GB1055069A - Turbine nozzle vane assembly - Google Patents

Turbine nozzle vane assembly

Info

Publication number
GB1055069A
GB1055069A GB52505/64A GB5250564A GB1055069A GB 1055069 A GB1055069 A GB 1055069A GB 52505/64 A GB52505/64 A GB 52505/64A GB 5250564 A GB5250564 A GB 5250564A GB 1055069 A GB1055069 A GB 1055069A
Authority
GB
United Kingdom
Prior art keywords
vane
rings
turbine
ring
shroud
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
GB52505/64A
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.)
RTX 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
Publication of GB1055069A publication Critical patent/GB1055069A/en
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)
GB52505/64A 1964-01-13 1964-12-24 Turbine nozzle vane assembly Expired GB1055069A (en)

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
GB1055069A true GB1055069A (en) 1967-01-11

Family

ID=23320435

Family Applications (1)

Application Number Title Priority Date Filing Date
GB52505/64A Expired GB1055069A (en) 1964-01-13 1964-12-24 Turbine nozzle vane assembly

Country Status (8)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2262574A (en) * 1991-12-18 1993-06-23 Snecma A structural arm for the casing of a turbomachine.

Families Citing this family (4)

* 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
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 (OSRAM) * 1953-11-06
DE1067971B (OSRAM) * 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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2262574A (en) * 1991-12-18 1993-06-23 Snecma A structural arm for the casing of a turbomachine.
GB2262574B (en) * 1991-12-18 1994-10-05 Snecma A structural arm for the casing of a turbomachine

Also Published As

Publication number Publication date
SE305569B (OSRAM) 1968-10-28
CH445524A (de) 1967-10-31
FR1420317A (fr) 1965-12-03
DE1426870A1 (de) 1968-11-21
US3269702A (en) 1966-08-30
NL6415199A (OSRAM) 1965-07-14
NL125370C (OSRAM) 1968-11-15
BE658208A (OSRAM) 1965-04-30
DE1426870B2 (de) 1971-12-30

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