IN2014CN03298A - - Google Patents

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Publication number
IN2014CN03298A
IN2014CN03298A IN3298CHN2014A IN2014CN03298A IN 2014CN03298 A IN2014CN03298 A IN 2014CN03298A IN 3298CHN2014 A IN3298CHN2014 A IN 3298CHN2014A IN 2014CN03298 A IN2014CN03298 A IN 2014CN03298A
Authority
IN
India
Prior art keywords
axial
radial
slot
leg
received
Prior art date
Application number
Inventor
David Scott Stapleton
Christopher Michael Ceglio
Victor Hugo Silva Correia
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IN2014CN03298A publication Critical patent/IN2014CN03298A/en

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • 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
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • F05D2240/57—Leaf seals
    • 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
    • F05D2240/00—Components
    • F05D2240/55—Seals
    • F05D2240/59—Lamellar seals

Abstract

A shroud apparatus for a gas turbine engine includes: an annular shroud segment (26) having an arcuate bottom wall (52) defining an arcuate inner flowpath surface(62) spaced apart forward and aft walls (54 56) extending radially outward from the bottom wall (52) and spaced apart side walls (58) extending radially outward from the bottom wall (52) and between the forward and aft walls (54 56) each side wall (58) defining an end face (74) which includes: an axial slot (76) extending in a generally axial direction along the end face (74); a first radial slot (78) extending in a generally radial direction along the end face (74) and intersecting the axial slot (76); an axial spline seal (82) received in the axial slot (76); and a first radial spline seal (84) having an L shape with radial and axial legs (88 90) the radial leg (88)being substantially longer than the axial leg (90) wherein the radial leg (88) is received in the first radial slot (78) and the axial leg is received in the axial slot (76).
IN3298CHN2014 2011-11-06 2012-08-24 IN2014CN03298A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161556270P 2011-11-06 2011-11-06
US13/443,947 US9810086B2 (en) 2011-11-06 2012-04-11 Asymmetric radial spline seal for a gas turbine engine
PCT/US2012/052185 WO2013074165A2 (en) 2011-11-06 2012-08-24 Asymmetric radial spline seal for a gas turbine engine

Publications (1)

Publication Number Publication Date
IN2014CN03298A true IN2014CN03298A (en) 2015-10-09

Family

ID=48223803

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3298CHN2014 IN2014CN03298A (en) 2011-11-06 2012-08-24

Country Status (8)

Country Link
US (1) US9810086B2 (en)
EP (1) EP2776681A2 (en)
JP (1) JP6031116B2 (en)
CN (1) CN103906896B (en)
BR (1) BR112014010747A8 (en)
CA (1) CA2853622C (en)
IN (1) IN2014CN03298A (en)
WO (1) WO2013074165A2 (en)

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* Cited by examiner, † Cited by third party
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US9810086B2 (en) * 2011-11-06 2017-11-07 General Electric Company Asymmetric radial spline seal for a gas turbine engine
JP5717904B1 (en) * 2014-08-04 2015-05-13 三菱日立パワーシステムズ株式会社 Stator blade, gas turbine, split ring, stator blade remodeling method, and split ring remodeling method
US9915159B2 (en) 2014-12-18 2018-03-13 General Electric Company Ceramic matrix composite nozzle mounted with a strut and concepts thereof
FR3041993B1 (en) * 2015-10-05 2019-06-21 Safran Aircraft Engines TURBINE RING ASSEMBLY WITH AXIAL RETENTION
US10161257B2 (en) 2015-10-20 2018-12-25 General Electric Company Turbine slotted arcuate leaf seal
US10494943B2 (en) * 2016-02-03 2019-12-03 General Electric Company Spline seal for a gas turbine engine
US10557360B2 (en) * 2016-10-17 2020-02-11 United Technologies Corporation Vane intersegment gap sealing arrangement
US10655495B2 (en) * 2017-02-24 2020-05-19 General Electric Company Spline for a turbine engine
KR101937586B1 (en) * 2017-09-12 2019-01-10 두산중공업 주식회사 Vane of turbine, turbine and gas turbine comprising it
EP3456927B1 (en) * 2017-09-15 2021-05-05 General Electric Company Polska sp. z o.o. Turbine nozzle assembly for a rotary machine
US10662794B2 (en) * 2017-10-19 2020-05-26 Rolls-Royce Corporation Strip seal axial assembly groove
EP3486018A1 (en) 2017-11-20 2019-05-22 Agie Charmilles SA Method and device for machining shapes using electrical machining
US20190309643A1 (en) * 2018-04-05 2019-10-10 United Technologies Corporation Axial stiffening ribs/augmentation fins
US10982559B2 (en) 2018-08-24 2021-04-20 General Electric Company Spline seal with cooling features for turbine engines
US10794206B2 (en) * 2018-09-05 2020-10-06 Raytheon Technologies Corporation CMC BOAS intersegment seal
US20200141276A1 (en) * 2018-11-07 2020-05-07 General Electric Company Turbine shroud with lapped seal segments
US11021990B2 (en) * 2018-12-19 2021-06-01 General Electric Company Shroud sealing for a gas turbine engine
US11326463B2 (en) * 2019-06-19 2022-05-10 Raytheon Technologies Corporation BOAS thermal baffle
US11187094B2 (en) 2019-08-26 2021-11-30 General Electric Company Spline for a turbine engine
US11401830B2 (en) * 2019-09-06 2022-08-02 Raytheon Technologies Corporation Geometry for a turbine engine blade outer air seal
US11215063B2 (en) 2019-10-10 2022-01-04 General Electric Company Seal assembly for chute gap leakage reduction in a gas turbine

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US5154577A (en) 1991-01-17 1992-10-13 General Electric Company Flexible three-piece seal assembly
US5641267A (en) * 1995-06-06 1997-06-24 General Electric Company Controlled leakage shroud panel
US5655876A (en) 1996-01-02 1997-08-12 General Electric Company Low leakage turbine nozzle
US5868398A (en) 1997-05-20 1999-02-09 United Technologies Corporation Gas turbine stator vane seal
US6162014A (en) 1998-09-22 2000-12-19 General Electric Company Turbine spline seal and turbine assembly containing such spline seal
FR2786222B1 (en) * 1998-11-19 2000-12-29 Snecma LAMELLE SEALING DEVICE
US6503051B2 (en) 2001-06-06 2003-01-07 General Electric Company Overlapping interference seal and methods for forming the seal
US6814538B2 (en) * 2003-01-22 2004-11-09 General Electric Company Turbine stage one shroud configuration and method for service enhancement
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US9810086B2 (en) * 2011-11-06 2017-11-07 General Electric Company Asymmetric radial spline seal for a gas turbine engine

Also Published As

Publication number Publication date
JP6031116B2 (en) 2016-11-24
CA2853622A1 (en) 2013-05-23
US20130115065A1 (en) 2013-05-09
WO2013074165A2 (en) 2013-05-23
CN103906896A (en) 2014-07-02
US9810086B2 (en) 2017-11-07
EP2776681A2 (en) 2014-09-17
BR112014010747A2 (en) 2017-06-13
CA2853622C (en) 2016-12-13
WO2013074165A8 (en) 2013-06-27
CN103906896B (en) 2016-08-31
JP2014532831A (en) 2014-12-08
WO2013074165A3 (en) 2013-08-15
BR112014010747A8 (en) 2017-06-20

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