Turboengine, and vane carrier unit for turboengine
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United States of America Patent
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Jan 5, 2021
Grant Date -
Oct 12, 2017
app pub date -
Apr 10, 2017
filing date -
Apr 8, 2016
priority date (Note) -
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status (Latency Note)
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Abstract
A turboengine as disclosed includes an outer wall structure and an inner wall structure, wherein the inner wall structure is provided at a radially inner position with respect to the outer wall structure, and each of the wall structures has a surface, the surfaces being arranged facing each other in the radial direction. At least one guide vane member includes at least one airfoil, a radially inner end and a radially outer end. The inner wall structure and the outer wall structure are jointly provided as a vane carrier unit, wherein the inner wall structure and the outer wall structure are fixedly connected to each other by at least one bridging member extending between the inner wall structure and the outer wall structure.
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