TURBOMACHINE WITH UNCOUPLING DEVICE, COMMON FOR FIRST AND SECOND BEARINGS OF ITS CONTROL SHAFT, COMPRESSOR, CONSISTING UNCOUPLING DEVICE, AND UNCOUPLING DEVICE Russian patent published in 2009 - IPC F01D21/04 

Abstract RU 2362888 C2

FIELD: mechanical engineering.

SUBSTANCE: invention relates to turbomachine, compressor and uncoupling device. Turbomachine contains rotor with control shaft, centered on the axis of turbomachine by means the first bearing and the second bearing, herewith bearings hold suitably by means of bearing part of the first bearing and bearing part of the second bearing, which are affixed to each other and connected to immovable structure of turbomachine by means of uncoupling device. Such turbomachine contains facilities, provided for joint action, at least, with one part of immovable structure of turbomachine for implementation of double function - prevention of gyration of bearing supports and holding of control shaft in radial direction in case of bearings detaching.

EFFECT: such implementation of turbomachine, compressor and uncoupling device will provide cost cutting and its weight.

21 cl, 3 dwg

Similar patents RU2362888C2

Title Year Author Number
TURBOMACHINE WITH ROTOR AXIAL CLAMP 2005
  • Laperg Gi
  • Servan Rezhi
  • Bushi Gaehl'
  • Bom Alen
RU2382886C2
TURBOJET ENGINE WITH FAN FIXED TO DRIVING SHAFT RETAINED BETWEEN FIRST AND SECOND BEARINGS 2005
  • Laperg Gi
  • Servan Rezhi
  • Bushi Gaehl'
RU2361100C2
SUPPORT ASSEMBLY OF TURBOMACHINE REDUCER SYSTEM AND METHOD OF REDUCER SYSTEM SUPPORT IN TURBOMACHINE 2013
  • Otto Dzhon R.
RU2644421C2
JET TURBINE ENGINE WITH FAN WHICH IS INTEGRAL WITH DRIVE SHAFT SUPPORTED WITH FIRST AND SECOND BEARINGS 2005
  • Laperg Gi
  • Servan Rezhi
  • Bushi Gaehl'
RU2386050C2
MODULAR ENGINE, SUCH AS JET ENGINE, WITH SPEED REDUCTION GEAR 2014
  • Bro Mishel Zhilber Rolan
  • Novakovski Natali
RU2674098C1
TURBOFAN ENGINE WITH COMPACT SYSTEM OF AIR TAKEOFF FROM BOOSTER COMPRESSOR 2006
  • Moniz Tomas Ori
RU2433312C2
AIRCRAFT COUNTER ROTATION GAS-TURBINE ENGINE WITH COMPRESSOR WITH HIGH COMMON DEGREE OF PRESSURE RISE 2003
  • Seda Dzhordzh F.
  • Danbar Lorens V.
  • Such Peter N.
  • Brauehr Dzhon S.
  • Dzhonson Dzhejms E.
RU2302545C2
CYCLOIDAL REDUCER, FAN MODULE OF DUAL-FLOW TURBOJET ENGINE AND DUAL-FLOW TURBOJET ENGINE 2013
  • Galle Fransua
  • Briante Boris
  • Serej Zhan-Per
  • Tan-Kim Aleksandr
RU2627990C2
DEVICE FOR MEASURING AIRFLOW CHARACTERISTICS 2019
  • Verniau Jean-Luc
  • Polo Filisan Gilles
  • Sozuan Adnan
  • Paris Simon
RU2784992C2
GEARED FAN WITH INNER COUNTER ROTATING COMPRESSOR 2013
  • Magovan Dzhon V.
RU2665572C2

RU 2 362 888 C2

Authors

Bro Mishel'

Morel' Patrik

Ziga Zoltan

Bushi Gaehl'

Pandelaki P'Er

Dates

2009-07-27Published

2005-11-18Filed