SYSTEM TO CONTROL TURBOJET ENGINE STATOR VANES WITH VARIABLE MOUNTING ANGLE Russian patent published in 2010 - IPC F01D17/16 

Abstract RU 2396438 C2

FIELD: engines and pumps.

SUBSTANCE: proposed system comprises drive element to revolve control ring of one of the stages by means of drive member arranged to turn on the casing, synchro lever to transmit aforesaid lever rotation to control ring of the other stage by means of servo element arranged to turn on aforesaid casing, and additional rotary member arranged between servo element and driven ring. Note here that said additional rotary member is arranged to turn simultaneously on the casing and said servo element.

EFFECT: possibility to vary vane mounting angle with acceleration (or deceleration) at certain local zone of control trajectory.

6 cl, 3 dwg

Similar patents RU2396438C2

Title Year Author Number
SYSTEM TO CONTROL TURBOJET ENGINE STATOR VANES WITH VARIABLE MOUNTING ANGLE 2006
  • Burju Mishel'
RU2396439C2
SYSTEM OF ROTATING BLADES STAGES CONTROL OF HIGH PRESSURE COMPRESSOR STATOR 2011
  • Krasinskij Leonid Grigor'Evich
  • Krjuchkov Jurij Aleksandrovich
  • Shishkin Anton Sergeevich
RU2474698C1
SYSTEM TO CONTROL EQUIPMENT OF GAS TURBINE ENGINE WITH VARIABLE GEOMETRY, IN PARTICULAR, BY MEANS OF CONTROL LEVERS 2009
  • Kolott Batist Benua
  • Golli Brjuno Rober
RU2501957C2
DEVICE TO VARY BLADES ANGLE IN TWO-STAGE FIXED BLADDING OF TURBOJET ENGINE 2004
  • Ren Floran
  • Rolen Dominik
  • Shatel' Alen Zhan Sharl'
RU2338932C2
CONTROL SYSTEM FOR EQUIPMENT WITH VARIABLE-GEOMETRY OF GAS TURBINE ENGINE COMPRISES, IN PARTICULAR, TRACKWAY JOINT 2009
  • Kolott Batist Benua
  • Golli Brjuno Rober
RU2507402C2
DRIVE ON BASE OF SYNCHRONIZED HYDRAULIC CYLINDERS, REACTION NOZZLE OF TURBOJET ENGINE (VERSIONS) AND TURBOJET ENGINE 2003
  • Brokar Zhan-Mari
  • Kettler Daniehl'
  • Lavi Alen
  • Misho Marion
RU2311553C2
SYSTEM FOR CONTROLLING VARIABLE GEOMETRY DEVICES IN TURBO MACHINES AND TURBO MACHINE HAVING SAID SYSTEM 2009
  • Burju, Mishel'
  • Golli, Brjuno
RU2529762C2
EQUIPMENT CONTROL SYSTEM WITH VARIABLE GEOMETRY OF GAS-TURBINE ENGINE, WHICH CONTAINS IN PARTICULAR DRUM CONNECTION 2009
  • Kolott Batist Benua
  • Golli Brjuno Rober
RU2503824C2
THRUST REVERSAL UNIT FOR TURBOJET ENGINE WITH ROTATABLE DOORS COUPLED WITH SYNCHRONIZATION AND CONTROL DEVICE 1998
  • Bodju P'Er Andre Marsel'
  • Gonidek Patrik
  • Ruje Paskal' Zherar
  • Voshel' Gi Bernar
RU2151316C1
AIR BLEED DEVICE, COMPRESSOR STAGE WITH SAID DEVICE, COMPRESSOR WITH SAID STAGE, AND TURBOJET WITH SAID COMPRESSOR 2008
  • Deren Zhaki
  • Russelehn Stefan
RU2467209C2

RU 2 396 438 C2

Authors

Burju Mishel'

Dates

2010-08-10Published

2006-05-16Filed