ES257350A1 - Un turbomotor de gas - Google Patents

Un turbomotor de gas

Info

Publication number
ES257350A1
ES257350A1 ES0257350A ES257350A ES257350A1 ES 257350 A1 ES257350 A1 ES 257350A1 ES 0257350 A ES0257350 A ES 0257350A ES 257350 A ES257350 A ES 257350A ES 257350 A1 ES257350 A1 ES 257350A1
Authority
ES
Spain
Prior art keywords
guide vanes
movement
relating
gas turbine
link 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
ES0257350A
Other languages
English (en)
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of ES257350A1 publication Critical patent/ES257350A1/es
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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)

Abstract

Turbomotor de gas que tiene: un compresor o una turbina provista de paletas de guía o álabes directores montados a pivotamiento; un dispositivo de accionamiento de álabes dispuesto por el interior de los álabes directores, dando lugar el movimiento de dicho dispositivo a un movimiento de pivotamiento de los álabes directores; medios dispuestos al exterior del motor para efectuar el movimiento del dispositivo de accionamiento de álabes; y un sistema de enlace articulado, espaciado de dichos álabes y que conecta los medios externos con el dispositivo de accionamiento de álabes, estando dicho sistema de enlace dispuesto de modo que no ocasiona obstrucción alguna, o esencialmente ninguna, al paso de fluido a través del motor.
ES0257350A 1959-04-30 1960-04-13 Un turbomotor de gas Expired ES257350A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1478059A GB876504A (en) 1959-04-30 1959-04-30 Improvements in or relating to gas turbine engines

Publications (1)

Publication Number Publication Date
ES257350A1 true ES257350A1 (es) 1960-06-16

Family

ID=10047357

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0257350A Expired ES257350A1 (es) 1959-04-30 1960-04-13 Un turbomotor de gas

Country Status (2)

Country Link
ES (1) ES257350A1 (es)
GB (1) GB876504A (es)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231960B (de) * 1962-12-17 1967-01-05 Rolls Royce Kombiniertes Gasturbinenstrahl- und Staustrahltriebwerk
GB971222A (en) * 1962-12-17 1964-09-30 Rolls Royce Gas turbine power plant
US3630633A (en) * 1970-05-07 1971-12-28 Ford Motor Co Gas turbine engine nozzle actuation system
US8915703B2 (en) * 2011-07-28 2014-12-23 United Technologies Corporation Internally actuated inlet guide vane for fan section

Also Published As

Publication number Publication date
GB876504A (en) 1961-09-06

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