FR944756A - Improvements to the guide vanes of compressors and axial type turbines - Google Patents

Improvements to the guide vanes of compressors and axial type turbines

Info

Publication number
FR944756A
FR944756A FR944756DA FR944756A FR 944756 A FR944756 A FR 944756A FR 944756D A FR944756D A FR 944756DA FR 944756 A FR944756 A FR 944756A
Authority
FR
France
Prior art keywords
compressors
guide vanes
axial type
type turbines
turbines
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
French (fr)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR944756A publication Critical patent/FR944756A/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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR944756D 1946-04-05 1947-04-05 Improvements to the guide vanes of compressors and axial type turbines Expired FR944756A (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
FR944756A true FR944756A (en) 1949-04-14

Family

ID=26237928

Family Applications (1)

Application Number Title Priority Date Filing Date
FR944756D Expired FR944756A (en) 1946-04-05 1947-04-05 Improvements to the guide vanes of compressors and axial type turbines

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
DE1278178B (en) * 1966-06-10 1968-09-19 Rolls Royce Inlet guide vane ring for axial compressors of gas turbine engines

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
NL104794C (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
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
GB2192233B (en) * 1986-07-02 1990-11-28 Rolls Royce Plc A gas turbine engine load transfer structure
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
DE1278178B (en) * 1966-06-10 1968-09-19 Rolls Royce Inlet guide vane ring for axial compressors of gas turbine engines

Also Published As

Publication number Publication date
BE487115A (en)
US2605997A (en) 1952-08-05
GB611326A (en) 1948-10-28
CH257532A (en) 1948-10-15

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