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EP2870342A4 - Engrènement de porte-joint de turbine haute pression sur cadre de turbine intermédiaire - Google Patents

Engrènement de porte-joint de turbine haute pression sur cadre de turbine intermédiaire

Info

Publication number
EP2870342A4
EP2870342A4 EP13816663.2A EP13816663A EP2870342A4 EP 2870342 A4 EP2870342 A4 EP 2870342A4 EP 13816663 A EP13816663 A EP 13816663A EP 2870342 A4 EP2870342 A4 EP 2870342A4
Authority
EP
European Patent Office
Prior art keywords
mid
seal support
turbine frame
support meshing
hpt
Prior art date
Legal status (The legal status 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 status listed.)
Withdrawn
Application number
EP13816663.2A
Other languages
German (de)
English (en)
Other versions
EP2870342A1 (fr
Inventor
Jorge I Farah
Shu Liu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
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 EP2870342A1 publication Critical patent/EP2870342A1/fr
Publication of EP2870342A4 publication Critical patent/EP2870342A4/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/501Elasticity

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP13816663.2A 2012-07-09 2013-07-09 Engrènement de porte-joint de turbine haute pression sur cadre de turbine intermédiaire Withdrawn EP2870342A4 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/544,229 US20140010649A1 (en) 2012-07-09 2012-07-09 Mid-turbine frame hpt seal support meshing
PCT/US2013/049646 WO2014011586A1 (fr) 2012-07-09 2013-07-09 Engrènement de porte-joint de turbine haute pression sur cadre de turbine intermédiaire

Publications (2)

Publication Number Publication Date
EP2870342A1 EP2870342A1 (fr) 2015-05-13
EP2870342A4 true EP2870342A4 (fr) 2015-07-22

Family

ID=49878661

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13816663.2A Withdrawn EP2870342A4 (fr) 2012-07-09 2013-07-09 Engrènement de porte-joint de turbine haute pression sur cadre de turbine intermédiaire

Country Status (3)

Country Link
US (1) US20140010649A1 (fr)
EP (1) EP2870342A4 (fr)
WO (1) WO2014011586A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10934890B2 (en) 2014-05-09 2021-03-02 Raytheon Technologies Corporation Shrouded conduit for arranging a fluid flowpath
US10215098B2 (en) 2015-01-22 2019-02-26 United Technologies Corporation Bearing compartment seal
US9926797B2 (en) 2015-01-22 2018-03-27 United Technologies Corporation Flange trapped seal configuration
US10161256B2 (en) * 2015-01-22 2018-12-25 Untied Technologies Corporation Seal with backup seal
DE102016218239A1 (de) 2016-09-22 2018-03-22 MTU Aero Engines AG Dichtungsanordnung für ein Turbinenzwischengehäuse einer Gasturbine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6183193B1 (en) * 1999-05-21 2001-02-06 Pratt & Whitney Canada Corp. Cast on-board injection nozzle with adjustable flow area
US20040007823A1 (en) * 2002-07-12 2004-01-15 General Electric Company Seal for a rotating member
US20040120807A1 (en) * 2002-12-19 2004-06-24 Albers Robert Joseph Method and apparatus for controlling fluid leakage through gas turbine engines
DE102009044103A1 (de) * 2008-11-29 2010-06-02 General Electric Co. Turbinengehäuseanordnung und Verfahren für eine Gasturbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6676369B2 (en) * 2002-03-26 2004-01-13 General Electric Company Aspirating face seal with axially extending seal teeth
US8061969B2 (en) * 2008-11-28 2011-11-22 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US20100132371A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8511969B2 (en) * 2009-10-01 2013-08-20 Pratt & Whitney Canada Corp. Interturbine vane with multiple air chambers
US8920113B2 (en) * 2011-11-28 2014-12-30 United Technologies Corporation Thermal gradiant tolerant turbomachine coupling member
US9394915B2 (en) * 2012-06-04 2016-07-19 United Technologies Corporation Seal land for static structure of a gas turbine engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6183193B1 (en) * 1999-05-21 2001-02-06 Pratt & Whitney Canada Corp. Cast on-board injection nozzle with adjustable flow area
US20040007823A1 (en) * 2002-07-12 2004-01-15 General Electric Company Seal for a rotating member
US20040120807A1 (en) * 2002-12-19 2004-06-24 Albers Robert Joseph Method and apparatus for controlling fluid leakage through gas turbine engines
DE102009044103A1 (de) * 2008-11-29 2010-06-02 General Electric Co. Turbinengehäuseanordnung und Verfahren für eine Gasturbine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2014011586A1 *

Also Published As

Publication number Publication date
WO2014011586A1 (fr) 2014-01-16
US20140010649A1 (en) 2014-01-09
EP2870342A1 (fr) 2015-05-13

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Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

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17P Request for examination filed

Effective date: 20150209

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

RIN1 Information on inventor provided before grant (corrected)

Inventor name: LIU, SHU

Inventor name: FARAH, JORGE I.

RA4 Supplementary search report drawn up and despatched (corrected)

Effective date: 20150619

RIC1 Information provided on ipc code assigned before grant

Ipc: F02C 7/00 20060101AFI20150615BHEP

Ipc: F01D 25/28 20060101ALI20150615BHEP

Ipc: F02C 7/28 20060101ALI20150615BHEP

Ipc: F01D 25/24 20060101ALI20150615BHEP

Ipc: F01D 11/00 20060101ALI20150615BHEP

DAX Request for extension of the european patent (deleted)
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18W Application withdrawn

Effective date: 20160118