| 摘要 |
Device for fixing a burner ring onto flameholder arms ( 14 ) in an afterburner combustion chamber of a turbojet engine, the burner ring being formed of ring sectors ( 12 ) placed more or less end to end and the ends of which are housed and guided between two circumferentially-directed parallel plates ( 34, 36 ) of the flameholder arms ( 14 ) and are immobilized between these plates ( 34, 36 ) by locking pieces ( 52 ) which are themselves held between the plates ( 34, 36 ) by immobilizing means ( 54, 56 ) engaged in aligned orifices ( 58, 60, 64 ) in the plates ( 34, 36 ) and in the locking pieces ( 52 ).
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