FIELD: turbojet engines. SUBSTANCE: proposed double-flow turbojet engine reheat unit contains outer ferrule and ferrule separating loops and flame stabilizer and fuel nozzles arranged in inner loop. Loops communicate lower in direction of flow from flame stabilizer exit section at distance not less than width of its flange. Reheat unit can be provided with head shield whose intake is arranged coaxially between outer ferrule and separating ferrule. Additional fuel nozzles are arranged in channel limited by separating ferrule and head shield. EFFECT: improved thrust and combustion characteristics of double-flow turbojet engine. 2 cl, 2 dwg
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