# US 5,344,162 A · Sealing ring for gas turbine engines

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- Number: US 5,344,162 A
- Document ID: US5344162A
- Status: Granted
- Kind: A
- Application number: 08/007,962
- Filed: 1993-01-22
- Granted: 1994-09-06
- Earliest claimed: 1992-02-29
- Assignees: ROLLS-ROYCE plc
- Inventors: John D. Kernon; Mark J. Knight
- Web page: https://patentgrep.com/patent/US5344162A

## CPC

- F16J 9/14: Joint-closures
- F16J 15/164: {the sealing action depending on movements; pressure difference, temperature or presence of leaking fluid}
- F16J 15/441: {with floating ring}
- F16J: PISTONS {(specially adapted for dampers F16F9/32)}; CYLINDERS; SEALINGS

## Abstract

A sealing ring for controlling gas leakage through the annular space between two rotating concentric members; for example engine shafts. The sealing ring 20 has a generally trapezoidal cross section and an overlapping scarf joint. The sealing ring improves sealing by providing continuous lines of contact at edges between inner and outer coaxial shaft members.

## Claims

### Claim 1

A rotor assembly comprising a first rotatable member having a surface with a groove formed therein, a second rotatable member concentric with the first member and spaced apart therefrom to define an annular gap therebetween, and an expandable sealing ring located in the groove for sealing the annular gap, the sealing ring comprising:
a first pair of adjoining surfaces defining a first edge, said first edge being the radially outermost part of the sealing ring, and a second pair of adjoining surfaces defining a second edge diagonally opposite and spaced a predetermined distance from the first edge, and
an expandable scarf joint connecting circumferential ends of said sealing ring, wherein said predetermined distance is defined to permit, via the centrifugal force generated when the rotor is rotated at high speed, the first edge to sealingly contact the second member, the second edge to sealingly contact the groove, and one of the first pair of adjoining surfaces to contact the groove, wherein the plane of the scarf joint lies between the first and second edges of the ring so that continuous line seal contacts are maintained at both the first and second edges of the ring.

### Claim 2 (depends on 1)

A sealing ring as claimed in claim 1, wherein the first edge is axially disposed towards a high pressure region and the second edge is axially disposed towards a low pressure region.

### Claim 3 (depends on 1)

A sealing ring as claimed in claim 1, wherein the ring is inwardly sprung in the groove.

### Claim 4 (depends on 1)

A sealing ring as claimed in claim 1, wherein an initial axial clearance exists between the ring and the groove.

### Claim 5 (depends on 1)

A sealing ring as claimed in claim 1, wherein one of the second pair of adjoining surfaces defines a chamfer.