FR1138118A - Dispositif annulaire d'étanchéité pour turbines et compresseurs - Google Patents

Dispositif annulaire d'étanchéité pour turbines et compresseurs

Info

Publication number
FR1138118A
FR1138118A FR1138118DA FR1138118A FR 1138118 A FR1138118 A FR 1138118A FR 1138118D A FR1138118D A FR 1138118DA FR 1138118 A FR1138118 A FR 1138118A
Authority
FR
France
Prior art keywords
compressors
turbines
sealing device
annular sealing
annular
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
Application number
Other languages
English (en)
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Application granted granted Critical
Publication of FR1138118A publication Critical patent/FR1138118A/fr
Expired 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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1138118D 1954-12-16 1955-12-16 Dispositif annulaire d'étanchéité pour turbines et compresseurs Expired FR1138118A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB345766X 1954-12-16

Publications (1)

Publication Number Publication Date
FR1138118A true FR1138118A (fr) 1957-06-11

Family

ID=10367346

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1138118D Expired FR1138118A (fr) 1954-12-16 1955-12-16 Dispositif annulaire d'étanchéité pour turbines et compresseurs

Country Status (7)

Country Link
US (1) US2863634A (fr)
BE (1) BE543709A (fr)
CH (1) CH345766A (fr)
DE (1) DE1080119B (fr)
FR (1) FR1138118A (fr)
GB (1) GB785466A (fr)
NL (2) NL202529A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2852053A1 (fr) * 2003-03-06 2004-09-10 Snecma Moteurs Turbine haute pression pour turbomachine

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1286810B (de) * 1963-11-19 1969-01-09 Licentia Gmbh Laufschaufelradialspalt-Abdeckring einer Axialturbomaschine, insbesondere -gasturbine
CH425341A (de) * 1965-07-23 1966-11-30 Bbc Brown Boveri & Cie Gasturbine mit Kühlung der Schaufelträger
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
US3520635A (en) * 1968-11-04 1970-07-14 Avco Corp Turbomachine shroud assembly
US3689174A (en) * 1971-01-11 1972-09-05 Westinghouse Electric Corp Axial flow turbine structure
BE792224A (fr) * 1971-12-01 1973-03-30 Penny Robert N Element composite long ayant un coefficient de dilatation lineaire effectif predetermine
GB1335145A (en) * 1972-01-12 1973-10-24 Rolls Royce Turbine casing for a gas turbine engine
US3807891A (en) * 1972-09-15 1974-04-30 United Aircraft Corp Thermal response turbine shroud
US3986720A (en) * 1975-04-14 1976-10-19 General Electric Company Turbine shroud structure
US4013376A (en) * 1975-06-02 1977-03-22 United Technologies Corporation Coolable blade tip shroud
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
DE3063386D1 (en) * 1979-01-15 1983-07-07 Carding Spec Canada Gas compressor or blower
GB2047354B (en) * 1979-04-26 1983-03-30 Rolls Royce Gas turbine engines
FR2455674A1 (fr) * 1979-05-02 1980-11-28 Snecma Dispositif d'etancheite entre deux elements de turbomachine
US4355952A (en) * 1979-06-29 1982-10-26 Westinghouse Electric Corp. Combustion turbine vane assembly
DE3018621C2 (de) * 1980-05-16 1982-06-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Außengehäuse für Axialverdichter oder -turbinen von Strömungsmaschinen, insbesondere Gasturbinentriebwerken
JPS59167919U (ja) * 1983-04-27 1984-11-10 カルソニックカンセイ株式会社 ファンシュラウド
US4921401A (en) * 1989-02-23 1990-05-01 United Technologies Corporation Casting for a rotary machine
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
US5297932A (en) * 1990-09-12 1994-03-29 United Technologies Corporation Fastener for multi-stage compressor
US5158430A (en) * 1990-09-12 1992-10-27 United Technologies Corporation Segmented stator vane seal
US5131811A (en) * 1990-09-12 1992-07-21 United Technologies Corporation Fastener mounting for multi-stage compressor
US5221096A (en) * 1990-10-19 1993-06-22 Allied-Signal Inc. Stator and multiple piece seal
US5088888A (en) * 1990-12-03 1992-02-18 General Electric Company Shroud seal
US5823741A (en) * 1996-09-25 1998-10-20 General Electric Co. Cooling joint connection for abutting segments in a gas turbine engine
NL1014013C2 (nl) * 2000-01-05 2001-07-18 Ventilatoren Sirocco Howden Bv Behuizingsdeel voor een ventilatorwaaier.
US6464453B2 (en) * 2000-12-04 2002-10-15 General Electric Company Turbine interstage sealing ring
US7063503B2 (en) * 2004-04-15 2006-06-20 Pratt & Whitney Canada Corp. Turbine shroud cooling system
RU2547351C2 (ru) 2010-11-29 2015-04-10 Альстом Текнолоджи Лтд Осевая газовая турбина
JP6271077B2 (ja) 2014-07-24 2018-01-31 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ ガスタービンエンジン内で使用可能なステータベーンシステム
EP3209865B1 (fr) * 2014-10-23 2021-05-05 Siemens Energy, Inc. Moteur à turbine à gaz avec système de commande de dégagement d'extrémité de pale de turbine
PL415534A1 (pl) * 2016-01-04 2017-07-17 General Electric Company Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych
US20200072070A1 (en) * 2018-09-05 2020-03-05 United Technologies Corporation Unified boas support and vane platform

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE185427C (fr) * 1904-11-17 1907-06-11
FR625938A (fr) * 1926-03-24 1927-08-23 Rateau Sa Dispositif de fixation de tuyères distributrices pour turbines à vapeur
US2510606A (en) * 1943-05-22 1950-06-06 Lockheed Aircraft Corp Turbine construction
CH270334A (de) * 1945-01-16 1950-08-31 Power Jets Res & Dev Ltd Schaufelträger in axialen Kreiselmaschinen.
BE463344A (fr) * 1945-01-23
GB597165A (en) * 1945-01-23 1948-01-20 Power Jets Res & Dev Ltd Improvements relating to the construction of stator elements of turbines, compressors or like machines
GB618525A (en) * 1946-06-18 1949-02-23 Adrian Albert Lombard Improvements in or relating to gas-turbine engines
GB679916A (en) * 1949-04-29 1952-09-24 Geoffrey Bertram Robert Feilde Improvements in gas turbines
US2685429A (en) * 1950-01-31 1954-08-03 Gen Electric Dynamic sealing arrangement for turbomachines
GB721453A (en) * 1951-10-19 1955-01-05 Vickers Electrical Co Ltd Improvements relating to gas turbines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2852053A1 (fr) * 2003-03-06 2004-09-10 Snecma Moteurs Turbine haute pression pour turbomachine
US7011493B2 (en) 2003-03-06 2006-03-14 Snecma Moteurs Turbomachine with cooled ring segments

Also Published As

Publication number Publication date
GB785466A (en) 1957-10-30
US2863634A (en) 1958-12-09
CH345766A (fr) 1960-04-15
DE1080119B (de) 1960-04-21
NL103792C (fr)
BE543709A (fr)
NL202529A (fr)

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