en) * 1989-06-19 1990-12-25 United Technologies Corporation Variable van drive mechanism
US5211537A (en) * 1992-03-02 1993-05-18 United Technologies Corporation Compressor vane lock
US5517817A (en) * 1993-10-28 1996-05-21 General Electric Company Variable area turbine nozzle for turbine engines
US5462403A (en) * 1994-03-21 1995-10-31 United Technologies Corporation Compressor stator vane assembly
US6375419B1 (en) * 1995-06-02 2002-04-23 United Technologies Corporation Flow directing element for a turbine engine
US6146093A (en) 1998-12-16 2000-11-14 General Electric Company Variable vane seal and washer
FR2835295B1 (fr) * 2002-01-29 2004-04-16 Snecma Moteurs Dispositif de commande d'aube a angle de calage variable a liaison par pincement pour redresseur de compresseur de turbomachine

Also Published As

Publication number Publication date
NO20044661D0 (no) 2004-10-28
EP1561906A2 (en) 2005-08-10
US7011494B2 (en) 2006-03-14
EP1561906A3 (en) 2009-01-07
AU2004226998A1 (en) 2005-08-18
CA2486587A1 (en) 2005-08-04
US20050169741A1 (en) 2005-08-04
EP1561906B1 (en) 2013-03-20

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Legal Events

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