CH294451A - Couronne d'aubes directrices pour turbine à écoulement axial. - Google Patents

Couronne d'aubes directrices pour turbine à écoulement axial.

Info

Publication number
CH294451A
CH294451A CH294451DA CH294451A CH 294451 A CH294451 A CH 294451A CH 294451D A CH294451D A CH 294451DA CH 294451 A CH294451 A CH 294451A
Authority
CH
Switzerland
Prior art keywords
ring
axial flow
guide vanes
flow turbine
turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Limited Canadian P Development
Original Assignee
Canadian Patents Dev
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 Canadian Patents Dev filed Critical Canadian Patents Dev
Publication of CH294451A publication Critical patent/CH294451A/fr

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH294451D 1950-01-21 1951-01-20 Couronne d'aubes directrices pour turbine à écoulement axial. CH294451A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US139867A US2609176A (en) 1950-01-21 1950-01-21 Turbine nozzle guide vane construction

Publications (1)

Publication Number Publication Date
CH294451A true CH294451A (fr) 1953-11-15

Family

ID=22488653

Family Applications (1)

Application Number Title Priority Date Filing Date
CH294451D CH294451A (fr) 1950-01-21 1951-01-20 Couronne d'aubes directrices pour turbine à écoulement axial.

Country Status (5)

Country Link
US (1) US2609176A (fr)
CH (1) CH294451A (fr)
DE (1) DE843700C (fr)
FR (1) FR1031214A (fr)
GB (1) GB689216A (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2702688A (en) * 1951-12-26 1955-02-22 Gen Electric Gas turbine nozzle casing
US2808226A (en) * 1952-02-08 1957-10-01 Ryan Aeronautical Co Turbine nozzle box
US2771622A (en) * 1952-05-09 1956-11-27 Westinghouse Electric Corp Diaphragm apparatus
US2915280A (en) * 1957-04-18 1959-12-01 Gen Electric Nozzle and seal assembly
BE570267A (fr) * 1957-08-16
DE1246321B (de) * 1964-10-02 1967-08-03 Daimler Benz Ag Leitschaufelkranz fuer axial durchstroemte Turbinen oder Verdichter von Gasturbinentriebwerken
US3300180A (en) * 1964-11-17 1967-01-24 Worthington Corp Segmented diaphragm assembly
GB1086432A (en) * 1965-09-21 1967-10-11 Bristol Siddeley Engines Ltd Gas turbine engines
FR1339521A (fr) * 1966-06-10 1963-10-11 Rolls Royce Machine à circulation de fluide
DE2250484A1 (de) * 1972-10-14 1974-04-18 Bulawin Stator der mehrstufen-stroemungsmaschine
DE3003469C2 (de) * 1980-01-31 1987-03-19 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verbindung einander rotationssymmetrisch zugeordneter, unterschiedlichen thermischen Einflüssen ausgesetzter Bauteile für Strömungsmaschinen, insbesondere Gasturbinentriebwerke
US4470754A (en) * 1980-05-19 1984-09-11 Avco Corporation Partially segmented supporting and sealing structure for a guide vane array of a gas turbine engine
US4452564A (en) * 1981-11-09 1984-06-05 The Garrett Corporation Stator vane assembly and associated methods
US4725199A (en) * 1985-12-23 1988-02-16 United Technologies Corporation Snap ring construction
US4815933A (en) * 1987-11-13 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Nozzle flange attachment and sealing arrangement
US4883405A (en) * 1987-11-13 1989-11-28 The United States Of America As Represented By The Secretary Of The Air Force Turbine nozzle mounting arrangement
US5131813A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade outer end attachment structure
US5176496A (en) * 1991-09-27 1993-01-05 General Electric Company Mounting arrangements for turbine nozzles
GB2268978B (en) * 1992-07-21 1995-11-08 Rolls Royce Plc Fan for a ducted fan gas turbine engine
US6641144B2 (en) * 2001-12-28 2003-11-04 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
DE10223655B3 (de) * 2002-05-28 2004-02-12 Mtu Aero Engines Gmbh Anordnung zum axialen und radialen Fixieren der Leitschaufeln eines Leitschaufelkranzes einer Gasturbine
US8984859B2 (en) 2010-12-28 2015-03-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and reheat system
US10072516B2 (en) 2014-09-24 2018-09-11 United Technologies Corporation Clamped vane arc segment having load-transmitting features
US20160177835A1 (en) * 2014-12-22 2016-06-23 Pratt & Whitney Canada Corp. Gas turbine engine with angularly offset turbine vanes

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US973472A (en) * 1908-03-28 1910-10-25 Gen Electric Turbine-nozzle.
US1061675A (en) * 1911-12-18 1913-05-13 Gen Electric Diaphragm and nozzle construction for turbines.
US2013512A (en) * 1933-03-11 1935-09-03 Laval Steam Turbine Co Guide vane and diaphragm construction for turbines
US2427244A (en) * 1944-03-07 1947-09-09 Gen Electric Gas turbine
BE487120A (fr) * 1946-03-25
FR957575A (fr) * 1946-10-02 1950-02-23
FR965713A (fr) * 1947-05-07 1950-09-20

Also Published As

Publication number Publication date
US2609176A (en) 1952-09-02
FR1031214A (fr) 1953-06-22
DE843700C (de) 1952-07-10
GB689216A (en) 1953-03-25

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