Machining system for turbomachine dovetail
Various embodiments include a system for machining a hole in a turbine blade. The system can include: a mount for engaging a first side of a turbine rotor, the mount including: a drill plate for coupling with the first side of the turbine rotor, the drill plate having: a body; a feed opening on a first side of the body; a passage extending from the feed opening through the body; and a second opening on a second side of the body, the second opening coupled with the passage and positioned to align with the pre-formed hole in the turbine rotor; an alignment bushing for engaging the pre-formed hole in the rotor at a second side of the rotor; and a cutting device for extending through the body and alignment bushing, the cutting device for machining the hole in the blade, the cutting device aligned along a chamfer axis relative to a primary axis of the turbine rotor.
1. A method comprising:
mounting a machining system on a turbine rotor, the turbine rotor including a pre-formed hole, the machining system having:
a mount for engaging a first side of the turbine rotor, the mount including:
a drill plate for coupling with the first side of the turbine rotor, the drill plate having: a body; a feed opening on a first side of the body; a passage extending from the feed opening through the body; and a second opening on a second side of the body, the second opening coupled with the passage and positioned to align with the pre-formed hole in the turbine rotor;
an alignment bushing for engaging an interior surface of the pre-formed hole in the turbine rotor at a second side of the turbine rotor, opposite the first side of the turbine rotor; and
a cutting device for extending through the body and the alignment bushing, the cutting device aligned along a chamfer axis relative to a primary axis of the turbine rotor; and
actuating the cutting device to machine a hole in at least one turbine blade of the turbine rotor, wherein actuating the cutting device includes machining the hole in the at least one turbine blade to align the at least one hole with the pre-formed hole in the turbine rotor, wherein the mount and the alignment bushing are configured to counter a reaction load from the cutting device during the machining of the hole in the at least one turbine blade.
2. The method of claim 1 , wherein the machining system further includes a feed bushing, the mounting further including inserting the feed bushing in the feed opening in the drill plate.
3. The method of claim 2 , wherein the cutting device extends through the feed bushing during the actuating of the cutting device.
4. The method of claim 1 , wherein the mounting includes aligning the cutting device along the primary axis of the feed opening and the second opening.
5. The method of claim 1 , wherein the alignment bushing is sized to line the pre-formed hole in the turbine rotor at the second side of the turbine rotor, the mounting including inserting the alignment bushing in the pre-formed hole and placing the cutting device inside the alignment bushing prior to actuating the cutting device.
6. The method of claim 1 , wherein the cutting device includes at least one of a power reaming device, an electrical discharge machining (EDM) rod or a laser device.
7. The method of claim 1 , further comprising an intervening alignment process, wherein the intervening alignment process includes placing at least one alignment pin proximate the turbine rotor to align the machining system.
8. The method of claim 1 , wherein the mount and the alignment bushing support a portion of a weight of the cutting device during the actuating of the cutting device.
9. A method comprising:
mounting a machining system on a turbine rotor, the turbine rotor including a pre-formed hole, the machining system having:
a mount for engaging a first side of the turbine rotor, the mount including:
a drill plate for coupling with the first side of the turbine rotor, the drill plate having: a body; a feed opening on a first side of the body; a passage extending from the feed opening through the body; and a second opening on a second side of the body, the second opening coupled with the passage and positioned to align with the pre-formed hole in the turbine rotor;
an alignment bushing for engaging an interior surface of the pre-formed hole in the turbine rotor at a second side of the turbine rotor, opposite the first side of the turbine rotor; and
a cutting device for extending through the body and the alignment bushing, the cutting device aligned along a chamfer axis relative to a primary axis of the turbine rotor; and
actuating the cutting device to machine a hole in the at least one turbine blade of the turbine rotor, wherein the mounting of the machining system and the actuating of the cutting device are performed sequentially without an intervening alignment process.
10. The method of claim 9 , wherein the drill plate includes at least one degree of freedom, and the mount further includes a corresponding locking mechanism through which an orientation of the at least one alignment pin is transferred to at least one degree of freedom of the drill plate and maintained after removing of the alignment pin.
11. The method of claim 9 , wherein the alignment bushing is sized to line the pre-formed hole in the turbine rotor at the second side of the turbine rotor, the mounting including inserting the alignment bushing in the pre-formed hole and placing the cutting device inside the alignment bushing prior to actuating the cutting device.