MONOBLOCK POST-FLAME STABILIZER FOR AFTERBURNER OF DOUBLE-FLOW TURBOJET ENGINE AND AFTERBURNER USED IN ENGINE Russian patent published in 2007 - IPC F02K3/10 F23R3/18 

Abstract RU 2309279 C2

FIELD: turbojet engines.

SUBSTANCE: support post 13 is designed for mounting in radial position in double-flow turbojet engine afterburner. Device contains first and second inner ring cases forming channel for primary flow, and outer ring case forming, together with first inner ring case, channel for secondary flow. Post 13 has monoblock structure made of composite material and containing two interconnected walls 14, 15 at one side made to form cavity 16 mainly of V-shaped profile and provided at other side with first end parts 17 interconnected and made to form leg 18, and second end parts 19, each made to form at least one flange 20, 21 designed for rigid connected with outer ring case 5.

EFFECT: improved operating characteristics, reduced temperature difference between support posts and case; improved operation capabilities.

31 cl, 10 dwg

Similar patents RU2309279C2

Title Year Author Number
AFTERBURNER OF DOUBLE-FLOW JET TURBINE ENGINE, DOUBLE-FLOW JET TURBINE ENGINE AND BRACKET OF FLAME STABILISER FOR AFTERBURNER 2007
  • Bjunel' Zhak Marsel'
  • Pazh Alen P'Er
  • Rosh Zhak Andre Mishel'
  • Vjuill'Meno Iann Fransua Zhan-Klod
RU2406033C2
ATTACHMENT OF FLAME STABILISER STRUT AT AUGMENTER BODY 2009
  • Ehrnandes Did'E Ippolit
  • Berdu Karolin Zhaklin Deniz
  • Bjunel' Zhak Marsel' Artjur
  • Vjuill'Mon Iann Fransua Zhan-Klod
RU2508508C2
DEVICE FOR SECURING ANNULAR BURNER WITHIN TURBOJET-ENGINE AFTERBURNER 2005
  • Bjunel' Zhak
  • Roshe Zhak
RU2293861C2
REHEAT RING FOR DOUBLE-FLOW TURBOJET ENGINE, REHEAT DEVICE AND TURBOJET ENGINE 2004
  • Bjunel' Zhak Marsel' Artjur
  • Rosh Zhak Andre Mishel'
  • Rakotondrenib B'En-Ehme Oliv'E Solo Samjuehl' Filipp
  • Tusho Stefan Anri Gi
RU2291315C2
GAS TURBINE ENGINE FAN CHANNEL 2007
  • Beten Brjuno Al'Ber
  • Derene Zhaki Rafaehl' Mishel'
RU2452865C2
DUCT BURNING BYPASS ENGINE WITH PROTECTIVE SCREEN FOR NOZZLE RING FUEL MANIFOLD, NOZZLE RING AND PROTECTIVE SCREEN 2005
  • Pazh Alen P'Er
  • Pomm'E Nikola
  • Rosh Zhak-A
  • Tusho Stefan Anri Gi
RU2382895C2
GAS TURBINE ENGINE AND STARTER-GENERATOR FOR GAS-TURBINE ENGINE 2007
  • Bujer Filipp P'Er Vinsen
  • Loran Ehntoni
  • Russelehn Stefan
RU2406829C2
INTERMEDIATE CASE OF JET TURBINE ENGINE, AND JET TURBINE ENGINE 2008
  • Djushatell' T'Erri
  • Verso Filipp
RU2484262C2
BRACKET OF FLAME STABILISER OF AFTERBURNER DUCT, VENTILATION CHAMBER OF FLAME STABILISER BRACKET, AND GAS-TURBINE ENGINE 2007
  • Bjunel' Zhak Marsel'
  • Zhirar Nikolja P'Er-Mari
RU2410604C2
DEVICE FOR AIR AND FUEL SUPPLY TO RING OF NOZZLES IN AFTERBURNER 2005
  • Bjunel' Zhak
  • Roshe Zhak
RU2358139C2

RU 2 309 279 C2

Authors

Blanshar Stefan P'Er Gijom

Tusho Stefan Anri Gi

Panku T'Erri Gabriehl'

Konet Ehrik

Kami P'Er

Abaru Zhorzh

Dates

2007-10-27Published

2005-01-21Filed