GAS TURBINE ENGINE COMPRESSOR COVER WITH AXIAL THRUST Russian patent published in 2014 - IPC F04D29/42 F01D25/24 

Abstract RU 2509232 C2

FIELD: engines and pumps.

SUBSTANCE: radial flow compressor comprises: cover 100, housing 30 and working wheel. Cover 100 includes upstream end 40a and downstream end 100b. Case 30 has upstream edge 32 and downstream edge 34. Vaned working wheel is fitted in the housing to run therein. Cover can close said vanes 28 to outer surface of make gas flow channel 38 extending between case upstream and downstream edges. Cover is secured to the case upstream edge by its upstream end while its downstream end 100b is free. additionally, said cover comprises thrust 102 to limit axial displacement of axial displacement of it downstream end 100b relative to the case downstream edge 34 in operation of the compressor.

EFFECT: ruled out contact between cover and vanes.

6 cl, 3 dwg

Similar patents RU2509232C2

Title Year Author Number
LOW-PRESSURE TURBINE OF GAS TURBINE MOTOR 2004
  • Bart Zhak
  • Betin Bruno
  • Buijer Filipp
RU2342547C2
FRAME, COMPRESSOR, TURBO AND GASTURBINE ENGINE INCLUDED INTO FRAME 2003
  • Le B'E Filipp
  • Lebre Jan
  • Mon Marsel'
RU2324076C2
TRANSITION CHANNEL BETWEEN TWO STAGES OF TURBINE AND GAS-TURBINE ENGINE 2007
  • Gimbar Zhan-Mishel'
  • Pabion Filipp
  • Shvarts Ehrik
  • Supizon Zhan-Ljuk
RU2455498C2
HEAT SHIELD FOR GAS TURBINE ENGINE 2018
  • Viano, Andrea
RU2748819C1
AUXILIARY EQUIPMENT DRIVE 2003
  • Bujler Filipp
  • Franshe Mishel'
  • Rjui Zhan-P'Er
RU2321761C2
PLATFORM FOR GAS TURBINE ENGINE WHEEL, BLADE, TURBINE WHEEL, COMPRESSOR AND GAS TURBINE ENGINE 2008
  • Derkle Alen
  • Ehrnst Filipp
RU2513535C2
ASSEMBLY CONSISTING OF TURBINE NOZZLE OR COMPRESSOR STATOR VANE MADE OF CMC FOR TURBINE ENGINE AND ABRADABLE SUPPORT RING, AND TURBINE OR COMPRESSOR INCLUDING SUCH ASSEMBLY 2012
  • Bozhar Antuan Zhan-Filipp
  • Fremon Elrik Zhorzh Andre
RU2601052C2
DEVICE FOR COOLING CASE OF TURBINE IN TURBO-MACHINE 2007
  • Dervo Aleksandr Nikolja
  • Azevis Filipp Zherar Mari
  • Marte Reno
  • Pabion Filipp Zhan-P'Er
  • Rozhe Stefani Dominik
  • Shvarts Ehrik
RU2416028C2
DUAL-CURVATURE VANE FOR TURBINE GUIDE VANES 2004
  • Fessu Filipp
  • Blozovski Mario
  • Ken'Ju Ehrve
RU2341660C2
GAS TURBINE ENGINE WITH A RADIAL DIFFUSER AND A SHORT-TERM MEDIUM PART 2013
  • Charron Richard K.
  • Montgomeri Mettyu D.
RU2631181C2

RU 2 509 232 C2

Authors

Zhuber Filipp

Labord Patris

Muz Jann

Pero Filipp

Dates

2014-03-10Published

2009-05-20Filed