| 摘要 |
<p>A turbine disk has an at least partially radially-extending first portion 40. An at least partially axially-extending circumferential flange 50 has a root 56 connecting the flange 50 to the first portion 40. The flange 50 extends to a rim 58 and has a plurality of pairs of first and second weight-mounting fastener apertures 80A,82A,80B,82B. A plurality of first recesses 84 are provided in the rim 58, each position between an associated first and second aperture 80a,82A of an associated one of the aperture pairs. A plurality of second recesses 86 are provided in the rim 58 each positioned between an adjacent two of the pairs 82A,80B. Also disclosed is a method for remanufacturing existing turbine disks.</p> |
