DEVICE FOR SECURING ANNULAR BURNER WITHIN TURBOJET-ENGINE AFTERBURNER Russian patent published in 2007 - IPC F02C7/20 

Abstract RU 2293861 C2

FIELD: attaching annular burner to flame-holder; assembling turbojet-engine afterburners.

SUBSTANCE: annular burner is made in the form of ring sectors butt-to-butt joined in effect; opposing ends of ring sectors arranged in tandem are inserted and passed between two parallel circular-direction plates of flame-holder, locked between these plates by means of locking devices installed between plates and between opposing ends of ring sectors. Locking devices are held in position between mentioned plates with aid of interlocking means mounted in holes of plates and locking devices which are arranged in single line.

EFFECT: facilitated and effective assembly in limited and hard-to-get-space; provision for thermal protecting of fastening means.

14 cl, 9 dwg

Similar patents RU2293861C2

Title Year Author Number
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
DEVICE FOR AIR AND FUEL SUPPLY TO RING OF NOZZLES IN AFTERBURNER 2005
  • Bjunel' Zhak
  • Roshe Zhak
RU2358139C2
OPEN AIR PROPELLER FOR TURBINE MACHINE 2011
  • Burju Mishel' Andre
  • Fabr Adrien Zhak Filipp
  • Jablonski Loran
  • Maje Zhan-Noehl'
RU2558411C2
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 ATTACHMENT OF GUIDE VANES OF TURBINE, TURBINE AND AIRCRAFT ENGINE WITH SUCH EQUIPMENT 2007
  • Bar Zhak
  • Russelehn Stefan
  • Ehskjur Did'E
RU2436965C2
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
CONTROL RING OF STAGE OF BLADES WITH VARIABLE ANGLE OF INSTALLATION FOR GAS TURBINE ENGINE 2015
  • Bazot, Olivier
  • Edynak, Jeremy
RU2705128C2
TURBOMACHINE WHEEL 2008
  • Fabr Adrien Zhak Filipp
RU2477800C2
FLUID PIPE FASTENER IN TURBOJET CASE 2005
  • Bjunel' Zhak
  • Rosh Zhak
  • Rjuehllan Frederik
  • Anri Filipp
RU2362896C2
METHOD TO IMPROVE IGNITION IN TWO-FLOW TURBOJET ENGINE AFTERBURNER AND AFTERBURNER TO THIS END 2005
  • Babef Sebast'En
  • Sharpenel' Sabin
  • Mehngr Ehrik
  • Pazh Alen
  • Rosh Zhak
RU2379537C2

RU 2 293 861 C2

Authors

Bjunel' Zhak

Roshe Zhak

Dates

2007-02-20Published

2005-05-04Filed