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FR1325261A - Fluid flow machine - Google Patents

Fluid flow machine

Info

Publication number
FR1325261A
FR1325261A FR898386A FR898386A FR1325261A FR 1325261 A FR1325261 A FR 1325261A FR 898386 A FR898386 A FR 898386A FR 898386 A FR898386 A FR 898386A FR 1325261 A FR1325261 A FR 1325261A
Authority
FR
France
Prior art keywords
fluid flow
flow machine
machine
fluid
flow
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
FR898386A
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
Priority claimed from GB1865461A external-priority patent/GB946995A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR898386A priority Critical patent/FR1325261A/en
Application granted granted Critical
Publication of FR1325261A publication Critical patent/FR1325261A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR898386A 1961-05-23 1962-05-22 Fluid flow machine Expired FR1325261A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR898386A FR1325261A (en) 1961-05-23 1962-05-22 Fluid flow machine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1865461A GB946995A (en) 1961-05-23 1961-05-23 Fluid flow machine such as a gas turbine engine
FR898386A FR1325261A (en) 1961-05-23 1962-05-22 Fluid flow machine

Publications (1)

Publication Number Publication Date
FR1325261A true FR1325261A (en) 1963-04-26

Family

ID=26195815

Family Applications (1)

Application Number Title Priority Date Filing Date
FR898386A Expired FR1325261A (en) 1961-05-23 1962-05-22 Fluid flow machine

Country Status (1)

Country Link
FR (1) FR1325261A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3367628A (en) * 1966-10-31 1968-02-06 United Aircraft Corp Movable vane unit
US3471126A (en) * 1966-10-31 1969-10-07 United Aircraft Corp Movable vane unit
FR2583817A1 (en) * 1985-06-20 1986-12-26 Snecma TURNBUCKLE CONTROL ROD WITH VARIABLE STATION OF TURBOMACHINE COMPRESSOR STATOR
EP1961922A2 (en) 2007-02-22 2008-08-27 Snecma Control of variable pitch angle blades
FR2982653A1 (en) * 2011-11-14 2013-05-17 Snecma CANNELE SHAFT TRANSMISSION SYSTEM.
WO2017189566A3 (en) * 2016-04-25 2017-12-28 Florida Turbine Technologies, Inc. Twin spool industrial gas turbine engine with variable inlet guide vanes

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3367628A (en) * 1966-10-31 1968-02-06 United Aircraft Corp Movable vane unit
US3471126A (en) * 1966-10-31 1969-10-07 United Aircraft Corp Movable vane unit
FR2583817A1 (en) * 1985-06-20 1986-12-26 Snecma TURNBUCKLE CONTROL ROD WITH VARIABLE STATION OF TURBOMACHINE COMPRESSOR STATOR
EP0209428A1 (en) * 1985-06-20 1987-01-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Actuation lever for a stator vane with variable incidence
US4732536A (en) * 1985-06-20 1988-03-22 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Turbo-machine compressor with variable incidence stator vanes
EP1961922A2 (en) 2007-02-22 2008-08-27 Snecma Control of variable pitch angle blades
FR2913052A1 (en) * 2007-02-22 2008-08-29 Snecma Sa CONTROL OF AUBES WITH VARIABLE SETTING ANGLE
EP1961922A3 (en) * 2007-02-22 2010-11-17 Snecma Control of variable pitch angle blades
US8147187B2 (en) 2007-02-22 2012-04-03 Snecma Control of variable-pitch blades
FR2982653A1 (en) * 2011-11-14 2013-05-17 Snecma CANNELE SHAFT TRANSMISSION SYSTEM.
WO2017189566A3 (en) * 2016-04-25 2017-12-28 Florida Turbine Technologies, Inc. Twin spool industrial gas turbine engine with variable inlet guide vanes

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