Method and tooling for machining the annulus of gas-turbine rotor provided with integrally formed-on blades
AssigneeRolls-Royce Deutschland Ltd & Co KG
InventorsJan Hollmann, Gregor Kappmeyer
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Abstract
With an integrally bladed rotor, material removal is performed from the annulus (5) on a wide, even machining path (8) using the front-side cutting area of an essentially cylindrical cutter head (7). The tool shank (9) is shaped and dimensioned such that it does not collide with the opposite lateral surfaces of the differently curved and twisted blades (4). This type of machining enables an essentially even, smooth annulus surface to be obtained with a reduced number of overlapping machining paths (8). The time required for machining the annulus and the tool wear are reduced. With an annulus machined in accordance with the present invention, the rotor will satisfy high requirements on aerodynamics.
Claims6
A method for machining an annulus of a gas turbine rotor having integrally formed-on blades extending from a circular periphery of the annulus, comprising:
- performing wide, even material removal on a respective machining path between a pair of adjacent ones of the blades using a planar front-side end cutting-edge area of a cutter head by moving the cutter head along a path that is parallel to the circular periphery surface of the annulus, the cutter head also including curved cutting edges on a toroidal lateral cutting area for machining a transition area between the blades and the annulus;
- and
- avoiding contacting opposite inner surfaces of the adjacent blades with a cutting tool supporting the cutter head.
Dependencies are inferred from the claim text.