GAS TURBINE ENGINE AND STARTER-GENERATOR FOR GAS-TURBINE ENGINE Russian patent published in 2010 - IPC F01D15/10 F02C7/27 

Abstract RU 2406829 C2

FIELD: machine building.

SUBSTANCE: gas-turbine engine consists of electric starter-generator, rotor of which is driven to rotation by shaft of compressor of high pressure, stator of which is mounted on intermediate carter of gas-turbine engine. The starter-generator is enclosed into a pressure tight case installed in a front compartment of the gas-turbine engine inside the intermediate carter containing oil. Compressed air is supplied into the pressure tight case of the starter-generator. The pressure tight case consists of the first elements of connection with electric cables running in structure poles of the intermediate carter. Also the first elements of connection are pressure tight and are arranged inside a chamber restricted with the case and the intermediate carter; the chamber is fed with compressed air. The starter-generator consists of an external cylinder element forming a support for the stator, of an internal cylinder element coaxial to the external cylinder element and forming the support of the rotor, and of circular covers secured on axial ends of the external cylinder element and interacting with the internal cylinder element. Bent devices for connection of stator coils with electric cables projecting outside the case in axial direction are arranged on the external cylinder element of the case.

EFFECT: facilitation of assembly and disassembly of built-in starter-generator and simplification of its connection with feeding electric cables or cables of current distribution.

15 cl, 5 dwg

Similar patents RU2406829C2

Title Year Author Number
FRONT PART OF AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE AND AIRCRAFT DOUBLE-FLOW GAS TURBINE ENGINE 2015
  • Nowakowski, Nathalie
  • Vincent, Thomas, Alain, Christian
RU2686248C2
STATOR OF AIRCRAFT GAS TURBINE ENGINE AND AIRCRAFT GAS TURBINE ENGINE 2015
  • Charbonnier, Simon, Pierre, Claude
  • Perrier, Matthieu, Yoann
RU2706098C2
DISTRIBUTED ARCHITECTURE OF GAS TURBINE STARTER-GENERATOR 2008
  • Bekkerell' Samjuehl'
  • Galivel' Zhan-P'Er
RU2445481C2
JET TURBINE ENGINE EQUIPPED WITH BUILT-IN ELECTRIC GENERATOR 2005
  • Bujer Filipp
  • Morr'Al' Serzh
  • Russelehn Stefan
RU2424435C2
ATOMIC SUBMARINE AND MARINE-VERSION GAS TURBINE ENGINE 2011
  • Bolotin Nikolaj Borisovich
  • Nefedova Elena Nikolaevna
  • Bolotina Marina Nikolaevna
RU2481233C1
ASSEMBLY FOR AIRCRAFT GAS-TURBINE ENGINE AND METHOD OF ITS MOUNTING 2015
  • Lemarchand, Kevin, Morgane
RU2673027C2
GAS TURBINE ENGINE 2016
  • Grigorev Aleksej Vladimirovich
  • Soloveva Anastasiya Valerevna
  • Zhurenkov Yurij Nikolaevich
RU2657051C1
GAS TURBINE ENGINE 2008
  • Bolotin Nikolaj Borisovich
RU2382210C1
GAS TURBINE ENGINE 2011
  • Generalov Nikolaj Petrovich
RU2463464C1
GAS-TURBINE ENGINE 2006
  • Grigorchuk Vladimir Stepanovich
RU2315191C1

RU 2 406 829 C2

Authors

Bujer Filipp P'Er Vinsen

Loran Ehntoni

Russelehn Stefan

Dates

2010-12-20Published

2007-01-23Filed