CH268031A - Leitschaufelanordnung in Gasturbinen. - Google Patents

Leitschaufelanordnung in Gasturbinen.

Info

Publication number
CH268031A
CH268031A CH268031DA CH268031A CH 268031 A CH268031 A CH 268031A CH 268031D A CH268031D A CH 268031DA CH 268031 A CH268031 A CH 268031A
Authority
CH
Switzerland
Prior art keywords
guide vane
gas turbines
vane arrangement
arrangement
turbines
Prior art date
Application number
Other languages
English (en)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of CH268031A publication Critical patent/CH268031A/de

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
CH268031D 1947-05-07 1948-05-07 Leitschaufelanordnung in Gasturbinen. CH268031A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB268031X 1947-05-07

Publications (1)

Publication Number Publication Date
CH268031A true CH268031A (de) 1950-04-30

Family

ID=10249461

Family Applications (1)

Application Number Title Priority Date Filing Date
CH268031D CH268031A (de) 1947-05-07 1948-05-07 Leitschaufelanordnung in Gasturbinen.

Country Status (4)

Country Link
US (1) US2488875A (de)
CH (1) CH268031A (de)
FR (1) FR965713A (de)
GB (1) GB623508A (de)

Families Citing this family (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2606741A (en) * 1947-06-11 1952-08-12 Gen Electric Gas turbine nozzle and bucket shroud structure
US2618461A (en) * 1948-10-05 1952-11-18 English Electric Co Ltd Gas turbine
BE496713A (de) * 1949-07-01
US2789787A (en) * 1949-10-22 1957-04-23 Svenska Turbinfab Ab Guide blade device for steam or gas turbines
US2763462A (en) * 1950-01-11 1956-09-18 Gen Motors Corp Turbine casing construction
US2609176A (en) * 1950-01-21 1952-09-02 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2747367A (en) * 1950-03-21 1956-05-29 United Aircraft Corp Gas turbine power plant supporting structure
US2741455A (en) * 1950-06-29 1956-04-10 Rolls Royce Gas-turbine engines and nozzle-guidevane assemblies therefor
GB701101A (en) * 1950-06-29 1953-12-16 Rolls Royce Improvements in or relating to gas-turbine engines
US2634090A (en) * 1950-07-28 1953-04-07 Westinghouse Electric Corp Turbine apparatus
US2849209A (en) * 1950-10-11 1958-08-26 Gen Electric Nozzle construction for turbines
US2702687A (en) * 1950-11-13 1955-02-22 United Aircraft Corp Rotor construction
US2681788A (en) * 1951-05-23 1954-06-22 Solar Aircraft Co Gas turbine vane structure
US2724544A (en) * 1951-05-25 1955-11-22 Westinghouse Electric Corp Stator shroud and blade assembly
US2710523A (en) * 1951-09-27 1955-06-14 A V Roe Canada Ltd Gas turbine tail cone
US2932485A (en) * 1954-10-01 1960-04-12 United Aircraft Corp Stator construction
BE543281A (de) * 1954-12-16
US2799473A (en) * 1955-04-27 1957-07-16 Gen Electric Gas turbine nozzle ring
US2934316A (en) * 1955-11-18 1960-04-26 Worthington Corp Turbine casing
GB804922A (en) * 1956-01-13 1958-11-26 Rolls Royce Improvements in or relating to axial-flow fluid machines for example compressors andturbines
GB804010A (en) * 1956-02-13 1958-11-05 Rolls Royce Improvements in or relating to stator vane assemblies such as are used in axial-flowfluid machines
US3018085A (en) * 1957-03-25 1962-01-23 Gen Motors Corp Floating labyrinth seal
US2919891A (en) * 1957-06-17 1960-01-05 Gen Electric Gas turbine diaphragm assembly
NL104794C (de) * 1957-08-16
NL99435C (de) * 1957-08-22
US3067983A (en) * 1958-07-01 1962-12-11 Gen Motors Corp Turbine mounting construction
GB904138A (en) * 1959-01-23 1962-08-22 Bristol Siddeley Engines Ltd Improvements in or relating to stator structures, for example for axial flow gas turbine engines
US3072380A (en) * 1959-02-05 1963-01-08 Dresser Ind Stator blade carrier assembly mounting
US3066911A (en) * 1959-05-12 1962-12-04 Thompson Ramo Wooldridge Inc Nozzle and turbine wheel shroud support
US3067981A (en) * 1959-06-15 1962-12-11 Ford Motor Co Gas turbine engine
US3075744A (en) * 1960-08-16 1963-01-29 United Aircraft Corp Turbine nozzle vane mounting means
US3074690A (en) * 1960-09-15 1963-01-22 Chrysler Corp Fixed nozzle support for gas turbine engine
DE1172900B (de) * 1962-04-17 1964-06-25 Gasturbinenbau Veb Verfahren zum Zusammenbau einer mehrstufigen Axialstroemungsmaschine
GB1051244A (de) * 1962-10-09
US3169366A (en) * 1963-03-25 1965-02-16 Gen Electric Multiple gas generator turbine
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
GB1086432A (en) * 1965-09-21 1967-10-11 Bristol Siddeley Engines Ltd Gas turbine engines
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
CH482915A (de) * 1967-11-03 1969-12-15 Sulzer Ag Leitvorrichtung für Axialturbine
US3990807A (en) * 1974-12-23 1976-11-09 United Technologies Corporation Thermal response shroud for rotating body
US4248569A (en) * 1978-11-13 1981-02-03 General Motors Corporation Stator mounting
US4245954A (en) * 1978-12-01 1981-01-20 Westinghouse Electric Corp. Ceramic turbine stator vane and shroud support
US4728257A (en) * 1986-06-18 1988-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal stress minimized, two component, turbine shroud seal
GB2234299B (en) * 1989-07-06 1994-01-05 Rolls Royce Plc Mounting system for engine components having dissimilar coefficients of thermal expansion
US5704762A (en) * 1993-11-08 1998-01-06 Alliedsignal Inc. Ceramic-to-metal stator vane assembly
DE50214427D1 (de) * 2002-01-17 2010-06-24 Siemens Ag Gegossene Turbinenleitschaufel mit Hakensockel
CN100412322C (zh) * 2002-12-19 2008-08-20 西门子公司 透平机和用于将透平机的导向叶片拆下的工作方法
ATE556197T1 (de) * 2006-12-22 2012-05-15 Techspace Aero Winkelfixierung für leitschaufeln von turbomachinen
EP2738356B1 (de) * 2012-11-29 2019-05-01 Safran Aero Boosters SA Statorschaufel einer Strömungsmaschine, Statorschaufelkranz einer Strömungsmaschine und zugehöriges Montageverfahren
EP3102793B1 (de) * 2014-01-24 2019-07-10 United Technologies Corporation Kippdichtung für eine kranzdichtung einer rotoranordnung
US20180216575A1 (en) * 2017-01-27 2018-08-02 General Electric Company Cool core gas turbine engine
US20200072070A1 (en) * 2018-09-05 2020-03-05 United Technologies Corporation Unified boas support and vane platform

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like

Also Published As

Publication number Publication date
FR965713A (de) 1950-09-20
US2488875A (en) 1949-11-22
GB623508A (en) 1949-05-18

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