FIELD: engines and pumps.
SUBSTANCE: proposed combustion chamber has main axis, inner and outer walls, chamber base arranged between said walls at chamber front and two fastening clips. Said clips are arranged behind the chamber to attach said walls to gas turbine engine parts. Each said wall is divided into multiple adjacent sectors. Each sector is attached to chamber base and one of said clips. Lateral edges of sectors are inclined to aforesaid main axis.
EFFECT: invention allows compensating difference in linear expansion between inner and outer walls, chamber base and fastening clips.
9 cl, 5 dwg
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