JPS5335205B2 - - Google Patents

Info

Publication number
JPS5335205B2
JPS5335205B2 JP6111575A JP6111575A JPS5335205B2 JP S5335205 B2 JPS5335205 B2 JP S5335205B2 JP 6111575 A JP6111575 A JP 6111575A JP 6111575 A JP6111575 A JP 6111575A JP S5335205 B2 JPS5335205 B2 JP S5335205B2
Authority
JP
Japan
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
JP6111575A
Other languages
Japanese (ja)
Other versions
JPS511820A (en:Method
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 JPS511820A publication Critical patent/JPS511820A/ja
Publication of JPS5335205B2 publication Critical patent/JPS5335205B2/ja
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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/24—Three-dimensional ellipsoidal
    • F05D2250/241—Three-dimensional ellipsoidal spherical
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
JP6111575A 1974-05-23 1975-05-23 Expired JPS5335205B2 (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US472753A US3910716A (en) 1974-05-23 1974-05-23 Gas turbine inlet vane structure utilizing a stable ceramic spherical interface arrangement

Publications (2)

Publication Number Publication Date
JPS511820A JPS511820A (en:Method) 1976-01-09
JPS5335205B2 true JPS5335205B2 (en:Method) 1978-09-26

Family

ID=23876805

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6111575A Expired JPS5335205B2 (en:Method) 1974-05-23 1975-05-23

Country Status (4)

Country Link
US (1) US3910716A (en:Method)
JP (1) JPS5335205B2 (en:Method)
CA (1) CA1001953A (en:Method)
IT (1) IT1038328B (en:Method)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4076451A (en) * 1976-03-05 1978-02-28 United Technologies Corporation Ceramic turbine stator
JPS5829308Y2 (ja) * 1977-01-22 1983-06-27 日信工業株式会社 二輪車用デイスクブレ−キにおける固定摩擦パツドの取付装置
FR2456836A1 (fr) * 1979-05-18 1980-12-12 Avco Corp Tuyere composite en metal et ceramique, pour turbine
US4312599A (en) * 1979-10-22 1982-01-26 General Electric Company High temperature article, article retainer, and cushion
US4302149A (en) * 1980-02-19 1981-11-24 General Motors Corporation Ceramic vane drive joint
US4832568A (en) * 1982-02-26 1989-05-23 General Electric Company Turbomachine airfoil mounting assembly
JPS59177702U (ja) * 1984-04-12 1984-11-28 三菱重工業株式会社 ラジアル型タ−ビンノズル
US4643636A (en) * 1985-07-22 1987-02-17 Avco Corporation Ceramic nozzle assembly for gas turbine engine
US4768924A (en) * 1986-07-22 1988-09-06 Pratt & Whitney Canada Inc. Ceramic stator vane assembly
US4861229A (en) * 1987-11-16 1989-08-29 Williams International Corporation Ceramic-matrix composite nozzle assembly for a turbine engine
CH676735A5 (en:Method) * 1988-08-03 1991-02-28 Asea Brown Boveri
US5074752A (en) * 1990-08-06 1991-12-24 General Electric Company Gas turbine outlet guide vane mounting assembly
US5141395A (en) * 1991-09-05 1992-08-25 General Electric Company Flow activated flowpath liner seal
ITMI991206A1 (it) * 1999-05-31 2000-12-01 Nuovo Pignone Spa Dispositivo di supporto e bloccaggio per ugelli di uno stadio ad altapressione in turbine a gas
US6648597B1 (en) 2002-05-31 2003-11-18 Siemens Westinghouse Power Corporation Ceramic matrix composite turbine vane
US6709230B2 (en) 2002-05-31 2004-03-23 Siemens Westinghouse Power Corporation Ceramic matrix composite gas turbine vane
US7093359B2 (en) 2002-09-17 2006-08-22 Siemens Westinghouse Power Corporation Composite structure formed by CMC-on-insulation process
US9068464B2 (en) * 2002-09-17 2015-06-30 Siemens Energy, Inc. Method of joining ceramic parts and articles so formed
US20050220622A1 (en) * 2004-03-31 2005-10-06 General Electric Company Integral covered nozzle with attached overcover
US7435058B2 (en) * 2005-01-18 2008-10-14 Siemens Power Generation, Inc. Ceramic matrix composite vane with chordwise stiffener
US8256088B2 (en) * 2009-08-24 2012-09-04 Siemens Energy, Inc. Joining mechanism with stem tension and interlocked compression ring
US9279335B2 (en) 2011-08-03 2016-03-08 United Technologies Corporation Vane assembly for a gas turbine engine
US9273565B2 (en) * 2012-02-22 2016-03-01 United Technologies Corporation Vane assembly for a gas turbine engine
US9121301B2 (en) * 2012-03-20 2015-09-01 General Electric Company Thermal isolation apparatus
CA2899891A1 (en) 2013-03-14 2014-10-02 Adam L. CHAMBERLAIN Bi-cast turbine vane
US9492780B2 (en) 2014-01-16 2016-11-15 Bha Altair, Llc Gas turbine inlet gas phase contaminant removal
US10502136B2 (en) 2014-10-06 2019-12-10 Bha Altair, Llc Filtration system for use in a gas turbine engine assembly and method of assembling thereof
EP3315729A1 (de) 2016-10-26 2018-05-02 MTU Aero Engines GmbH Ellipsoidische innere leitschaufellagerung
US10260362B2 (en) 2017-05-30 2019-04-16 Rolls-Royce Corporation Turbine vane assembly with ceramic matrix composite airfoil and friction fit metallic attachment features
DE202021004007U1 (de) * 2020-10-21 2022-05-02 3BE Berliner Beratungs- und Beteiligungs-Gesellschaft mbH Radialgasturbine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3066911A (en) * 1959-05-12 1962-12-04 Thompson Ramo Wooldridge Inc Nozzle and turbine wheel shroud support
GB1387866A (en) * 1972-06-21 1975-03-19 Rolls Royce Aerofoil members for gas turbine engines

Also Published As

Publication number Publication date
CA1001953A (en) 1976-12-21
US3910716A (en) 1975-10-07
JPS511820A (en:Method) 1976-01-09
IT1038328B (it) 1979-11-20

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