Radial turbine nozzle and method for assembling the same
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United States of America Patent
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Jul 16, 2024
Grant Date -
Jan 18, 2024
app pub date -
Jul 10, 2023
filing date -
Jul 13, 2022
priority date (Note) -
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Abstract
In a radial turbine nozzle and its assembling method, a first flange member of a first divided annular portion is inserted into a first outer side groove of a first ring. A second flange member of a second divided annular portion is inserted into a second outer side groove of a second ring. A plurality of segments are connected together in a circumferential direction, by overlapping first divided surfaces of two of the segments that are adjacent in a circumferential direction of a radial turbine, and overlapping second divided surfaces of the two of the segments.
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