DE60201718D1 - Befestigung von Statorelementen in einem Turbomaschinengehäuse - Google Patents

Befestigung von Statorelementen in einem Turbomaschinengehäuse

Info

Publication number
DE60201718D1
DE60201718D1 DE60201718T DE60201718T DE60201718D1 DE 60201718 D1 DE60201718 D1 DE 60201718D1 DE 60201718 T DE60201718 T DE 60201718T DE 60201718 T DE60201718 T DE 60201718T DE 60201718 D1 DE60201718 D1 DE 60201718D1
Authority
DE
Germany
Prior art keywords
attachment
stator elements
turbomachine housing
turbomachine
housing
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
DE60201718T
Other languages
English (en)
Other versions
DE60201718T2 (de
Inventor
Francois Crozet
Daniel Didier
Christian Ducrocq
Sebastien Imbourg
Laurent Palmisano
Jean-Marc Rongvaux
Andre Verbrugge
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
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 SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE60201718D1 publication Critical patent/DE60201718D1/de
Publication of DE60201718T2 publication Critical patent/DE60201718T2/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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • F01D25/145—Thermally insulated casings
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Gasket Seals (AREA)
DE60201718T 2001-08-30 2002-08-29 Befestigung von Statorelementen in einem Turbomaschinengehäuse Expired - Lifetime DE60201718T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0111232A FR2829176B1 (fr) 2001-08-30 2001-08-30 Carter de stator de turbomachine
FR0111232 2001-08-30

Publications (2)

Publication Number Publication Date
DE60201718D1 true DE60201718D1 (de) 2004-12-02
DE60201718T2 DE60201718T2 (de) 2006-02-09

Family

ID=8866814

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60201718T Expired - Lifetime DE60201718T2 (de) 2001-08-30 2002-08-29 Befestigung von Statorelementen in einem Turbomaschinengehäuse

Country Status (12)

Country Link
US (1) US7070387B2 (de)
EP (1) EP1288444B1 (de)
JP (1) JP4279667B2 (de)
CN (1) CN1325765C (de)
CA (1) CA2457892C (de)
DE (1) DE60201718T2 (de)
ES (1) ES2229067T3 (de)
FR (1) FR2829176B1 (de)
MA (1) MA26137A1 (de)
RU (1) RU2324057C2 (de)
UA (1) UA76185C2 (de)
WO (1) WO2003018962A1 (de)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10359730A1 (de) * 2003-12-19 2005-07-14 Mtu Aero Engines Gmbh Turbomaschine, insbesondere Gasturbine
FR2868467B1 (fr) * 2004-04-05 2006-06-02 Snecma Moteurs Sa Carter de turbine a crochets refractaires obtenu par procede mdp
FR2871398B1 (fr) * 2004-06-15 2006-09-29 Snecma Moteurs Sa Procede de fabrication d'un carter de stator de turbine
FR2891583B1 (fr) * 2005-09-30 2010-06-18 Snecma Turbine comportant des secteurs d'etancheite demontables par l'amont
US20090096174A1 (en) * 2007-02-28 2009-04-16 United Technologies Corporation Blade outer air seal for a gas turbine engine
FR2914017B1 (fr) * 2007-03-20 2011-07-08 Snecma Dispositif d'etancheite pour un circuit de refroidissement, carter inter-turbine en etant equipe et turboreacteur les comportant
US7811054B2 (en) * 2007-05-30 2010-10-12 General Electric Company Shroud configuration having sloped seal
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
US8439639B2 (en) * 2008-02-24 2013-05-14 United Technologies Corporation Filter system for blade outer air seal
FR2933458B1 (fr) * 2008-07-01 2010-09-03 Snecma Compresseur axialo-centrifuge a systeme de pilotage
US8794913B2 (en) * 2008-08-11 2014-08-05 Mitsubishi Heavy Industries, Ltd. Steam turbine facility
EP2184445A1 (de) * 2008-11-05 2010-05-12 Siemens Aktiengesellschaft Axial segmentierter Leitschaufelträger für einen Gasturbine
US8939715B2 (en) * 2010-03-22 2015-01-27 General Electric Company Active tip clearance control for shrouded gas turbine blades and related method
US8668431B2 (en) * 2010-03-29 2014-03-11 United Technologies Corporation Seal clearance control on non-cowled gas turbine engines
FR2965010B1 (fr) * 2010-09-17 2015-02-20 Snecma Refroidissement de la paroi exterieure d'un carter de turbine
ITCO20110060A1 (it) * 2011-12-12 2013-06-13 Nuovo Pignone Spa Turbina a vapore, paletta e metodo
FR2984428B1 (fr) * 2011-12-19 2018-12-07 Safran Aircraft Engines Redresseur de compresseur pour turbomachine.
EP2647796A1 (de) * 2012-04-04 2013-10-09 MTU Aero Engines GmbH Dichtungssystem für eine Strömungsmaschine
US9291061B2 (en) * 2012-04-13 2016-03-22 General Electric Company Turbomachine blade tip shroud with parallel casing configuration
ITTO20120519A1 (it) * 2012-06-14 2013-12-15 Avio Spa Turbina a gas per motori aeronautici
EP2896796B1 (de) * 2014-01-20 2019-09-18 Safran Aero Boosters SA Stator einer axialen Strömungsmaschine und zugehörige Strömungsmaschine
EP3141705B1 (de) * 2015-09-08 2018-12-26 Ansaldo Energia Switzerland AG Gasturbinenrotorabdeckung
FR3041037B1 (fr) * 2015-09-15 2018-08-17 Safran Aircraft Engines Dispositif de ventilation d'un carter de turbine d'une turbomachine
US10975721B2 (en) 2016-01-12 2021-04-13 Pratt & Whitney Canada Corp. Cooled containment case using internal plenum
US10815824B2 (en) * 2017-04-04 2020-10-27 General Electric Method and system for rotor overspeed protection
US11098649B2 (en) * 2018-07-19 2021-08-24 The Boeing Company Self-regulating back-side pressurization system for thermal insulation blankets
US11015475B2 (en) * 2018-12-27 2021-05-25 Rolls-Royce Corporation Passive blade tip clearance control system for gas turbine engine
RU190280U1 (ru) * 2019-01-09 2019-06-25 Публичное Акционерное Общество "Одк-Сатурн" Устройство для фиксации сегментов сопловых лопаток в силовом корпусе статора турбины
FR3098849B1 (fr) * 2019-07-16 2022-10-14 Safran Aircraft Engines Carter amélioré de module d’aéronef
CN112302729B (zh) * 2019-07-31 2022-10-11 中国航发商用航空发动机有限责任公司 航空发动机涡轮静子组件及航空发动机
GB2614760A (en) * 2022-01-13 2023-07-19 Rolls Royce Plc Turbine for gas turbine engine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
US4019320A (en) * 1975-12-05 1977-04-26 United Technologies Corporation External gas turbine engine cooling for clearance control
US4131388A (en) * 1977-05-26 1978-12-26 United Technologies Corporation Outer air seal
GB2076071B (en) * 1980-05-16 1983-11-02 United Technologies Corp Flow directing assembly for a gas turbine engine
GB2115487B (en) * 1982-02-19 1986-02-05 Gen Electric Double wall compressor casing
US4522559A (en) * 1982-02-19 1985-06-11 General Electric Company Compressor casing
GB2117843B (en) * 1982-04-01 1985-11-06 Rolls Royce Compressor shrouds
FR2635562B1 (fr) * 1988-08-18 1993-12-24 Snecma Anneau de stator de turbine associe a un support de liaison au carter de turbine
GB2226365B (en) * 1988-12-22 1993-03-10 Rolls Royce Plc Turbomachine clearance control
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
US5180281A (en) * 1990-09-12 1993-01-19 United Technologies Corporation Case tying means for gas turbine engine
FR2683851A1 (fr) * 1991-11-20 1993-05-21 Snecma Turbomachine equipee de moyens facilitant le reglage des jeux du stator entree stator et rotor.
GB9306719D0 (en) * 1993-03-31 1993-06-02 Rolls Royce Plc A turbine assembly for a gas turbine engine
FR2711730B1 (fr) * 1993-10-27 1995-12-01 Snecma Turbomachine équipée de moyens de pilotage des jeux entre rotor et stator.
DE4442157A1 (de) * 1994-11-26 1996-05-30 Abb Management Ag Verfahren und Vorrichtung zur Beeinflussung des Radialspieles der Beschaufelung in axialdurchströmten Verdichtern
US5653581A (en) * 1994-11-29 1997-08-05 United Technologies Corporation Case-tied joint for compressor stators
FR2766232B1 (fr) * 1997-07-18 1999-08-20 Snecma Dispositif de refroidissement ou d'echauffement d'un carter circulaire
US6179560B1 (en) * 1998-12-16 2001-01-30 United Technologies Corporation Turbomachinery module with improved maintainability

Also Published As

Publication number Publication date
JP2005501192A (ja) 2005-01-13
CN1549887A (zh) 2004-11-24
WO2003018962A1 (fr) 2003-03-06
US20040184912A1 (en) 2004-09-23
EP1288444B1 (de) 2004-10-27
ES2229067T3 (es) 2005-04-16
CN1325765C (zh) 2007-07-11
UA76185C2 (uk) 2006-07-17
CA2457892C (fr) 2011-02-08
DE60201718T2 (de) 2006-02-09
JP4279667B2 (ja) 2009-06-17
EP1288444A1 (de) 2003-03-05
FR2829176A1 (fr) 2003-03-07
RU2324057C2 (ru) 2008-05-10
US7070387B2 (en) 2006-07-04
CA2457892A1 (fr) 2003-03-06
RU2004109232A (ru) 2005-05-20
FR2829176B1 (fr) 2005-06-24
MA26137A1 (fr) 2004-04-01

Similar Documents

Publication Publication Date Title
DE60201718D1 (de) Befestigung von Statorelementen in einem Turbomaschinengehäuse
DE60114696D1 (de) Turbinengehäuse
DE60114697D1 (de) Turbinengehäuse
DE50306097D1 (de) Abgasturbinengehäuse
DE59905762D1 (de) Turbinengehäuse
DE60138579D1 (de) Beschaufelte Rotoranordnung
DE60120875D1 (de) Beschaufelter Rotor
DE50312707D1 (de) Abgasturbinengehäuse
DE60026687D1 (de) Statorstufe eines Verdichters
DE60136101D1 (de) Isoelektronische kodotierung
DE69908741D1 (de) Flügelzellenpumpe
DE69926438D1 (de) Flügelzellenpumpe
DE60200172D1 (de) Motorgehäuse
DE60026686D1 (de) Statorstufe eines Verdichters
FR2761119B1 (fr) Stator de compresseur de turbomachine
DE59805746D1 (de) Turbinengehäuse
DE60214841D1 (de) Hermetischer elektrischer kompressor
FR2834751B1 (fr) Amenagement de rotor d'une turbomachine
DE60202032D1 (de) Anordnung von Statorsegmenten in einer Turbomaschine
DE60120549D1 (de) Turbinenstator
DE50203631D1 (de) Flügelzellenpumpe
DE50209302D1 (de) Motorgehäuse
DE50202731D1 (de) Gehäuse
DE19880474D2 (de) Flügelzellenpumpe
FR2828631B1 (fr) Engin automoteur a conducteur embarque

Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR