INSERT ASSEMBLY, AIRFOIL, GAS TURBINE, AND AIRFOIL MANUFACTURING METHOD

An insert assembly (79) includes an insert (80), a reinforcing member (85), and a retaining member (90). The insert (80) is fixed to an end of an airfoil body (51) on one side in a radial direction. The reinforcing member (85) is disposed adjacent to an end of the insert (80) on the other side in th...

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Bibliographische Detailangaben
Hauptverfasser: HADA, Satoshi, TSUKAGOSHI, Keizo, MATSUO, Saki, WAKI, Kunihiko, OKAJIMA, Yoshifumi
Format: Patent
Sprache:eng
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Zusammenfassung:An insert assembly (79) includes an insert (80), a reinforcing member (85), and a retaining member (90). The insert (80) is fixed to an end of an airfoil body (51) on one side in a radial direction. The reinforcing member (85) is disposed adjacent to an end of the insert (80) on the other side in the radial direction and enhances the rigidity of the insert (80). The retaining member (90) is fixed to an end of the airfoil body (51) on the other side in the radial direction, and allows the insert (80) to be positioned relative to the airfoil body (51) in a direction orthogonal to the radial direction.