Turbo Machine Patents (Class 416/210A)
  • Patent number: 5197857
    Abstract: A rotor assembly for supporting rotor blades includes a plurality of axially adjoining discrete disks each having a rim, web, and hub. The rims include axial dovetail grooves for collectively supporting a respective blade dovetail therein. Each of the disks includes at least one axially extending annular arm joined integrally with the disk and fixedly joined to an adjacent one of the arms. The disks are fixedly joined together solely by the blade dovetails in the rim dovetail grooves and by the arms so that upon a crack failure of one of the disks, centrifugal load from the failed disk is transferred to an adjacent disk.
    Type: Grant
    Filed: June 6, 1991
    Date of Patent: March 30, 1993
    Assignee: General Electric Company
    Inventors: Christopher C. Glynn, Martin C. Hemsworth