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FR1146656A - Couronne de capot en plusieurs parties, notamment pour turbo-moteurs - Google Patents

Couronne de capot en plusieurs parties, notamment pour turbo-moteurs

Info

Publication number
FR1146656A
FR1146656A FR1146656DA FR1146656A FR 1146656 A FR1146656 A FR 1146656A FR 1146656D A FR1146656D A FR 1146656DA FR 1146656 A FR1146656 A FR 1146656A
Authority
FR
France
Prior art keywords
turbo
engines
several parts
crown
hood
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.)
Canadian Patents and Development Ltd
Original Assignee
Canadian Patents and Development Ltd
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 and Development Ltd filed Critical Canadian Patents and Development Ltd
Application granted granted Critical
Publication of FR1146656A publication Critical patent/FR1146656A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; 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)
FR1146656D 1955-02-28 1956-01-12 Couronne de capot en plusieurs parties, notamment pour turbo-moteurs Expired FR1146656A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEC10835A DE1017420B (de) 1955-02-28 1955-02-28 Gasturbinentriebwerk mit einer mehrstufigen Turbine

Publications (1)

Publication Number Publication Date
FR1146656A true FR1146656A (fr) 1957-11-14

Family

ID=7014845

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1146656D Expired FR1146656A (fr) 1955-02-28 1956-01-12 Couronne de capot en plusieurs parties, notamment pour turbo-moteurs

Country Status (3)

Country Link
DE (1) DE1017420B (fr)
FR (1) FR1146656A (fr)
GB (1) GB790280A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2317480A1 (fr) * 1975-06-25 1977-02-04 United Technologies Corp Turbomachine a ecoulement axial avec une aube de stator amovible

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US6354797B1 (en) * 2000-07-27 2002-03-12 General Electric Company Brazeless fillet turbine nozzle
DE602005024425D1 (de) 2005-12-22 2010-12-09 Techspace Aero Milmort Schaufelleitring einer Strömungsmaschine, Strömungsmaschine mit einem solchen Leitring und Leitschaufel
US8231338B2 (en) 2009-05-05 2012-07-31 General Electric Company Turbine shell with pin support
FR2960590B1 (fr) * 2010-05-25 2014-04-11 Snecma Distributeur de turbine pour une turbomachine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE858478C (de) * 1939-12-12 1952-12-08 Versuchsanstalt Fuer Luftfahrt Halterung fuer Duesensegmente von axial beaufschlagten Dampf- oder Gasturbinen, insbesondere Abgasturbinen
DE907179C (de) * 1943-08-24 1954-03-22 Svenska Rotor Maskiner Ab Turbine mit einem oder mehreren Ringkoerpern
BE492385A (fr) * 1948-11-27
GB695724A (en) * 1950-08-01 1953-08-19 Rolls Royce Improvements in or relating to structural elements for axial-flow turbo-machines such as compressors or turbines of gas-turbine engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2317480A1 (fr) * 1975-06-25 1977-02-04 United Technologies Corp Turbomachine a ecoulement axial avec une aube de stator amovible

Also Published As

Publication number Publication date
DE1017420B (de) 1957-10-10
GB790280A (en) 1958-02-05

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