CN103291387B - 用于燃气涡轮发动机的护罩段和包括其的护罩设备 - Google Patents

用于燃气涡轮发动机的护罩段和包括其的护罩设备 Download PDF

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Publication number
CN103291387B
CN103291387B CN201310056712.0A CN201310056712A CN103291387B CN 103291387 B CN103291387 B CN 103291387B CN 201310056712 A CN201310056712 A CN 201310056712A CN 103291387 B CN103291387 B CN 103291387B
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China
Prior art keywords
wall
shield sections
suspension
shield
equipment according
Prior art date
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CN201310056712.0A
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English (en)
Chinese (zh)
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CN103291387A (zh
Inventor
M.J.弗兰克斯
J.D.夏皮罗
S.R.鲁利
R.L.道蒂
J.B.贾米森
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General Electric Co
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General Electric Co
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Publication date
Priority claimed from US13/402,616 external-priority patent/US9175579B2/en
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN103291387A publication Critical patent/CN103291387A/zh
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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
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20Actively adjusting tip-clearance
    • F01D11/24Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/11Shroud seal segments
    • 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
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6033Ceramic matrix composites [CMC]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201310056712.0A 2012-02-22 2013-02-22 用于燃气涡轮发动机的护罩段和包括其的护罩设备 Active CN103291387B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/402,616 US9175579B2 (en) 2011-12-15 2012-02-22 Low-ductility turbine shroud
US13/402616 2012-02-22

Publications (2)

Publication Number Publication Date
CN103291387A CN103291387A (zh) 2013-09-11
CN103291387B true CN103291387B (zh) 2017-04-26

Family

ID=47790007

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310056712.0A Active CN103291387B (zh) 2012-02-22 2013-02-22 用于燃气涡轮发动机的护罩段和包括其的护罩设备

Country Status (4)

Country Link
EP (1) EP2631434A3 (enExample)
JP (1) JP6063285B2 (enExample)
CN (1) CN103291387B (enExample)
CA (1) CA2806401A1 (enExample)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9726043B2 (en) 2011-12-15 2017-08-08 General Electric Company Mounting apparatus for low-ductility turbine shroud
CA2912428C (en) 2013-05-17 2018-03-13 General Electric Company Cmc shroud support system of a gas turbine
CA2932612C (en) * 2013-12-12 2022-01-18 General Electric Company Cmc shroud support system
WO2015108658A1 (en) 2014-01-17 2015-07-23 General Electric Company Cmc hanger sleeve for cmc shroud
EP2930308B1 (fr) * 2014-04-11 2021-07-28 Safran Aero Boosters SA Carter à facettes de turbomachine axiale
WO2015173312A1 (en) * 2014-05-15 2015-11-19 Nuovo Pignone Srl Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine
JP6363232B2 (ja) * 2014-06-12 2018-07-25 ゼネラル・エレクトリック・カンパニイ シュラウドハンガーアセンブリ
US10465558B2 (en) 2014-06-12 2019-11-05 General Electric Company Multi-piece shroud hanger assembly
WO2015191185A1 (en) 2014-06-12 2015-12-17 General Electric Company Shroud hanger assembly
US9874104B2 (en) 2015-02-27 2018-01-23 General Electric Company Method and system for a ceramic matrix composite shroud hanger assembly
US10422244B2 (en) * 2015-03-16 2019-09-24 General Electric Company System for cooling a turbine shroud
FR3034132B1 (fr) * 2015-03-23 2018-06-15 Safran Ceramics Ensemble d'anneau de turbine comprenant une pluralite de secteurs d'anneau en materiau composite a matrice ceramique
CA2925588A1 (en) 2015-04-29 2016-10-29 Rolls-Royce Corporation Brazed blade track for a gas turbine engine
US10550709B2 (en) 2015-04-30 2020-02-04 Rolls-Royce North American Technologies Inc. Full hoop blade track with flanged segments
US9932901B2 (en) 2015-05-11 2018-04-03 General Electric Company Shroud retention system with retention springs
US9915153B2 (en) 2015-05-11 2018-03-13 General Electric Company Turbine shroud segment assembly with expansion joints
FR3036433B1 (fr) * 2015-05-22 2019-09-13 Safran Ceramics Ensemble d'anneau de turbine avec maintien par crabotage
EP3121387B1 (en) * 2015-07-24 2018-12-26 Rolls-Royce Corporation A gas turbine engine with a seal segment
US10100654B2 (en) * 2015-11-24 2018-10-16 Rolls-Royce North American Technologies Inc. Impingement tubes for CMC seal segment cooling
US20170370583A1 (en) * 2016-06-22 2017-12-28 General Electric Company Ceramic Matrix Composite Component for a Gas Turbine Engine
FR3056632B1 (fr) 2016-09-27 2020-06-05 Safran Aircraft Engines Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
US10633996B2 (en) 2016-11-17 2020-04-28 Rolls-Royce Corporation Turbine cooling system
US10619514B2 (en) 2017-10-18 2020-04-14 Rolls-Royce Corporation Ceramic matrix composite assembly with compliant pin attachment features
US20190170013A1 (en) * 2017-12-06 2019-06-06 General Electric Company Discontinuous Molded Tape Wear Interface for Composite Components
US10801350B2 (en) 2018-02-23 2020-10-13 Rolls-Royce Corporation Actively cooled engine assembly with ceramic matrix composite components
US11408300B2 (en) 2018-12-03 2022-08-09 Raytheon Technologies Corporation Rotor overspeed protection assembly
US10914186B2 (en) * 2018-12-05 2021-02-09 Raytheon Technologies Corporation BOAS control structure with center support hook
US10934878B2 (en) * 2018-12-05 2021-03-02 Raytheon Technologies Corporation CMC loop boas
US11724969B2 (en) * 2018-12-14 2023-08-15 General Electric Company Coating for improved surface finish
US10927694B2 (en) 2019-03-13 2021-02-23 Raytheon Technologies Corporation BOAS carrier with cooling supply
FR3095668B1 (fr) * 2019-05-03 2021-04-09 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
US11365644B2 (en) 2019-07-01 2022-06-21 Raytheon Technologies Corporation Double box boas and carrier system
CN113062781B (zh) * 2021-05-06 2022-07-08 中国航发湖南动力机械研究所 一种用于cmc燃气涡轮外环的定心定位结构

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3583824A (en) * 1969-10-02 1971-06-08 Gen Electric Temperature controlled shroud and shroud support
CN102135020A (zh) * 2010-01-25 2011-07-27 株式会社日立制作所 具有陶瓷可磨耗涂层的燃气涡轮机用护罩
CA2740538A1 (en) * 2010-05-28 2011-11-28 General Electric Company Low-ductility turbine shroud and mounting apparatus

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2580033A1 (en) * 1985-04-03 1986-10-10 Snecma Elastically suspended turbine ring for a turbine machine
JPH10103014A (ja) * 1996-09-30 1998-04-21 Toshiba Corp ガスタービンシュラウド構造
US6340285B1 (en) * 2000-06-08 2002-01-22 General Electric Company End rail cooling for combined high and low pressure turbine shroud
US6478545B2 (en) * 2001-03-07 2002-11-12 General Electric Company Fluted blisk
US6733233B2 (en) * 2002-04-26 2004-05-11 Pratt & Whitney Canada Corp. Attachment of a ceramic shroud in a metal housing
JP2004036443A (ja) * 2002-07-02 2004-02-05 Ishikawajima Harima Heavy Ind Co Ltd ガスタービンシュラウド構造
US7270518B2 (en) * 2005-05-19 2007-09-18 General Electric Company Steep angle turbine cover buckets having relief grooves
US7563071B2 (en) * 2005-08-04 2009-07-21 Siemens Energy, Inc. Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
US7749565B2 (en) 2006-09-29 2010-07-06 General Electric Company Method for applying and dimensioning an abradable coating
GB0703827D0 (en) * 2007-02-28 2007-04-11 Rolls Royce Plc Rotor seal segment
US8753073B2 (en) * 2010-06-23 2014-06-17 General Electric Company Turbine shroud sealing apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3583824A (en) * 1969-10-02 1971-06-08 Gen Electric Temperature controlled shroud and shroud support
CN102135020A (zh) * 2010-01-25 2011-07-27 株式会社日立制作所 具有陶瓷可磨耗涂层的燃气涡轮机用护罩
CA2740538A1 (en) * 2010-05-28 2011-11-28 General Electric Company Low-ductility turbine shroud and mounting apparatus

Also Published As

Publication number Publication date
CN103291387A (zh) 2013-09-11
JP2013170578A (ja) 2013-09-02
EP2631434A3 (en) 2017-07-26
JP6063285B2 (ja) 2017-01-18
EP2631434A2 (en) 2013-08-28
CA2806401A1 (en) 2013-08-22

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