BE543709A - - Google Patents

Info

Publication number
BE543709A
BE543709A BE543709DA BE543709A BE 543709 A BE543709 A BE 543709A BE 543709D A BE543709D A BE 543709DA BE 543709 A BE543709 A BE 543709A
Authority
BE
Belgium
Application number
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.)
Publication of BE543709A publication Critical patent/BE543709A/xx

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
BE543709D 1954-12-16 BE543709A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BE543709A true BE543709A (en)

Family

ID=10367346

Family Applications (1)

Application Number Title Priority Date Filing Date
BE543709D BE543709A (en) 1954-12-16

Country Status (7)

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

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1286810B (en) * 1963-11-19 1969-01-09 Licentia Gmbh Rotor blade radial gap cover ring of an axial turbine machine, in particular a gas turbine
CH425341A (en) * 1965-07-23 1966-11-30 Bbc Brown Boveri & Cie Gas turbine with cooling of the blade carriers
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 (en) * 1971-12-01 1973-03-30 Penny Robert N LONG COMPOSITE ELEMENT WITH A PREDETERMINED EFFECTIVE LINEAR EXPANSION COEFFICIENT
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
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
US4013376A (en) * 1975-06-02 1977-03-22 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 (en) * 1979-05-02 1980-11-28 Snecma SEALING DEVICE BETWEEN TWO TURBOMACHINE ELEMENTS
US4355952A (en) * 1979-06-29 1982-10-26 Westinghouse Electric Corp. Combustion turbine vane assembly
DE3018621C2 (en) * 1980-05-16 1982-06-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Outer casing for axial compressors or turbines of flow machines, in particular gas turbine engines
JPS59167919U (en) * 1983-04-27 1984-11-10 カルソニックカンセイ株式会社 fan shroud
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
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
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
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 (en) * 2000-01-05 2001-07-18 Ventilatoren Sirocco Howden Bv Housing part for a fan impeller.
US6464453B2 (en) * 2000-12-04 2002-10-15 General Electric Company Turbine interstage sealing ring
FR2852053B1 (en) * 2003-03-06 2007-12-28 Snecma Moteurs HIGH PRESSURE TURBINE FOR TURBOMACHINE
US7063503B2 (en) * 2004-04-15 2006-06-20 Pratt & Whitney Canada Corp. Turbine shroud cooling system
RU2547351C2 (en) 2010-11-29 2015-04-10 Альстом Текнолоджи Лтд Axial gas turbine
JP6271077B2 (en) 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 Stator vane system for use in gas turbine engines
US10830083B2 (en) * 2014-10-23 2020-11-10 Siemens Energy, Inc. Gas turbine engine with a turbine blade tip clearance control system
PL415534A1 (en) * 2016-01-04 2017-07-17 General Electric Company System for the shield and partition unit of initial guide vanes
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 (en) * 1904-11-17 1907-06-11
FR625938A (en) * 1926-03-24 1927-08-23 Rateau Sa Fixing device for dispensing nozzles for steam turbines
US2510606A (en) * 1943-05-22 1950-06-06 Lockheed Aircraft Corp Turbine construction
CH270334A (en) * 1945-01-16 1950-08-31 Power Jets Res & Dev Ltd Blade carrier in axial centrifugal machines.
NL70901C (en) * 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

Also Published As

Publication number Publication date
GB785466A (en) 1957-10-30
NL202529A (en)
NL103792C (en)
US2863634A (en) 1958-12-09
FR1138118A (en) 1957-06-11
DE1080119B (en) 1960-04-21
CH345766A (en) 1960-04-15

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