JP2005061418A - ガスタービンエンジンを製作するための方法及び装置 - Google Patents

ガスタービンエンジンを製作するための方法及び装置 Download PDF

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Publication number
JP2005061418A
JP2005061418A JP2004236971A JP2004236971A JP2005061418A JP 2005061418 A JP2005061418 A JP 2005061418A JP 2004236971 A JP2004236971 A JP 2004236971A JP 2004236971 A JP2004236971 A JP 2004236971A JP 2005061418 A JP2005061418 A JP 2005061418A
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JP
Japan
Prior art keywords
rim
assembly
ring member
flange
casing
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Withdrawn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
JP2004236971A
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English (en)
Japanese (ja)
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JP2005061418A5 (enExample
Inventor
Thomas Maclean
トマス・マクリーン
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2005061418A publication Critical patent/JP2005061418A/ja
Publication of JP2005061418A5 publication Critical patent/JP2005061418A5/ja
Withdrawn legal-status Critical Current

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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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2004236971A 2003-08-18 2004-08-17 ガスタービンエンジンを製作するための方法及び装置 Withdrawn JP2005061418A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/642,719 US6848885B1 (en) 2003-08-18 2003-08-18 Methods and apparatus for fabricating gas turbine engines

Publications (2)

Publication Number Publication Date
JP2005061418A true JP2005061418A (ja) 2005-03-10
JP2005061418A5 JP2005061418A5 (enExample) 2007-09-27

Family

ID=34063447

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004236971A Withdrawn JP2005061418A (ja) 2003-08-18 2004-08-17 ガスタービンエンジンを製作するための方法及び装置

Country Status (3)

Country Link
US (1) US6848885B1 (enExample)
EP (1) EP1508673A3 (enExample)
JP (1) JP2005061418A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007538199A (ja) * 2004-05-17 2007-12-27 カルダレア、エル、ジェームス、ジュニア ガスタービンジェットエンジンにおけるタービンケースの補強

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US7377742B2 (en) * 2005-10-14 2008-05-27 General Electric Company Turbine shroud assembly and method for assembling a gas turbine engine
US8079773B2 (en) * 2005-10-18 2011-12-20 General Electric Company Methods and apparatus for assembling composite structures
US8393855B2 (en) * 2007-06-29 2013-03-12 General Electric Company Flange with axially curved impingement surface for gas turbine engine clearance control
US8197186B2 (en) * 2007-06-29 2012-06-12 General Electric Company Flange with axially extending holes for gas turbine engine clearance control
GB0909470D0 (en) * 2009-06-03 2009-07-15 Rolls Royce Plc A guide vane assembly
WO2014051686A1 (en) * 2012-09-26 2014-04-03 United Technologies Corporation Combined high pressure turbine case and turbine intermediate case
US10132187B2 (en) * 2013-08-07 2018-11-20 United Technologies Corporation Clearance control assembly
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
US9784132B2 (en) * 2015-04-20 2017-10-10 Pratt & Whitney Canada Corp. Voltage discharge channelling assembly for a gas turbine engine
EP3153671A1 (de) 2015-10-08 2017-04-12 MTU Aero Engines GmbH Schutzvorrichtung für eine strömungsmaschine
US20250198306A1 (en) * 2023-12-14 2025-06-19 Rtx Corporation Split case with coatable transistion feature

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR996476A (fr) * 1949-10-01 1951-12-19 Cem Comp Electro Mec Cylindre pour turbines à gaz
US2749026A (en) * 1951-02-27 1956-06-05 United Aircraft Corp Stator construction for compressors
GB2019954B (en) * 1978-04-04 1982-08-04 Rolls Royce Turbomachine housing
US4840026A (en) * 1988-02-24 1989-06-20 The United States Of America As Represented By The Secretary Of The Air Force Band clamp apparatus
US5154575A (en) * 1991-07-01 1992-10-13 United Technologies Corporation Thermal blade tip clearance control for gas turbine engines
GB9709086D0 (en) * 1997-05-07 1997-06-25 Rolls Royce Plc Gas turbine engine cooling apparatus
US6290455B1 (en) * 1999-12-03 2001-09-18 General Electric Company Contoured hardwall containment
US6514041B1 (en) * 2001-09-12 2003-02-04 Alstom (Switzerland) Ltd Carrier for guide vane and heat shield segment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007538199A (ja) * 2004-05-17 2007-12-27 カルダレア、エル、ジェームス、ジュニア ガスタービンジェットエンジンにおけるタービンケースの補強

Also Published As

Publication number Publication date
US6848885B1 (en) 2005-02-01
EP1508673A3 (en) 2007-06-13
US20050042090A1 (en) 2005-02-24
EP1508673A2 (en) 2005-02-23

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