AR231564A1 - Estructura de alabe de estator para una turbina fundida por el procedimiento de cera perdida,de una sola pieza - Google Patents

Estructura de alabe de estator para una turbina fundida por el procedimiento de cera perdida,de una sola pieza

Info

Publication number
AR231564A1
AR231564A1 AR292016A AR29201683A AR231564A1 AR 231564 A1 AR231564 A1 AR 231564A1 AR 292016 A AR292016 A AR 292016A AR 29201683 A AR29201683 A AR 29201683A AR 231564 A1 AR231564 A1 AR 231564A1
Authority
AR
Argentina
Prior art keywords
single piece
stator blade
blade structure
lost wax
turbine cast
Prior art date
Application number
AR292016A
Other languages
English (en)
Spanish (es)
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Application granted granted Critical
Publication of AR231564A1 publication Critical patent/AR231564A1/es

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AR292016A 1982-02-02 1983-02-02 Estructura de alabe de estator para una turbina fundida por el procedimiento de cera perdida,de una sola pieza AR231564A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/345,125 US4511306A (en) 1982-02-02 1982-02-02 Combustion turbine single airfoil stator vane structure

Publications (1)

Publication Number Publication Date
AR231564A1 true AR231564A1 (es) 1984-12-28

Family

ID=23353635

Family Applications (1)

Application Number Title Priority Date Filing Date
AR292016A AR231564A1 (es) 1982-02-02 1983-02-02 Estructura de alabe de estator para una turbina fundida por el procedimiento de cera perdida,de una sola pieza

Country Status (10)

Country Link
US (1) US4511306A (sv)
JP (1) JPS58138206A (sv)
AR (1) AR231564A1 (sv)
BE (1) BE895761A (sv)
BR (1) BR8300273A (sv)
CA (1) CA1202570A (sv)
GB (1) GB2114234B (sv)
IT (1) IT1193648B (sv)
MX (1) MX155781A (sv)
SE (1) SE453314B (sv)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5071313A (en) * 1990-01-16 1991-12-10 General Electric Company Rotor blade shroud segment
US5248240A (en) * 1993-02-08 1993-09-28 General Electric Company Turbine stator vane assembly
US5662160A (en) * 1995-10-12 1997-09-02 General Electric Co. Turbine nozzle and related casting method for optimal fillet wall thickness control
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
US6517313B2 (en) 2001-06-25 2003-02-11 Pratt & Whitney Canada Corp. Segmented turbine vane support structure
DE10210866C5 (de) * 2002-03-12 2008-04-10 Mtu Aero Engines Gmbh Leitschaufelbefestigung in einem Strömungskanal einer Fluggasturbine
EP1573172B1 (de) * 2002-12-19 2010-12-01 Siemens Aktiengesellschaft Turbine und Arbeitsverfahren zum Ausbau der Leitschaufeln einer Turbine
SE525879C2 (sv) * 2003-03-21 2005-05-17 Volvo Aero Corp Förfarande för framställning av en statorkomponent
JP4269763B2 (ja) * 2003-04-28 2009-05-27 株式会社Ｉｈｉ タービンノズルセグメント
FR2894282A1 (fr) * 2005-12-05 2007-06-08 Snecma Sa Distributeur de turbine de turbomachine ameliore
US7762766B2 (en) * 2006-07-06 2010-07-27 Siemens Energy, Inc. Cantilevered framework support for turbine vane
EP2211023A1 (de) * 2009-01-21 2010-07-28 Siemens Aktiengesellschaft Leitschaufelsystem für eine Strömungsmaschine mit segmentiertem Leitschaufelträger
US9156086B2 (en) 2010-06-07 2015-10-13 Siemens Energy, Inc. Multi-component assembly casting
US8684683B2 (en) * 2010-11-30 2014-04-01 General Electric Company Gas turbine nozzle attachment scheme and removal/installation method
EP2530249A1 (en) * 2011-05-30 2012-12-05 Siemens Aktiengesellschaft Piston seal ring
US8888442B2 (en) 2012-01-30 2014-11-18 Pratt & Whitney Canada Corp. Stress relieving slots for turbine vane ring
EP2706196A1 (en) 2012-09-07 2014-03-12 Siemens Aktiengesellschaft Turbine vane arrangement
WO2015023331A2 (en) * 2013-06-10 2015-02-19 United Technologies Corporation Turbine vane with non-uniform wall thickness
ES2695723T3 (es) 2013-06-14 2019-01-10 United Technologies Corp Alabe de turbina con radio interior variable de borde posterior
WO2014204608A1 (en) * 2013-06-17 2014-12-24 United Technologies Corporation Turbine vane with platform pad
US10876417B2 (en) * 2017-08-17 2020-12-29 Raytheon Technologies Corporation Tuned airfoil assembly
CN111206964A (zh) * 2018-11-22 2020-05-29 中发天信(北京)航空发动机科技股份有限公司 一种整体铸造航空发动机涡轮导向器及其制备方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2497041A (en) * 1945-03-27 1950-02-07 United Aircraft Corp Nozzle ring for gas turbines
US2811331A (en) * 1951-05-02 1957-10-29 Curtiss Wright Corp Clamp for parts operating at different temperatures
FR1326037A (fr) * 1962-06-07 1963-05-03 Napier Aero Engines Ltd Turbine
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
US3511577A (en) * 1968-04-10 1970-05-12 Caterpillar Tractor Co Turbine nozzle construction
US3689174A (en) * 1971-01-11 1972-09-05 Westinghouse Electric Corp Axial flow turbine structure
US3728041A (en) * 1971-10-04 1973-04-17 Gen Electric Fluidic seal for segmented nozzle diaphragm
US3752598A (en) * 1971-11-17 1973-08-14 United Aircraft Corp Segmented duct seal
US3841787A (en) * 1973-09-05 1974-10-15 Westinghouse Electric Corp Axial flow turbine structure
US4011718A (en) * 1975-08-01 1977-03-15 United Technologies Corporation Gas turbine construction
US4028787A (en) * 1975-09-15 1977-06-14 Cretella Salvatore Refurbished turbine vanes and method of refurbishment thereof
SU670734A1 (ru) * 1976-05-27 1979-06-30 Предприятие П/Я А-3492 Сопловой аппарат турбомашины
CA1125660A (en) * 1979-06-29 1982-06-15 David L. Brown Cooled vane structure for a combustion turbine engine
US4288201A (en) * 1979-09-14 1981-09-08 United Technologies Corporation Vane cooling structure

Also Published As

Publication number Publication date
JPH0151883B2 (sv) 1989-11-07
SE453314B (sv) 1988-01-25
US4511306A (en) 1985-04-16
GB2114234B (en) 1985-09-18
SE8300316L (sv) 1983-08-03
BE895761A (fr) 1983-08-01
GB8302880D0 (en) 1983-03-09
SE8300316D0 (sv) 1983-01-21
JPS58138206A (ja) 1983-08-17
CA1202570A (en) 1986-04-01
MX155781A (es) 1988-04-28
GB2114234A (en) 1983-08-17
IT1193648B (it) 1988-07-21
IT8319336A0 (it) 1983-01-28
BR8300273A (pt) 1983-10-25

Similar Documents

Publication Publication Date Title
AR231564A1 (es) Estructura de alabe de estator para una turbina fundida por el procedimiento de cera perdida,de una sola pieza
ES491604A0 (es) Un procedimiento para preparar, una composicion fotopolime- rizable.
IT8221755A0 (it) Paletta per una turbina a gas.
DE69006433T4 (de) Turbinenschaufel.
IT7924547A0 (it) Perfezionata paletta di turbomacchina.
ES519367A0 (es) Procedimiento para preparar derivados de ciclohexano-1,3-diona.
ES496349A0 (es) Un montaje de cabeza de rotor para una centufuga de laboratorio.
ES499970A0 (es) Una turbina de viento mejorada para la generacion de poten- cia
IT1215664B (it) Procedimento per fissare una paletta di turbina.
ES520957A0 (es) Procedimiento para preparar composiciones herbicidas.
ES490073A0 (es) Procedimiento para la obtencion de una composicion para sol-dar.
IT8024691A0 (it) Turbina particolarmente per turbocompressori.
BR7905704A (pt) Dispositivo de retencao de lamina para turbina eolica
IT8320366A0 (it) Struttura di paletta a profilo aerodinamico per turbina.
NO147776C (no) Kutteblad for gressklipper.
IT8223026A0 (it) Struttura perfezionata per una paletta raffreddata di rotore di turbina.
ES479803A0 (es) Un procedimiento para la preparacion de una aleacion metali-ca amorfa.
BR8100975A (pt) Rotor para maquina hidreletrica
IT8321305A0 (it) Dispositivo azionatore per una racla.
ES519709A0 (es) Procedimiento para preparar derivados de ciclohexeno-1,2-diona 5-aril-sustituidos.
NO845115L (no) Anordning for vridning av rotorblader.
ES538034A0 (es) Procedimiento para fabricar una aleacion a base de aluminio.
IT7920713A0 (it) Pala di rotore, specialmente per aeromobili ad ali rotanti.
ES496979A0 (es) Un procedimiento para la preparacion de una composicion derivada de al menos un aminofenol.
ES519366A0 (es) Procedimiento para preparar derivados de ciclohexano-1,3-diona-5-fenil-sustituidos.