FR1095927A - Improvements to the mounting of wing profile vanes in compressors and other applications - Google Patents

Improvements to the mounting of wing profile vanes in compressors and other applications

Info

Publication number
FR1095927A
FR1095927A FR1095927DA FR1095927A FR 1095927 A FR1095927 A FR 1095927A FR 1095927D A FR1095927D A FR 1095927DA FR 1095927 A FR1095927 A FR 1095927A
Authority
FR
France
Prior art keywords
compressors
applications
mounting
wing profile
profile vanes
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of FR1095927A publication Critical patent/FR1095927A/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
    • F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1095927D 1953-02-02 1954-02-02 Improvements to the mounting of wing profile vanes in compressors and other applications Expired FR1095927A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1095927X 1953-02-02

Publications (1)

Publication Number Publication Date
FR1095927A true FR1095927A (en) 1955-06-07

Family

ID=10873696

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1095927D Expired FR1095927A (en) 1953-02-02 1954-02-02 Improvements to the mounting of wing profile vanes in compressors and other applications

Country Status (1)

Country Link
FR (1) FR1095927A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095453B (en) * 1955-07-18 1960-12-22 Rolls Royce Multi-stage axial flow machine
EP1081336A3 (en) * 1999-08-30 2003-10-01 MTU Aero Engines GmbH Vane ring assembly for gas turbines
EP1548233A1 (en) * 2003-12-18 2005-06-29 Techspace Aero S.A. Fastening device for stator blades and compressor stator stage comprising such a fastening device
EP1746252A3 (en) * 2005-07-20 2010-03-17 United Technologies Corporation Structural strut and shroud element

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1095453B (en) * 1955-07-18 1960-12-22 Rolls Royce Multi-stage axial flow machine
EP1081336A3 (en) * 1999-08-30 2003-10-01 MTU Aero Engines GmbH Vane ring assembly for gas turbines
EP1548233A1 (en) * 2003-12-18 2005-06-29 Techspace Aero S.A. Fastening device for stator blades and compressor stator stage comprising such a fastening device
EP1746252A3 (en) * 2005-07-20 2010-03-17 United Technologies Corporation Structural strut and shroud element

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