FR1528203A - Axial turbine nozzle guide vane system - Google Patents

Axial turbine nozzle guide vane system

Info

Publication number
FR1528203A
FR1528203A FR108845A FR108845A FR1528203A FR 1528203 A FR1528203 A FR 1528203A FR 108845 A FR108845 A FR 108845A FR 108845 A FR108845 A FR 108845A FR 1528203 A FR1528203 A FR 1528203A
Authority
FR
France
Prior art keywords
guide vane
turbine nozzle
nozzle guide
axial turbine
vane system
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
FR108845A
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.)
Rover Co Ltd
Original Assignee
Rover 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
Priority claimed from GB24823/66A external-priority patent/GB1119439A/en
Application filed by Rover Co Ltd filed Critical Rover Co Ltd
Priority to FR108845A priority Critical patent/FR1528203A/en
Application granted granted Critical
Publication of FR1528203A publication Critical patent/FR1528203A/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)
FR108845A 1966-06-03 1967-06-02 Axial turbine nozzle guide vane system Expired FR1528203A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR108845A FR1528203A (en) 1966-06-03 1967-06-02 Axial turbine nozzle guide vane system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB24823/66A GB1119439A (en) 1966-06-03 1966-06-03 Adjustable nozzle guide vane assembly for an axial flow turbine
FR108845A FR1528203A (en) 1966-06-03 1967-06-02 Axial turbine nozzle guide vane system

Publications (1)

Publication Number Publication Date
FR1528203A true FR1528203A (en) 1968-06-07

Family

ID=26176994

Family Applications (1)

Application Number Title Priority Date Filing Date
FR108845A Expired FR1528203A (en) 1966-06-03 1967-06-02 Axial turbine nozzle guide vane system

Country Status (1)

Country Link
FR (1) FR1528203A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2443577A1 (en) * 1978-12-04 1980-07-04 Gen Electric DEVICE FOR MAINTAINING A MINIMUM GAME BETWEEN AERODYNAMIC PROFILES AND THE WALLS OF THE GAS FLOW PATH OF A GAS TURBINE ENGINE
FR2599086A1 (en) * 1986-05-23 1987-11-27 Snecma Device for controlling the variable-pitch air inlet directing vanes of a jet engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2443577A1 (en) * 1978-12-04 1980-07-04 Gen Electric DEVICE FOR MAINTAINING A MINIMUM GAME BETWEEN AERODYNAMIC PROFILES AND THE WALLS OF THE GAS FLOW PATH OF A GAS TURBINE ENGINE
FR2599086A1 (en) * 1986-05-23 1987-11-27 Snecma Device for controlling the variable-pitch air inlet directing vanes of a jet engine

Similar Documents

Publication Publication Date Title
BE744592A (en) SPACING ELEMENT FOR TURBOMACHINE BLADES
CH463877A (en) Turbine nozzle
FR1529698A (en) Character identification system
FR1547844A (en) Turbine blade
FR1462062A (en) Axial centering device for the fins of a turbomachine rotor
FR1511726A (en) Construction of blades for a helicopter rotor
FR1507568A (en) Excitation system
FR93891E (en) Erosion reducer.
FR1528203A (en) Axial turbine nozzle guide vane system
FR1536480A (en) Aircraft stop system
FR1500793A (en) Safety axis stop
FR1512120A (en) Wiper blade
FR89439E (en) Hydraulic servo device
CH445524A (en) Turbine guide vane attachment
FR1500148A (en) Improved stop arrangement for drilling turbines
FR1462137A (en) Conical drawing die
FR1390593A (en) Diffuser, in particular for fixed irrigation systems
FR94167E (en) Improvements to waveguide filters.
FR1537338A (en) Turbomachine rotor
FR1523664A (en) Flow modifier
OA02689A (en) Erosion reducer.
FR1541926A (en) Coating system
FR1492358A (en) Animation system
FR91174E (en) Animation system
FR1529342A (en) Turbomachinery foundation