CH257532A - Guide vane assembly. - Google Patents

Guide vane assembly.

Info

Publication number
CH257532A
CH257532A CH257532DA CH257532A CH 257532 A CH257532 A CH 257532A CH 257532D A CH257532D A CH 257532DA CH 257532 A CH257532 A CH 257532A
Authority
CH
Switzerland
Prior art keywords
guide vane
vane assembly
assembly
guide
vane
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH257532A publication Critical patent/CH257532A/en

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH257532D 1946-04-05 1947-01-31 Guide vane assembly. CH257532A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB257532X 1946-04-05
GB30147X 1947-01-03

Publications (1)

Publication Number Publication Date
CH257532A true CH257532A (en) 1948-10-15

Family

ID=26237928

Family Applications (1)

Application Number Title Priority Date Filing Date
CH257532D CH257532A (en) 1946-04-05 1947-01-31 Guide vane assembly.

Country Status (5)

Country Link
US (1) US2605997A (en)
BE (1) BE487115A (en)
CH (1) CH257532A (en)
FR (1) FR944756A (en)
GB (1) GB611326A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4756153A (en) * 1986-07-02 1988-07-12 Rolls-Royce Plc Load transfer structure

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2932485A (en) * 1954-10-01 1960-04-12 United Aircraft Corp Stator construction
DE1067971B (en) * 1955-10-18 1959-10-29
US2915280A (en) * 1957-04-18 1959-12-01 Gen Electric Nozzle and seal assembly
BE570267A (en) * 1957-08-16
US3072380A (en) * 1959-02-05 1963-01-08 Dresser Ind Stator blade carrier assembly mounting
US3075744A (en) * 1960-08-16 1963-01-29 United Aircraft Corp Turbine nozzle vane mounting means
FR1339521A (en) * 1966-06-10 1963-10-11 Rolls Royce Fluid circulation machine
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
US4861229A (en) * 1987-11-16 1989-08-29 Williams International Corporation Ceramic-matrix composite nozzle assembly for a turbine engine
US5494402A (en) * 1994-05-16 1996-02-27 Solar Turbines Incorporated Low thermal stress ceramic turbine nozzle
US6517313B2 (en) * 2001-06-25 2003-02-11 Pratt & Whitney Canada Corp. Segmented turbine vane support structure
US8096746B2 (en) * 2007-12-13 2012-01-17 Pratt & Whitney Canada Corp. Radial loading element for turbine vane
FR2935430B1 (en) * 2008-08-26 2012-03-09 Snecma IMPROVED TURBOMACHINE HIGH-PRESSURE TURBINE, DISPENSER SECTOR AND AIRCRAFT ENGINE
US9702252B2 (en) * 2012-12-19 2017-07-11 Honeywell International Inc. Turbine nozzles with slip joints and methods for the production thereof
US20140255174A1 (en) * 2012-12-21 2014-09-11 United Technologies Corporation Manufacture of full ring strut vane pack
US9816387B2 (en) 2014-09-09 2017-11-14 United Technologies Corporation Attachment faces for clamped turbine stator of a gas turbine engine
EP3763917A1 (en) * 2019-07-08 2021-01-13 MTU Aero Engines GmbH Guide blade segment with support section rib

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB191016889A (en) * 1910-07-15 1910-10-20 James Howden Improvements in Means for Fixing Blades in Turbines.
US2402418A (en) * 1943-01-20 1946-06-18 Westinghouse Electric Corp Turbine apparatus
US2427244A (en) * 1944-03-07 1947-09-09 Gen Electric Gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4756153A (en) * 1986-07-02 1988-07-12 Rolls-Royce Plc Load transfer structure

Also Published As

Publication number Publication date
US2605997A (en) 1952-08-05
BE487115A (en)
FR944756A (en) 1949-04-14
GB611326A (en) 1948-10-28

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