Apparatus and method for securing a rotor blade in a rotor...

Details Apparatus and method for securing a rotor blade in a rotor... Apparatus and method for securing a rotor blade in a rotor...

2007-12-11

2007-12-11

Look, Edward K. (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Specific working member mount

Blade received by continuous circumferential channel

C416S218000, C416S22000A, C416S234000

Reexamination Certificate

active

11413753

ABSTRACT:
A rotor of a turbine-type machine, in particular a gas turbine rotor, is disclosed. The rotor has a rotor base body, where the rotor base body has a groove extending in the circumferential direction of the rotor base body, and has multiple rotor blades, or rotor blade segments, or an integrally bladed, circumferentially closed rotor blade ring. The rotor blades, or rotor blade segments, or rotor blade ring are/is anchored in the groove extending in the circumferential direction of the rotor base body by a blade base or ring base. The groove has a profiled groove wall leg on only one side, with the blade base of the rotor blades or the rotor blade segments, or ring base of the rotor blade ring, being in contact with the profiled groove wall leg with a correspondingly profiled supporting flank.

REFERENCES:
patent: 747523 (1903-12-01), Wilkinson
patent: 1345678 (1920-07-01), Kasley
patent: 1347327 (1920-07-01), Dickinson
patent: 1366592 (1921-01-01), Pentheny et al.
patent: 1466324 (1923-08-01), Wilkinson
patent: 1640451 (1927-08-01), Junggren
patent: 5330324 (1994-07-01), Agram et al.

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