FR1053647A - Gas turbine thruster improvements - Google Patents

Gas turbine thruster improvements

Info

Publication number
FR1053647A
FR1053647A FR1053647DA FR1053647A FR 1053647 A FR1053647 A FR 1053647A FR 1053647D A FR1053647D A FR 1053647DA FR 1053647 A FR1053647 A FR 1053647A
Authority
FR
France
Prior art keywords
gas turbine
thruster
turbine thruster
gas
turbine
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)
Inventor
Michel-Robert Garnier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1053647A publication Critical patent/FR1053647A/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)
FR1053647D 1952-04-05 1952-04-05 Gas turbine thruster improvements Expired FR1053647A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1053647T 1952-04-05

Publications (1)

Publication Number Publication Date
FR1053647A true FR1053647A (en) 1954-02-03

Family

ID=9596056

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1053647D Expired FR1053647A (en) 1952-04-05 1952-04-05 Gas turbine thruster improvements

Country Status (1)

Country Link
FR (1) FR1053647A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1016505B (en) * 1954-04-21 1957-09-26 Florencio Bienvenido Casale Continuously working jet engine, especially for motor vehicle propulsion
DE1036582B (en) * 1956-03-28 1958-08-14 Armstrong Siddeley Motors Ltd Gas turbine jet engine
DE1084981B (en) * 1957-01-25 1960-07-07 Konink Luchtvaart Mij N V Aircraft engine
DE1140029B (en) * 1959-07-06 1962-11-22 Gen Electric Control device for a turbo jet engine with compressor guide vanes
DE1237844B (en) * 1959-11-30 1967-03-30 Dowty Rotol Ltd Control device for adjusting the angle of attack of a propeller and the power of the turbine that drives it
EP0795681A1 (en) * 1996-03-14 1997-09-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Actuation mechanism for variable inlet vanes in turbomachine compressor
EP1256698A2 (en) * 2001-05-11 2002-11-13 FIATAVIO S.p.A. Axial turbine with a variable-geometry stator
EP1256697A2 (en) * 2001-05-11 2002-11-13 FIATAVIO S.p.A. Stator vane of a variable-geometry turbine
EP1382804A2 (en) * 2002-07-16 2004-01-21 AVIO S.p.A. Hinge device for a rotary member of an aircraft engine
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 (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1016505B (en) * 1954-04-21 1957-09-26 Florencio Bienvenido Casale Continuously working jet engine, especially for motor vehicle propulsion
DE1036582B (en) * 1956-03-28 1958-08-14 Armstrong Siddeley Motors Ltd Gas turbine jet engine
DE1084981B (en) * 1957-01-25 1960-07-07 Konink Luchtvaart Mij N V Aircraft engine
DE1140029B (en) * 1959-07-06 1962-11-22 Gen Electric Control device for a turbo jet engine with compressor guide vanes
DE1237844B (en) * 1959-11-30 1967-03-30 Dowty Rotol Ltd Control device for adjusting the angle of attack of a propeller and the power of the turbine that drives it
FR2746141A1 (en) * 1996-03-14 1997-09-19 Snecma CONTROL DEVICE FOR INTEGRATED PIVOT IN A MANIFOLD
EP0795681A1 (en) * 1996-03-14 1997-09-17 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Actuation mechanism for variable inlet vanes in turbomachine compressor
EP1256698A2 (en) * 2001-05-11 2002-11-13 FIATAVIO S.p.A. Axial turbine with a variable-geometry stator
EP1256697A2 (en) * 2001-05-11 2002-11-13 FIATAVIO S.p.A. Stator vane of a variable-geometry turbine
EP1256698A3 (en) * 2001-05-11 2004-03-10 AVIO S.p.A. Axial turbine with a variable-geometry stator
EP1256697A3 (en) * 2001-05-11 2004-03-10 AVIO S.p.A. Stator vane of a variable-geometry turbine
US6860717B2 (en) 2001-05-11 2005-03-01 Avio S.P.A. Axial turbine for aeronautical applications
EP1382804A2 (en) * 2002-07-16 2004-01-21 AVIO S.p.A. Hinge device for a rotary member of an aircraft engine
EP1382804A3 (en) * 2002-07-16 2004-09-15 AVIO S.p.A. Hinge device for a rotary member of an aircraft engine
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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