TURBINE BLISK AND METHOD OF MANUFACTURING THEREOF
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United States of America Patent
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May 2, 2019
app pub date -
May 7, 2018
filing date -
May 7, 2018
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Abstract
A turbine blisk is provided. The turbine blisk includes an inner rim, a plurality of adjacent rotor blades extending radially outward from said inner rim, a shroud segment integrally coupled to each of the plurality of adjacent rotor blades, thereby forming a plurality of adjacent shroud segments, and a gap defined between each of the adjacent shroud segments. The gap has a geometry that facilitates interlocking the plurality of adjacent shroud segments when a torsional force is applied to the plurality of adjacent rotor blades.
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