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High-pressure turbine for turbomachine, associated guide vane sector and aircraft engine
High-pressure turbine for turbomachine, associated guide vane sector and aircraft engine
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机译:用于涡轮机的高压涡轮机,相关的导向叶片部分和飞机发动机
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摘要
An assembling of a guide vane assembly of a turbomachine turbine, formed by an annular row of stationary flow-stabilizing vanes. An outer edge of the guide vane assembly is axially bearing on a line of an external casing of the turbine and an inner edge of the guide vane assembly is in axial sliding connection with the line of the internal casing of the turbine, the axial sliding connection allowing the inner edge to be free along the motor axis with the axial stop being achieved by the axial bearing of the outer edge of the vane.
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