FR1420317A - Dispositif de fixation d'aubes pour turbine - Google Patents

Dispositif de fixation d'aubes pour turbine

Info

Publication number
FR1420317A
FR1420317A FR1715A FR1715A FR1420317A FR 1420317 A FR1420317 A FR 1420317A FR 1715 A FR1715 A FR 1715A FR 1715 A FR1715 A FR 1715A FR 1420317 A FR1420317 A FR 1420317A
Authority
FR
France
Prior art keywords
turbine blade
attachment device
blade attachment
turbine
blade
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
FR1715A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft 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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR1420317A publication Critical patent/FR1420317A/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
    • 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)
FR1715A 1964-01-13 1965-01-13 Dispositif de fixation d'aubes pour turbine Expired FR1420317A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US337407A US3269702A (en) 1964-01-13 1964-01-13 Nozzle vane assembly

Publications (1)

Publication Number Publication Date
FR1420317A true FR1420317A (fr) 1965-12-03

Family

ID=23320435

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1715A Expired FR1420317A (fr) 1964-01-13 1965-01-13 Dispositif de fixation d'aubes pour turbine

Country Status (8)

Country Link
US (1) US3269702A (fr)
BE (1) BE658208A (fr)
CH (1) CH445524A (fr)
DE (1) DE1426870B2 (fr)
FR (1) FR1420317A (fr)
GB (1) GB1055069A (fr)
NL (1) NL125370C (fr)
SE (1) SE305569B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5222360A (en) * 1991-10-30 1993-06-29 General Electric Company Apparatus for removably attaching a core frame to a vane frame with a stable mid ring
FR2685383B1 (fr) * 1991-12-18 1994-02-11 Snecma Bras structural du carter d'une turbomachine.
US5765993A (en) * 1996-09-27 1998-06-16 Chromalloy Gas Turbine Corporation Replacement vane assembly for fan exit guide
US10047763B2 (en) * 2015-12-14 2018-08-14 General Electric Company Rotor assembly for use in a turbofan engine and method of assembling
US10563542B2 (en) * 2016-05-23 2020-02-18 United Technologies Corporation Retention hardware

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA626485A (en) * 1961-08-29 General Motors Corporation Sheet metal compressor casing
FR998220A (fr) * 1949-10-26 1952-01-16 Soc D Const Et D Equipements M Perfectionnement dans le montage et dans la fixation des aubes fixes pour turbomachines
BE533039A (fr) * 1953-11-06
DE1067971B (fr) * 1955-10-18 1959-10-29
US3026087A (en) * 1957-08-13 1962-03-20 Gen Motors Corp Stator ring assembly
GB856599A (en) * 1958-06-16 1960-12-21 Gen Motors Corp Improvements relating to axial-flow compressors
US3042367A (en) * 1958-07-17 1962-07-03 Gen Motors Corp Fluid seal

Also Published As

Publication number Publication date
GB1055069A (en) 1967-01-11
SE305569B (fr) 1968-10-28
CH445524A (de) 1967-10-31
NL6415199A (fr) 1965-07-14
BE658208A (fr) 1965-04-30
DE1426870A1 (de) 1968-11-21
NL125370C (fr) 1968-11-15
US3269702A (en) 1966-08-30
DE1426870B2 (de) 1971-12-30

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