FR1556914A - - Google Patents

Info

Publication number
FR1556914A
FR1556914A FR1556914DA FR1556914A FR 1556914 A FR1556914 A FR 1556914A FR 1556914D A FR1556914D A FR 1556914DA FR 1556914 A FR1556914 A FR 1556914A
Authority
FR
France
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
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 filed Critical
Application granted granted Critical
Publication of FR1556914A publication Critical patent/FR1556914A/fr
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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1556914D 1967-04-03 1968-03-25 Expired FR1556914A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB15224/67A GB1118898A (en) 1967-04-03 1967-04-03 Fluid flow machine

Publications (1)

Publication Number Publication Date
FR1556914A true FR1556914A (fr) 1969-02-07

Family

ID=10055250

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1556914D Expired FR1556914A (fr) 1967-04-03 1968-03-25

Country Status (4)

Country Link
US (1) US3494539A (fr)
DE (1) DE1751094A1 (fr)
FR (1) FR1556914A (fr)
GB (1) GB1118898A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636375A1 (fr) * 1988-08-15 1990-03-16 Gen Electric Anneau de renforcement pour etage a basse pression d'un compresseur
WO2015049548A1 (fr) * 2013-10-03 2015-04-09 Franco Tosi Meccanica S.P.A. Étage de rotor de turbine axiale avec rapport de corde/pas amélioré

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1428365A (en) * 1972-03-15 1976-03-17 Rolls Royce Fluid flow machines
GB1485032A (en) * 1974-08-23 1977-09-08 Rolls Royce Gas turbine engine casing
US4012165A (en) * 1975-12-08 1977-03-15 United Technologies Corporation Fan structure
GB1549422A (en) * 1976-10-19 1979-08-08 Rolls Royce Axial flow gas turbine engine compressor
GB2192238B (en) * 1986-07-02 1990-05-23 Rolls Royce Plc Gas turbine engine power turbine
GB2192237B (en) * 1986-07-02 1990-05-16 Rolls Royce Plc Gas turbine engine power turbine
US5224341A (en) * 1992-01-06 1993-07-06 United Technologies Corporation Separable fan strut for a gas turbofan powerplant
US5358382A (en) * 1993-07-21 1994-10-25 Eaton Corporation Fan and fan drive assembly
US5649419A (en) * 1995-01-27 1997-07-22 The Boeing Company Rotating acoustically lined inlet splitter for a turbo-fan engine
US7094033B2 (en) * 2004-01-21 2006-08-22 General Electric Company Methods and apparatus for assembling gas turbine engines
GB2455785B (en) * 2007-12-21 2009-11-11 Rolls Royce Plc Annular component
US8667775B1 (en) * 2009-08-05 2014-03-11 The Boeing Company Reverse flow engine core having a ducted fan with integrated secondary flow blades
US8813864B2 (en) 2011-09-09 2014-08-26 Jack D. Layton Support system for a box blade attached to a tractor
GB201705732D0 (en) * 2017-04-10 2017-05-24 Rolls Royce Plc Acoustic attenuation in gas turbine engines
US20200017229A1 (en) * 2018-07-13 2020-01-16 Bell Helicopter Textron Inc. Fan clutch for convertible engine
GB202216057D0 (en) * 2022-10-31 2022-12-14 Rolls Royce Plc Flow splitter

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3216654A (en) * 1965-11-09 Tureeofan engine
US3037742A (en) * 1959-09-17 1962-06-05 Gen Motors Corp Compressor turbine
US3070284A (en) * 1960-10-07 1962-12-25 Gen Electric Turbo-fan rotor
GB1003313A (en) * 1960-11-17 1965-09-02 Bristol Siddeley Engines Ltd Improvements in blades for ducted axial flow machines
GB981476A (en) * 1963-11-04 1965-01-27 Rolls Royce Gas turbine engine vane assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2636375A1 (fr) * 1988-08-15 1990-03-16 Gen Electric Anneau de renforcement pour etage a basse pression d'un compresseur
WO2015049548A1 (fr) * 2013-10-03 2015-04-09 Franco Tosi Meccanica S.P.A. Étage de rotor de turbine axiale avec rapport de corde/pas amélioré

Also Published As

Publication number Publication date
GB1118898A (en) 1968-07-03
US3494539A (en) 1970-02-10
DE1751094A1 (de) 1970-08-13

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
ST Notification of lapse