LINE OF FLOW-STRAIGHTENING GRID VANES DRIVEN BY ROTARY RING DRIVEN BY ELECTRICAL ACTUATORS, COMPRESSOR INCORPORATING SAID LINE OF VANES AND TURBOJET ENGINE COMPRISING SUCH COMPRESSOR Russian patent published in 2010 - IPC F01D17/14 F04D29/56 F01D9/02 

Abstract RU 2397331 C2

FIELD: engines and pumps.

SUBSTANCE: line of vanes with variable pitch comprises vanes arranged in casing and driven by their control system. Said control system comprises driving ring secured on said casing and articulated by levers with aforesaid vanes to set them moving simultaneously. Driving ring is simply revolved around turbojet engine axis. Control system comprises two coaxial parts, namely: inner part rigidly coupled with casing and outer part incorporating said driving ring coupled with aforesaid levers and directed to revolve about said inner part. At least one electrically driven unit is arranged between said inner and outer parts. Another invention of the set relates to compressor furnished with said row of vanes of straightening grid. One more invention relates to turbojet engine comprises aforesaid compressor.

EFFECT: accurate alignment of driving ring with engine axis.

12 cl, 5 dwg

Similar patents RU2397331C2

Title Year Author Number
ROW OF BLADES OF STRAIGHTENING DEVICE DRIVEN WITH ROTARY RING OF AUTOMATIC CENTRING, COMPRESSOR EQUIPPED WITH SAID ROW OF BLADES AND GAS-TURBINE MOTOR CONTAINING THIS COMPRESSOR 2005
  • Burju Mishel' Andre
RU2416724C2
ASSEMBLY OF FIXED GUIDE VANES, COMPRESSOR OF GAS TURBINE ENGINE AND GAS TURBINE ENGINE 2007
  • Abgrall' Oliv'E
  • Kloarek Ivon
RU2439338C2
MULTI-STAGE COMPRESSOR FOR TURBOMACHINE 2006
  • Shar'E Zhil' Alen Mari
  • Konan Frank Kristian
  • Eharit Toma Zhjul'En Rolan
  • Leandri Mark
RU2375607C2
METHOD FOR SOLDERING VANES OF STRAIGHTENING APPARATUS OF COMPRESSOR OF TURBINE-JET ENGINE 2004
  • Klemen Zhan-Fransua Did'E
RU2290285C2
VORTEX GENERATORS AT INLET OF COMPRESSOR BLADE SYSTEM 2011
  • Domerk Olive Stefan
  • Perro Vensan Pol Gabriel
  • Pestej Anes
RU2583190C2
AIR BLEED DEVICE, COMPRESSOR STAGE WITH SAID DEVICE, COMPRESSOR WITH SAID STAGE, AND TURBOJET WITH SAID COMPRESSOR 2008
  • Deren Zhaki
  • Russelehn Stefan
RU2467209C2
GAS TURBINE ENGINE COMPRESSOR AND INSERT FOR SAID COMPRESSOR 2005
  • Fushe Kristell'
  • Lezhar Klod Rober Lui
  • Ribi Did'E
RU2405975C2
GAS COMPRESSOR GUIDE VANES SYSTEM TO BE FITTED IN THROAT 2010
  • Klemons Dzhonatan D.
  • Sabin Mark R.
  • Gerber Tomas E.
RU2508476C2
AIR INJECTION INTO GAS TURBINE ENGINE COMPRESSOR PATH 2009
  • Domerk Oliv'E Stefan
  • Perro Vensan Pol' Gabriehl'
  • Puatven Zhan-P'Er
RU2482339C2
SYSTEM TO MODIFY ANGLE OF ATTACK OF IMPELLER BLADES IN GAS TURBINE ENGINE OF AIRCRAFT, USING BRUSHLESS ELECTRIC MOTOR 2010
  • Ehro Zhan-Lui
RU2531088C2

RU 2 397 331 C2

Authors

Burju Mishel' Andre

Dates

2010-08-20Published

2005-12-15Filed