USB563412I5 - - Google Patents

Info

Publication number
USB563412I5
USB563412I5 US56341275D USB563412I5 US B563412 I5 USB563412 I5 US B563412I5 US 56341275 D US56341275 D US 56341275D US B563412 I5 USB563412 I5 US B563412I5
Authority
US
United States
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.)
Pending
Application number
Other languages
English (en)
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 filed Critical
Publication of USB563412I5 publication Critical patent/USB563412I5/en
Pending 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/005—Selecting particular materials
    • 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
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
US56341275 1975-03-28 1975-03-28 Pending USB563412I5 (nl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/563,412 US3992127A (en) 1975-03-28 1975-03-28 Stator vane assembly for gas turbines

Publications (1)

Publication Number Publication Date
USB563412I5 true USB563412I5 (nl) 1976-02-24

Family

ID=24250381

Family Applications (2)

Application Number Title Priority Date Filing Date
US56341275 Pending USB563412I5 (nl) 1975-03-28 1975-03-28
US05/563,412 Expired - Lifetime US3992127A (en) 1975-03-28 1975-03-28 Stator vane assembly for gas turbines

Family Applications After (1)

Application Number Title Priority Date Filing Date
US05/563,412 Expired - Lifetime US3992127A (en) 1975-03-28 1975-03-28 Stator vane assembly for gas turbines

Country Status (3)

Country Link
US (2) USB563412I5 (nl)
JP (1) JPS51120310A (nl)
CA (1) CA1017678A (nl)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0355312A1 (de) * 1988-08-03 1990-02-28 Asea Brown Boveri Ag Axialdurchströmte Turbine mit radial-axialer erster Stufe
WO1991007572A1 (en) * 1989-11-20 1991-05-30 Allied-Signal Inc. High temperature turbine engine structure
US5228284A (en) * 1988-12-06 1993-07-20 Allied-Signal Inc. High temperature turbine engine structure
US5279031A (en) * 1988-12-06 1994-01-18 Alliedsignal Inc. High temperature turbine engine structure

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2106995B (en) * 1981-09-26 1984-10-03 Rolls Royce Turbine blades
DE4017861A1 (de) * 1990-06-02 1991-12-05 Mtu Muenchen Gmbh Leitkranz fuer eine gasturbine
EP1329592A1 (de) * 2002-01-18 2003-07-23 Siemens Aktiengesellschaft Turbine mit mindestens vier Stufen und Verwendung einer Turbinenschaufel mit verringerter Masse
EP1489264A1 (de) * 2003-06-18 2004-12-22 Siemens Aktiengesellschaft Modular aufgebaute Schaufel
US20050129340A1 (en) * 2003-12-10 2005-06-16 Arnold Robert A. Hourglass bearing
US7452182B2 (en) * 2005-04-07 2008-11-18 Siemens Energy, Inc. Multi-piece turbine vane assembly
US7316539B2 (en) * 2005-04-07 2008-01-08 Siemens Power Generation, Inc. Vane assembly with metal trailing edge segment
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
US7824152B2 (en) * 2007-05-09 2010-11-02 Siemens Energy, Inc. Multivane segment mounting arrangement for a gas turbine
WO2009157817A1 (en) * 2008-06-26 2009-12-30 Volvo Aero Corporation Vane assembly and method of fabricating, and a turbo-machine with such vane assembly
US8251652B2 (en) * 2008-09-18 2012-08-28 Siemens Energy, Inc. Gas turbine vane platform element
EP3505727A1 (en) 2013-03-10 2019-07-03 Rolls-Royce Corporation Gas turbine engines and corresponding method
US11118471B2 (en) * 2013-11-18 2021-09-14 Raytheon Technologies Corporation Variable area vane endwall treatments
US10132186B2 (en) 2015-08-13 2018-11-20 General Electric Company System and method for supporting a turbine shroud
US10626739B2 (en) * 2015-10-27 2020-04-21 Mitsubishi Heavy Industries, Ltd. Rotary machine
US11448078B2 (en) * 2020-04-23 2022-09-20 Raytheon Technologies Corporation Spring loaded airfoil vane
US11512604B1 (en) * 2021-05-04 2022-11-29 Raytheon Technologies Corporation Spring for radially stacked assemblies
US12055058B2 (en) * 2022-05-31 2024-08-06 Pratt & Whitney Canada Corp. Joint between gas turbine engine components with a spring element

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1891948A (en) * 1931-10-02 1932-12-27 Gen Electric Elastic fluid turbine
AU226940A (en) * 1940-06-07 1941-06-19 William Dougherty David Improved regulator for automobile windows
DE826673C (de) * 1945-04-04 1952-01-03 Maschf Augsburg Nuernberg Ag Leitapparat mit keramischen Leitschaufeln
US2595829A (en) * 1946-12-19 1952-05-06 Benson Mfg Company Axial flow fan and compressor
DE846342C (de) * 1944-11-26 1952-08-11 Maschf Augsburg Nuernberg Ag Turbinenleitapparat aus keramischen Werkstoffen
DE919802C (de) * 1952-09-06 1954-11-04 Maschf Augsburg Nuernberg Ag Einrichtung zur Befestigung von Laufschaufeln fuer axial durchstroemte Kreiselradmaschinen
US2801076A (en) * 1952-11-18 1957-07-30 Parsons & Marine Eng Turbine Turbine nozzles
US2819869A (en) * 1950-05-02 1958-01-14 Jr Andre J Meyer Mounting arrangement for turbine or compressor blading
US3843279A (en) * 1972-06-21 1974-10-22 Rolls Royce 1971 Ltd Stator assembly for gas turbine engines which accommodate circumferential and axial expansion of engine components
US3857649A (en) * 1973-08-09 1974-12-31 Westinghouse Electric Corp Inlet vane structure for turbines
US3864056A (en) * 1973-07-27 1975-02-04 Westinghouse Electric Corp Cooled turbine blade ring assembly
US3867065A (en) * 1973-07-16 1975-02-18 Westinghouse Electric Corp Ceramic insulator for a gas turbine blade structure

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US387649A (en) * 1888-08-14 Conveyer-bucket

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1891948A (en) * 1931-10-02 1932-12-27 Gen Electric Elastic fluid turbine
AU226940A (en) * 1940-06-07 1941-06-19 William Dougherty David Improved regulator for automobile windows
DE846342C (de) * 1944-11-26 1952-08-11 Maschf Augsburg Nuernberg Ag Turbinenleitapparat aus keramischen Werkstoffen
DE826673C (de) * 1945-04-04 1952-01-03 Maschf Augsburg Nuernberg Ag Leitapparat mit keramischen Leitschaufeln
US2595829A (en) * 1946-12-19 1952-05-06 Benson Mfg Company Axial flow fan and compressor
US2819869A (en) * 1950-05-02 1958-01-14 Jr Andre J Meyer Mounting arrangement for turbine or compressor blading
DE919802C (de) * 1952-09-06 1954-11-04 Maschf Augsburg Nuernberg Ag Einrichtung zur Befestigung von Laufschaufeln fuer axial durchstroemte Kreiselradmaschinen
US2801076A (en) * 1952-11-18 1957-07-30 Parsons & Marine Eng Turbine Turbine nozzles
US3843279A (en) * 1972-06-21 1974-10-22 Rolls Royce 1971 Ltd Stator assembly for gas turbine engines which accommodate circumferential and axial expansion of engine components
US3867065A (en) * 1973-07-16 1975-02-18 Westinghouse Electric Corp Ceramic insulator for a gas turbine blade structure
US3864056A (en) * 1973-07-27 1975-02-04 Westinghouse Electric Corp Cooled turbine blade ring assembly
US3857649A (en) * 1973-08-09 1974-12-31 Westinghouse Electric Corp Inlet vane structure for turbines

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0355312A1 (de) * 1988-08-03 1990-02-28 Asea Brown Boveri Ag Axialdurchströmte Turbine mit radial-axialer erster Stufe
CH676735A5 (nl) * 1988-08-03 1991-02-28 Asea Brown Boveri
EP0355312B1 (de) * 1988-08-03 1993-02-10 Asea Brown Boveri Ag Axialdurchströmte Turbine mit radial-axialer erster Stufe
US5116158A (en) * 1988-12-06 1992-05-26 Allied-Signal Inc. High temperature turbine engine structure
US5228284A (en) * 1988-12-06 1993-07-20 Allied-Signal Inc. High temperature turbine engine structure
US5279031A (en) * 1988-12-06 1994-01-18 Alliedsignal Inc. High temperature turbine engine structure
WO1991007572A1 (en) * 1989-11-20 1991-05-30 Allied-Signal Inc. High temperature turbine engine structure

Also Published As

Publication number Publication date
JPS561446B2 (nl) 1981-01-13
JPS51120310A (en) 1976-10-21
CA1017678A (en) 1977-09-20
US3992127A (en) 1976-11-16

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