CENTRING DEVICE, INPUT GUIDE VANES AND TURBINE MACHINE Russian patent published in 2015 - IPC F04D29/00 

Abstract RU 2562503 C2

FIELD: machine building.

SUBSTANCE: centring device contains rotating part made with possibility of rotation around the first axis passing along the axial direction of the hole, made in the rotating part, roller secured to the first end of the rotating part and made with possibility of rotation, rod secured to the second end of the rotating part and made with possibility of movement along the second axis, spring mechanism, in which part of said rod is located, and that is made with possibility of pressing force application to the rotating part, and casing for rod made with possibility of location in it of the said rod end.

EFFECT: invention excludes possibility of shift of the lead ring, and reduction of thermal expansion of input guide vanes.

10 cl, 11 dwg

Similar patents RU2562503C2

Title Year Author Number
DRIVING INLET GUIDE VANES, TURBO-MACHINE AND METHOD OF TURBINE MACHINE DRIVING INLET GUIDE VANES MAKING 2012
  • Asti Antonio
  • Del Turco Paolo
  • Landi Giacomo
RU2616336C2
TURBOFAN GAS TURBINE ENGINE WITH ADJUSTABLE FAN OUTLET GUIDE VANES (VERSIONS) 2006
  • Vud Piter Dzhon
  • Zenon Rubi Lasandra
  • Lachapelle Donald Dzhordzh
  • Milke Mark Dzhozef
  • Grant Karl
RU2435057C2
CONTROL RING OF STAGE OF BLADES WITH VARIABLE ANGLE OF INSTALLATION FOR GAS TURBINE ENGINE 2015
  • Bazot, Olivier
  • Edynak, Jeremy
RU2705128C2
VANED-ROTOR ICE 2009
  • Khakimov Viktor Alekseevich
RU2413853C1
TURBINE ENGINE COMPRESSOR, IN PARTICULAR OF AEROPLANE TURBOPROP OR TURBOFAN 2014
  • Sebrecht Pierre-Alain Francis Claude
  • Cochon Sebastien
  • Langlois Arnaud
RU2670473C1
GAS TURBINE ENGINE AIR MANIFOLD 2009
  • Bil' Ehrik Stefan
  • Bro Mishel' Zhil'Ber Rolan
RU2494287C2
ADJUSTABLE INPUT GUIDE 2023
  • Kruglov Aleksandr Mikhajlovich
  • Nikitin Stanislav Evgenevich
  • Chirkov Artur Konstantinovich
RU2814582C1
VELOMOBILE WITH PNEUMATIC AND ACCUMULATOR DRIVE 0
  • Chikin German Alekseevich
SU1717471A1
CONNECTION OF DEVICE OF BALL HINGE WITH ANGULAR TRANSMISSION PLUG TYPE, CONTROL SYSTEM OF STRAIGHTENER BLADE WITH ADJUSTABLE BLADE SETTING ANGLE, WHICH CONTAINS SUCH CONNECTION, AND AIRCRAFT ENGINE EQUIPPED WITH SUCH SYSTEM 2007
  • Burju Mishel' Andre
  • Ehtual' Zherar Zhoehl' Patrik
RU2449183C2

RU 2 562 503 C2

Authors

Sarri Franco

Iurisci Giuseppe

Dates

2015-09-10Published

2011-08-30Filed