High pressure turbine rotor two-piece blade retainer

Claim 1

In combination with a turbine rotor disc and at least one turbine blade mounted in a peripheral rim of said disc such that a cavity is formed between said blade and said disc and opens at least at one side thereof, a blade retainer, comprising: (a) a first blade loading piece including in serially interconnected relationship: (i) a first element engaging said blade, (ii) a second element abutting a first shoulder on said disc rim and anchoring said blade loading piece against centrifugal forces generated during rotor disc rotation, and (iii) a third element for attachment of said blade loading piece to said disc rim so as to impose a vibration-dampening load force on said blade via said first element; (b) a second cavity sealing piece separate from said first piece and including in serially interconnected relationship: (i) a first member closing said cavity at least at said one side thereof and for attachment of said cavity sealing piece to said rim, and (ii) a second member anchoring said cavity sealing piece against centrifugal forces generated during rotor disc rotation; (c) said third element of said first piece and said first member of said second piece being disposed in an overlapped relationship for attachment to said disc rim, said first member of said second piece being disposed adjacent said disc rim and said third element of said first piece being spaced from said disc rim; and (d) common fastening means connecting both said first member of said second piece and third element of said first piece together and attaching the same in said overlapped relationship to said disc rim; (e) said third element of said first piece further having defined therein a first set of spaced apart holes through which said first piece may be attached to said disc rim by said common fastening means, and stress concentration reducing means for relieving stress concentration in the region of said holes.