SE305569B - - Google Patents

Info

Publication number
SE305569B
SE305569B SE339/65A SE33965A SE305569B SE 305569 B SE305569 B SE 305569B SE 339/65 A SE339/65 A SE 339/65A SE 33965 A SE33965 A SE 33965A SE 305569 B SE305569 B SE 305569B
Authority
SE
Sweden
Application number
SE339/65A
Inventor
A Nichols
E Westler
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 SE305569B publication Critical patent/SE305569B/xx

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)
SE339/65A 1964-01-13 1965-01-12 SE305569B (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
SE305569B true SE305569B (en) 1968-10-28

Family

ID=23320435

Family Applications (1)

Application Number Title Priority Date Filing Date
SE339/65A SE305569B (en) 1964-01-13 1965-01-12

Country Status (8)

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

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 (en) * 1991-12-18 1994-02-11 Snecma STRUCTURAL ARM OF THE HOUSING OF A 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 (en) * 1949-10-26 1952-01-16 Soc D Const Et D Equipements M Advanced training in the assembly and fixing of fixed blades for turbomachines
BE533039A (en) * 1953-11-06
DE1067971B (en) * 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
DE1426870B2 (en) 1971-12-30
US3269702A (en) 1966-08-30
BE658208A (en) 1965-04-30
NL6415199A (en) 1965-07-14
FR1420317A (en) 1965-12-03
NL125370C (en) 1968-11-15
DE1426870A1 (en) 1968-11-21
GB1055069A (en) 1967-01-11
CH445524A (en) 1967-10-31

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