FIELD: engines and pumps.
SUBSTANCE: invention relates to airborne and ground gas turbines, in particular to a coupling of the compressor with the combustion chamber. The gas turbine engine incorporates a high-pressure compressor outer casing and its inner casing, and a casing of the combustion chamber rests. The compressor inner casing is tied with the compressor outer casing and with said casing of the combustion chamber rests by two elastic shells. The casing of the combustion chamber rests goes linked with the outer casing and the compressor inner casing by two elastic shells.
EFFECT: higher reliability and toughness of the said engine and its lower weight.
2 cl, 2 dwg
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