IMPROVED CHARACTERISTICS OF COMBUSTION CHAMBER BY MULTI-PERFORATION OF ITS WALLS Russian patent published in 2011 - IPC F23R3/06 

Abstract RU 2413134 C2

FIELD: machine building.

SUBSTANCE: in wall there are made multitude of primary orifices, multitude of orifices of dilution to ensure penetration of air moving from cold side of wall to hot side and ensuring combustion and dilution of fuel mixture with air and multitude of cooling orifices designed for penetration of air moving from cold side of wall to its hot side to generate film of cooling air along said wall. The primary orifices and dilution orifices are distributed along radial rows. The cooling orifices are distributed along multitude of radial rows spaced one from another in axial direction at a certain distance; number of these cooling orifices is equal in each of the said rows. A circular wall additionally has multitude of orifices of perforation arranged directly behind and downstream from the primary orifices and dilution orifices and distributed along multitude of circular rows. The perforation orifices of the same row have in essence equal diametre, are spaced from each other at a certain constant interval and possess characteristics different from corresponding characteristics of the said orifices of cooling in adjacent rows.

EFFECT: reduced cost and time for fabrication of circular wall of combustion chamber.

6 cl, 3 dwg

Similar patents RU2413134C2

Title Year Author Number
COMBUSTION CHAMBER WALL WITH OPTIMISED LIQUEFACTION AND COOLING; COMBUSTION CHAMBER AND GAS TURBINE ENGINE EQUIPPED WITH SUCH WALL 2008
  • Kazalen Mishel' P'Er
  • Kommare Patris Andre
  • Ljunel' Romehn Nikolja
RU2478875C2
ANNULAR WALL OF COMBUSTION CHAMBER WITH OPTIMIZED COOLING 2016
  • Commaret, Patrice, Andre
  • Bunel, Jacques, Marcel, Arthur
  • Lunel, Romain, Nicolas
RU2718371C2
CIRCULAR COMBUSTION WALL WITH PERFECTED COOLING AT PRIMARY BORES AND/OR DILUTION BORES LEVEL 2012
  • Rjullo Matt'E Fransua
  • Karrer Bernar Zhozef Zhan-P'Er
  • Verd'E Juber Paskal'
RU2575490C2
ANNULAR COMBUSTION CHAMBER FOR GAS TURBINE ENGINE CONTAINING IMPROVED HOLES FOR COOLING 2012
  • Leblon Nikolja Kristian Rajmon
  • Bjunel Zhak Marsel Artjur
  • Len Dominik Moris Zhak
RU2584746C2
ANNULAR COMBUSTION CHAMBER OF GAS-TURBINE ENGINE, GAS TURBINE CHAMBER, ELEMENT OF SIDE WALL DESIGNED TO FORM COMBUSTION CHAMBER 2007
  • B'Ebel' Romehn
  • Dagene Ljuk
  • Sandeli Deni
RU2354889C2
INJECTION DEVICE OF FUEL-AIR MIXTURE, COMBUSTION CHAMBER AND GAS TURBINE ENGINE EQUIPPED WITH SUCH DEVICE 2006
  • Kommare Patris Andre
  • Sandeli Deni Zhan Moris
  • Trao Deni
RU2420691C2
GAS TURBINE ENGINE COMBUSTION CHAMBER 2007
  • Bessan'E Florian Andre Fransua
  • Kommare Patris Andre
  • De Suza Mario Sezar
  • Ehrnandes Did'E Ippolit
RU2457400C2
COMBUSTION CHAMBER WITH OPTIMISED DISSOLUTION AND TURBOMACHINE EQUIPPED WITH SUCH CHAMBER 2008
  • Kamp'On Zhan-Mishel' Zhak
  • Kazalen Mishel' P'Er
  • Kommare Patris Andre
  • Rolle Paskal'
RU2474763C2
INJECTION SYSTEM OF AIR MIXED WITH FUEL TO COMBUSTION CHAMBER OF GAS TURBINE ENGINE 2008
  • P'Esserg Kristof
  • Sandeli Deni Zhan Moris
RU2478878C2
GAS TURBINE ENGINE COMBUSTION CHAMBER WALL VENTILATION SYSTEM AND GAS TURBINE ENGINE WITH SAID SYSTEM 2007
  • Kommare Patris
  • Ehrnandes Did'E
  • Lokatelli David
RU2446296C2

RU 2 413 134 C2

Authors

Bern'E Daniel'

Kamp'En Zhan-Mishel'

Tusho Stefan

Dates

2011-02-27Published

2006-10-17Filed