DE69923935D1 - Montagemethode für eine Turbomaschine - Google Patents

Montagemethode für eine Turbomaschine

Info

Publication number
DE69923935D1
DE69923935D1 DE69923935T DE69923935T DE69923935D1 DE 69923935 D1 DE69923935 D1 DE 69923935D1 DE 69923935 T DE69923935 T DE 69923935T DE 69923935 T DE69923935 T DE 69923935T DE 69923935 D1 DE69923935 D1 DE 69923935D1
Authority
DE
Germany
Prior art keywords
turbomachine
mounting method
mounting
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.)
Expired - Lifetime
Application number
DE69923935T
Other languages
English (en)
Other versions
DE69923935T2 (de
Inventor
Harvey I Weiner
Christopher G Demers
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.)
Raytheon Technologies 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 DE69923935D1 publication Critical patent/DE69923935D1/de
Application granted granted Critical
Publication of DE69923935T2 publication Critical patent/DE69923935T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • 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
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
DE69923935T 1998-12-22 1999-12-22 Montagemethode für eine Turbomaschine Expired - Lifetime DE69923935T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US218705 1998-12-22
US09/218,705 US6148518A (en) 1998-12-22 1998-12-22 Method of assembling a rotary machine

Publications (2)

Publication Number Publication Date
DE69923935D1 true DE69923935D1 (de) 2005-04-07
DE69923935T2 DE69923935T2 (de) 2006-04-06

Family

ID=22816151

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69923935T Expired - Lifetime DE69923935T2 (de) 1998-12-22 1999-12-22 Montagemethode für eine Turbomaschine

Country Status (7)

Country Link
US (1) US6148518A (de)
EP (1) EP1013888B1 (de)
JP (1) JP2000186571A (de)
KR (1) KR100678528B1 (de)
DE (1) DE69923935T2 (de)
SG (1) SG79251A1 (de)
TW (1) TW386137B (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6341419B1 (en) * 2000-02-29 2002-01-29 General Electric Company Loop stacked rotor assembly
US6898547B1 (en) * 2000-09-11 2005-05-24 Axiam, Incorporated Rotor assembly system and method
US7565257B2 (en) * 2000-09-11 2009-07-21 Axiam, Incorporated System for optimal alignment of a bearing seal on a shaft of a gas turbine
US7765082B2 (en) * 2000-09-11 2010-07-27 Axiam, Incorporated System for optimal alignment of a shaft of a gas turbine
GB2388161A (en) * 2002-05-02 2003-11-05 Rolls Royce Plc Gas turbine engine compressor casing
EP1969222B1 (de) * 2005-12-12 2012-11-21 United Technologies Corporation Lagerartige struktur zur steuerung von durchbiegungen eines rotierenden teils
FR2898641B1 (fr) * 2006-03-17 2008-05-02 Snecma Sa Habillage de carter dans un turboreacteur
US8950069B2 (en) * 2006-12-29 2015-02-10 Rolls-Royce North American Technologies, Inc. Integrated compressor vane casing
US7854586B2 (en) * 2007-05-31 2010-12-21 United Technologies Corporation Inlet guide vane inner air seal surge retaining mechanism
US9157723B2 (en) 2009-01-30 2015-10-13 Axiam, Inc. Absolute diameter measurement arm
US8219353B2 (en) * 2009-01-30 2012-07-10 Axiam, Inc. Absolute diameter measurement arm
US8684669B2 (en) * 2011-02-15 2014-04-01 Siemens Energy, Inc. Turbine tip clearance measurement
US8777793B2 (en) 2011-04-27 2014-07-15 United Technologies Corporation Fan drive planetary gear system integrated carrier and torque frame
US9322280B2 (en) * 2011-08-12 2016-04-26 United Technologies Corporation Method of measuring turbine blade tip erosion
US9890648B2 (en) * 2012-01-05 2018-02-13 General Electric Company Turbine rotor rim seal axial retention assembly
US20130192198A1 (en) 2012-01-31 2013-08-01 Lisa I. Brilliant Compressor flowpath
US8863491B2 (en) 2012-01-31 2014-10-21 United Technologies Corporation Gas turbine engine shaft bearing configuration
US10400629B2 (en) 2012-01-31 2019-09-03 United Technologies Corporation Gas turbine engine shaft bearing configuration
US9038366B2 (en) 2012-01-31 2015-05-26 United Technologies Corporation LPC flowpath shape with gas turbine engine shaft bearing configuration
US9322337B2 (en) 2012-06-20 2016-04-26 United Technologies Corporation Aerodynamic intercompressor bleed ports
US9957826B2 (en) 2014-06-09 2018-05-01 United Technologies Corporation Stiffness controlled abradeable seal system with max phase materials and methods of making same
US10808720B2 (en) * 2016-06-21 2020-10-20 Rolls-Royce Corporation Axial flow compressor assembly
US10934943B2 (en) 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US10914318B2 (en) 2019-01-10 2021-02-09 General Electric Company Engine casing treatment for reducing circumferentially variable distortion
CN112747037B (zh) * 2019-10-31 2023-04-07 新疆金风科技股份有限公司 轴系结构、密封组件以及风力发电机组

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3183007A (en) * 1961-05-15 1965-05-11 Tann Corp Seal employing oil-impregnated wicking material and method of making
BE789908A (fr) * 1972-02-29 1973-02-01 Federal Mogul Corp Palier pour vitesses elevees equipe d'un dispositif d'etancheite sensible a la pression de l'air
US4016636A (en) * 1974-07-23 1977-04-12 United Technologies Corporation Compressor construction
JPS5223531A (en) * 1975-08-18 1977-02-22 Nissan Motor Abrasionnresistant sliding member and its production method
FR2370171A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
JPS57234Y2 (de) 1978-01-27 1982-01-05
US4257735A (en) * 1978-12-15 1981-03-24 General Electric Company Gas turbine engine seal and method for making same
US4532054A (en) * 1982-12-28 1985-07-30 General Electric Company Polyetherimide bearing compositions
US4705463A (en) * 1983-04-21 1987-11-10 The Garrett Corporation Compressor wheel assembly for turbochargers
US4611464A (en) * 1984-05-02 1986-09-16 United Technologies Corporation Rotor assembly for a gas turbine engine and method of disassembly
JPS61171607A (ja) * 1985-01-24 1986-08-02 Tokai Kogyo Kk 自動車用密封構成部材
US4730832A (en) * 1985-09-13 1988-03-15 Solar Turbines Incorporated Sealed telescopic joint and method of assembly
US4704075A (en) * 1986-01-24 1987-11-03 Johnston Andrew E Turbocharger water-cooled bearing housing
US4897021A (en) * 1988-06-02 1990-01-30 United Technologies Corporation Stator vane asssembly for an axial flow rotary machine
US4826397A (en) * 1988-06-29 1989-05-02 United Technologies Corporation Stator assembly for a gas turbine engine
US5006114A (en) * 1990-04-20 1991-04-09 Rogers Bobby E Medical valve assembly
US5536022A (en) * 1990-08-24 1996-07-16 United Technologies Corporation Plasma sprayed abradable seals for gas turbine engines
JP2970945B2 (ja) * 1991-01-24 1999-11-02 ユナイテッド テクノロジーズ コーポレイション ガスタービンケースに対する冷却流量の制御方法
US5304032A (en) * 1991-07-22 1994-04-19 Bosna Alexander A Abradable non-metallic seal for rotating turbine engines
US5299910A (en) * 1992-01-23 1994-04-05 General Electric Company Full-round compressor casing assembly in a gas turbine engine
US5205708A (en) * 1992-02-07 1993-04-27 General Electric Company High pressure turbine component interference fit up
US5380155A (en) * 1994-03-01 1995-01-10 United Technologies Corporation Compressor stator assembly
US5456327A (en) * 1994-03-08 1995-10-10 Smith International, Inc. O-ring seal for rock bit bearings
JP3435945B2 (ja) * 1995-11-02 2003-08-11 エヌオーケー株式会社 密封装置の初期潤滑剤塗布方法
US5658127A (en) * 1996-01-26 1997-08-19 Sundstrand Corporation Seal element cooling in high speed mechanical face seals
US5975533A (en) * 1996-09-13 1999-11-02 Brenco, Incorporated Labyrinth-type seal for railway car journal bearing

Also Published As

Publication number Publication date
EP1013888B1 (de) 2005-03-02
JP2000186571A (ja) 2000-07-04
EP1013888A3 (de) 2002-07-31
US6148518A (en) 2000-11-21
TW386137B (en) 2000-04-01
EP1013888A2 (de) 2000-06-28
KR20000048215A (ko) 2000-07-25
DE69923935T2 (de) 2006-04-06
KR100678528B1 (ko) 2007-02-05
SG79251A1 (en) 2001-03-20

Similar Documents

Publication Publication Date Title
DE69923935D1 (de) Montagemethode für eine Turbomaschine
DE60024541D1 (de) Stator für eine Turbomaschine
DE69833538D1 (de) Kühlungskonfiguration für eine Strömungsmaschinenschaufel
DE69920463D1 (de) Zwischendichtung für eine turbine
DE69932966D1 (de) Leitschaufelanordnung für eine Turbomaschine
DE60027650D1 (de) Leitschaufel für eine Strömungsmaschine
DE59811004D1 (de) Herstellungsverfahren für mikromechanische vorrichtung
DE69907773D1 (de) In-Situ Reparaturverfahren für ein Turbomaschinenbauteil.
DE69832110D1 (de) Herstellungsverfahren für eine Prüfnadel für Halbleitergeräte
DE69824817D1 (de) Schwingungsgedämpfte Turbomaschinenschaufel
DE69924920D1 (de) Abdeckung für eine Turbinenleitschaufel
DE69838129D1 (de) Herstellungsverfahren für gewebe
DE69932488D1 (de) Montagemethode für verstellbare Leitschaufeln
ATE226991T1 (de) Einbauverfahren für eine feste schienenfahrbahn
DE69905255D1 (de) Verbesserte verschachteler für turbo-kodes
DE978976T1 (de) Applikationsverteiler für eine Serverapplikation
DE69817638D1 (de) Kompressionssystem für eine Turbomaschine
DE59906444D1 (de) Rotor für eine turbomaschine
DE60018706D1 (de) Kühlverfahren für eine verbrennungsturbine
DE69737340D1 (de) Herstellungsverfahren für eine LED
DE69940428D1 (de) Halterung für eine flugzeug-bordküche
DE59910328D1 (de) Schaufelanordnung für eine Strömungsmaschine
DE69815815D1 (de) Leitbeschaufelung für eine Turbomaschine
DE59804215D1 (de) Herstellungsverfahren für eine mikromechanische vorrichtung
DE69909700D1 (de) Beschichtung für Turbinenkomponenten

Legal Events

Date Code Title Description
8364 No opposition during term of opposition