1. The fastening part of the turbine nozzle structure comprising a plurality of nozzle segments of the turbine, each of which contains a plurality of stator blades arranged annularly around the axis of the jet engine and secured between the turbine housing and the jet engine nacelle, wherein an arcuate external bandage is provided in the nozzle segment of the turbine, connecting to each other on the other, each of the distal ends of the stator blades on the side opposite the axis; a hook is formed on the outer band in the nozzle segment of the turbine odeystvuyuschy with a support groove of the nozzle formed in the turbine casing, a recessed portion integral with the anti-rotation lug fixed to the turbine casing, and a protruding portion protruding to the rear of a jet engine in accordance with a recess depressed portion on the rear side of said recessed portion; moreover, the nozzle segment of the turbine interacts with the hook of the outer brace with the support groove of the nozzle of the turbine housing at the back of the jet engine, and also combines the deepened portion of the outer brace with the anti-rotation tab on the back of the jet engine and combines the counter-rotation gap formed on the nacelle with the protruding section formed on the rear side of the recessed section behind the jet engine, whereby the nozzle segment of the turbine is fixed between the turbine housing and the nacelle. 2. A turbine in which the fixing part of the turbine nozzle structure according to claim 1 is used for the fixing part of the turbine nozzle structure, which is part of the turbine in a jet engine.
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