# US 5,702,574 A · Jig for coating rotor blades

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- Number: US 5,702,574 A
- Document ID: US5702574A
- Status: Granted
- Kind: A
- Application number: 08/505,322
- Filed: 1996-05-03
- Granted: 1997-12-30
- Earliest claimed: 1993-12-21
- Assignees: Praxair S.T. Technology, Inc.
- Inventors: John Foster; Alan Taylor; Martin Patrick Chatterley
- Web page: https://patentgrep.com/patent/US5702574A

## CPC

- F01D 25/285: {Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures}
- C25D 5/02: Electroplating of selected surface areas
- C25D 15/02: Combined electrolytic and electrophoretic processes {with charged materials}
- C25D 17/06: Suspending or supporting devices for articles to be coated
- F01D 11/12: using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- C25D: PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR

## Abstract

A method of and apparatus for producing abrasive tips on compressor or turbine rotor blades by electrolytic or electroless deposition in which the blades are mounted in a hollow jig with the tips of the blades extending through sealed openings in the jig and abrasive tips are formed on the tips. The parts of the blades within the hollow jig are isolated from the electrolyte without the need for wax masking. Preferably the jig is cylindrical with the blades extending radially through at least one circumferential row of apertures. The jig may comprise two end discs and at least one ring in which a circumferential row of apertures is formed. The ring is positioned between the end discs and means are provided for securing the discs and ring together.

## Claims

### Claim 1

A jig for use in the production by electrodeposition of abrasive tips on compressor or turbine rotor blades comprising a hollow, generally cylindrical housing having two end discs and at least one ring therebetween, the discs and the ring defining an interior to receive the majority of each blade, the ring having respective apertures for outer portions of aerofoil parts of the blades to project therethrough, sealing means for sealing the blades as they pass through the respective apertures, and means for securing the discs and the ring together.

### Claim 2 (depends on 1)

The jig of claim 1 in which the respective apertures are arranged in at least one circumfertial row.

### Claim 3 (depends on 1)

The jig of claim 1 in which the sealing means comprises, for each aperture, a block of resilient material having a blade aperture which is adapted to be a close fit around such blade and which is a close fit in the respective aperture in the ring.

### Claim 4 (depends on 3)

The jig of claim 3 in which the respective apertures are notches which are arranged in at least one circumfertial row.

### Claim 5 (depends on 4)

The jig of claim 4 in which there are at least two rings disposed between the end discs.

### Claim 6 (depends on 5)

The jig of claim 5 further including at least one blade supporting unit mounted on an axial support and having carrying means for receiving roots of the blades.