# US 10,119,420 B2 · Seal

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- Number: US 10,119,420 B2
- Document ID: US10119420B2
- Status: Granted
- Kind: B2
- Application number: 15/171,577
- Filed: 2016-06-02
- Published: 2017-01-05
- Granted: 2018-11-06
- Earliest claimed: 2015-06-30
- Assignees: ROLLS-ROYCE plc
- Applicants: ROLLS-ROYCE plc
- Inventors: David P Scothern
- Web page: https://patentgrep.com/patent/US10119420B2

## CPC

- F01D 25/183: {Sealing means}
- F01D 11/003: {by packing rings; Mechanical seals}
- F01D 11/04: using sealing fluid, e.g. steam
- F01D 11/10: using sealing fluid, e.g. steam
- F02C 7/28: Arrangement of seals
- F16J 15/40: by means of fluid
- F16J 15/42: kept in sealing position by centrifugal force
- F05D 2220/32: in gas turbines
- F05D 2240/55: Seals
- F05D 2260/98: Lubrication
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F16J: PISTONS {(specially adapted for dampers F16F9/32)}; CYLINDERS; SEALINGS
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A hydraulic seal arrangement including first and second rotatable components, the first defining a first annular trough defined by radially inwardly extending first and second walls, the second component defining a radially outwardly extending web between the walls. The first component includes a second trough defined by the second wall and a third wall axially spaced from the second, the second trough defining an open radially inner end defined by a radially inner end of the second wall such that the first and second annular troughs fluidly communicate around the circumference of the first component via the inner end of the second wall. At a first circumferential position, the second wall of the first component defines a second trough oil inlet providing further fluid communication between the first and second troughs and at a second circumferential position, the third wall of the first component defines a second trough oil outlet.

## Claims

### Claim 1

A hydraulic seal arrangement for a rotating machine comprising:
first and second relatively rotatable components, the first component defining a first annular trough defined by radially inwardly extending axially spaced first and second walls, the second component defining a radially outwardly extending web extending between the radially inwardly extending walls of the first component; the first component further comprising:
a second trough defined by the radially inwardly extending second wall and a radially inwardly extending third wall axially spaced from the second radially extending wall, the second trough defining an open radially inner end defined by a radially inner end of the second radially extending wall such that the first and second annular troughs fluidly communicate around substantially the whole circumference of the first component via the radially inner end of the second radially extending wall; wherein
at a first circumferential position, the second radially inwardly extending wall of the first component defines a second trough oil inlet providing fluid communication between the first and second annular troughs; and
at a second circumferential position, the third radially extending wall of the first component defines a second trough oil outlet.

### Claim 2 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the first and second radially extending walls of the first component are axially spaced by a first axially extending wall provided at a radially outer end of the first and second radially extending walls.

### Claim 3 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the second and third walls are axially spaced by a second axially extending wall provided at a radially outer end of the second and third radially extending walls.

### Claim 4 (depends on 3)

A hydraulic seal arrangement as claimed in claim 3, in which the second trough defines a first volume at the first circumferential position, and defines a second volume at the second circumferential position.

### Claim 5 (depends on 4)

A hydraulic seal arrangement as claimed in claim 4, in which the second volume is equal to or greater than the first volume.

### Claim 6 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the second trough oil inlet and second trough oil outlet are located at the same radial position.

### Claim 7 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the second trough oil inlet is located radially inwardly from a radially outer end of the radially outwardly extending web of the second component.

### Claim 8 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the second and third walls of the first component are axially spaced to a greater extent at the second circumferential position than at the first circumferential position.

### Claim 9 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which at the first circumferential position, the second axially extending wall is located at a first radial position, and at the second circumferential position, the second axially extending wall is located at a second radial position radially outwardly of the first radial position.

### Claim 10 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the second trough oil inlet and oil outlet are circumferentially spaced by 90° from one another.

### Claim 11 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which a pair of second trough oil inlets and a pair of second trough oil outlets are provided at diametrically opposite circumferential positions.

### Claim 12 (depends on 1)

A hydraulic seal arrangement as claimed in claim 1, in which the rotating machine is a gas turbine engine.

### Claim 13 (depends on 12)

A hydraulic seal arrangement as claimed in claim 12, in which a first shaft of the gas turbine engine comprises or is coupled to the first component, and a second shaft of the gas turbine engine comprises or is coupled to the second component.

### Claim 14 (depends on 1)

A hydraulic seal as claimed in claim 1, in which the second trough oil inlet comprises a first aperture provided in the second radially extending wall.

### Claim 15 (depends on 1)

A hydraulic seal as claimed in claim 1, in which the second trough oil outlet comprises a second aperture provided in the third radially extending wall.

### Claim 16 (depends on 1)

A gas turbine engine comprising a hydraulic seal arrangement in accordance with claim 1.
