FIELD: machine building.
SUBSTANCE: flame stabilizer for afterburner turbojet engine comprises chute-shaped post forming cavity, and heat shield fixed in rack cavity. Flame stabilizer additionally comprises a fastening plate having a first tab made integral with the fastening plate, and a second leg installed with possibility of removal on the plate. Post is attached to the first and second legs by means of fasteners.
EFFECT: invention is aimed at simplifying the mounting plate and reducing the manufacturing costs thereof.
10 cl, 7 dwg
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