FR1045841A - Turbine à gaz à aubes directrices creuses - Google Patents

Turbine à gaz à aubes directrices creuses

Info

Publication number
FR1045841A
FR1045841A FR1045841DA FR1045841A FR 1045841 A FR1045841 A FR 1045841A FR 1045841D A FR1045841D A FR 1045841DA FR 1045841 A FR1045841 A FR 1045841A
Authority
FR
France
Prior art keywords
gas turbine
guide vane
hollow guide
vane gas
hollow
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1045841A publication Critical patent/FR1045841A/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1045841D 1950-06-29 1951-06-26 Turbine à gaz à aubes directrices creuses Expired FR1045841A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB294130X 1950-06-29
GB230451X 1951-04-23
GB220651X 1951-06-22

Publications (1)

Publication Number Publication Date
FR1045841A true FR1045841A (fr) 1953-12-01

Family

ID=27258081

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1045841D Expired FR1045841A (fr) 1950-06-29 1951-06-26 Turbine à gaz à aubes directrices creuses

Country Status (4)

Country Link
US (1) US2738949A (fr)
CH (1) CH294130A (fr)
FR (1) FR1045841A (fr)
GB (1) GB701101A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528494A1 (fr) * 1982-06-10 1983-12-16 Rolls Royce Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2974928A (en) * 1961-03-14 ridley
US2919104A (en) * 1953-12-02 1959-12-29 Napier & Son Ltd Interstage seals and cooling means in axial flow turbines
US2932485A (en) * 1954-10-01 1960-04-12 United Aircraft Corp Stator construction
GB803137A (en) * 1955-08-05 1958-10-22 Rolls Royce Improvements in or relating to axial-flow fluid machines for example turbines and compressors of gas-turbine engines
US2996279A (en) * 1956-07-16 1961-08-15 English Electric Co Ltd Gas turbines
DE1043718B (de) * 1956-07-31 1958-11-13 Maschf Augsburg Nuernberg Ag Axial beaufschlagter Turbinenlaeufer mit Kuehlung durch ein gasfoermiges Kuehlmittel, insbesondere fuer Gasturbinen
DE1106557B (de) * 1957-07-18 1961-05-10 Rolls Royce Gasturbine, deren Laeuferschaufeln innere Kuehlkanaele aufweisen
DE1080352B (de) * 1957-10-21 1960-04-21 Bmw Triebwerkbau Ges M B H Kuehleinrichtung fuer Gasturbinen, insbesondere fuer mit Schweroel betriebene Gasturbinen
US3075744A (en) * 1960-08-16 1963-01-29 United Aircraft Corp Turbine nozzle vane mounting means
DE1163604B (de) * 1962-04-21 1964-02-20 Gasturbinenbau Und Energiemasc Kuehleinrichtung fuer Gasturbinenlaeufer
US3941500A (en) * 1974-06-10 1976-03-02 Westinghouse Electric Corporation Turbomachine interstage seal assembly
US3990812A (en) * 1975-03-03 1976-11-09 United Technologies Corporation Radial inflow blade cooling system
SE411931B (sv) * 1975-03-25 1980-02-11 United Technologies Corp Anordning vid turbinmunstycken for gasturbinmotor
DE3003469A1 (de) * 1980-01-31 1981-08-06 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verbindung einander rotationssymmetrisch zugeordneter bauteile fuer stroemungsmaschinen, insbesondere gasturbinentriebwerke
JPS59134302A (ja) * 1983-01-24 1984-08-02 Toshiba Corp 蒸気タ−ビンの腐蝕防止装置
US4890978A (en) * 1988-10-19 1990-01-02 Westinghouse Electric Corp. Method and apparatus for vane segment support and alignment in combustion turbines
GB2234299B (en) * 1989-07-06 1994-01-05 Rolls Royce Plc Mounting system for engine components having dissimilar coefficients of thermal expansion
US5429478A (en) * 1994-03-31 1995-07-04 United Technologies Corporation Airfoil having a seal and an integral heat shield
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
US6884023B2 (en) * 2002-09-27 2005-04-26 United Technologies Corporation Integral swirl knife edge injection assembly
US7588418B2 (en) * 2006-09-19 2009-09-15 General Electric Company Methods and apparatus for assembling turbine engines
EP2949872A1 (fr) * 2014-05-27 2015-12-02 Siemens Aktiengesellschaft Turbomachine avec un joint de séparation de fluide de travail, fluide de refroidissement de la turbomachine et utilisation de la turbomachine
US10202857B2 (en) * 2015-02-06 2019-02-12 United Technologies Corporation Vane stages
CN111140289B (zh) 2019-12-20 2020-12-29 南京航空航天大学 一种降低燃气入侵量的篦齿封严装置

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE383506C (de) * 1923-10-13 Conrad Baerwolff Dipl Ing Lauf- und Leitzeugkuehlung fuer Verbrennungsturbinen
GB359350A (en) * 1930-03-03 1931-10-22 Ltd Co Formerly Skoda Works Connection of rotarys for combustion turbines
US2319846A (en) * 1941-02-01 1943-05-25 Carling Turbine Blower Co Turbine rotor
FR957575A (fr) * 1946-10-02 1950-02-23
GB617472A (en) * 1946-10-02 1949-02-07 Adrian Albert Lombard Improvements in or relating to gas-turbine-engines
FR965713A (fr) * 1947-05-07 1950-09-20
US2606741A (en) * 1947-06-11 1952-08-12 Gen Electric Gas turbine nozzle and bucket shroud structure
GB666537A (en) * 1949-08-27 1952-02-13 Armstrong Siddeley Motors Ltd Mounting of the stator blades of a gaseous fluid turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2528494A1 (fr) * 1982-06-10 1983-12-16 Rolls Royce Element de distribution de charge pour une turbine d'un moteur a turbine a gaz et ensemble comportant deux tels elements

Also Published As

Publication number Publication date
CH294130A (de) 1953-10-31
GB701101A (en) 1953-12-16
US2738949A (en) 1956-03-20

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