# US 10,870,079 B2 · Air-oil separator with first separator radially outward of matrix separator

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- Number: US 10,870,079 B2
- Document ID: US10870079B2
- Status: Granted
- Kind: B2
- Application number: 15/949,240
- Filed: 2018-04-10
- Published: 2019-10-10
- Granted: 2020-12-22
- Earliest claimed: 2018-04-10
- Assignees: Pratt & Whitney Canada Corp.
- Applicants: Pratt & Whitney Canada Corp.
- Inventors: Sylvain Brouillet; Pierre Gauvin
- Web page: https://patentgrep.com/patent/US10870079B2

## CPC

- B01D 50/20: Combinations of devices covered by groups B01D45/00 and B01D46/00
- B01D 45/14: generated by rotating vanes, discs, drums or brushes
- B01D 46/0031: {with collecting, draining means}
- B01D 46/0056: {with rotational movement}
- B01D 46/64: arranged concentrically or coaxially
- B01D 2267/40: Different types of filters
- B01D 2275/202: Disc-shaped filter elements
- B01D 2275/40: Porous blocks
- F01D 25/18: Lubricating arrangements (of machines or engines in general F01M)
- F01M 13/04: having means for purifying air before leaving crankcase, e.g. removing oil
- F01M 2013/0422: {Separating oil and gas with a centrifuge device}
- F02C 7/06: Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M)
- F02C 7/32: Arrangement, mounting, or driving, of auxiliaries
- F05D 2240/50: Bearings
- F05D 2260/609: Deoiling or demisting
- F05D 2300/514: Porosity
- B01D: SEPARATION (separating solids from solids by wet methods B03B, B03D; by pneumatic jigs or tables B03B; by other dry methods B07; magnetic or electrostatic separation of solid materials from solid materials or fluids, separation by high-voltage electric fields B03C; centrifuges, vortex apparatus B04; presses per se for squeezing-out liquid from liquid-containing material B30B9/02; treatment of water C02F, e.g. softening by ion-exchange C02F1/42; {arrangements of air intake cleaners in gas turbine plants F02C7/05} ; arrangements or mounting of filters in air-conditioning, air-humidification or ventilation F24F13/28)
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F01M: LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- 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)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

There is disclosed a separator having a first separator and a matrix separator. The first separator caters to an air-oil mixture having a first oil concentration and the matrix separator caters to an air-oil mixture having a second oil concentration being less than the first oil concentration. The matrix separator is disposed at least partially concentrically within the first separator. A wall is disposed radially between the first and second separators. A radial passage extends through the wall. An air-oil mixture outlet of the first separator is fluidly connected to an air-oil mixture inlet of the matrix separator via the radial passage. At least one passage extends radially outwardly from the matrix separator across the first separator. The at least one passage fluidly connects the matrix separator to an environment outside the air-oil separator. A method of removing oil from an air-oil mixture is also disclosed.

## Claims

### Claim 1

A gas turbine engine comprising an air-oil separator, the air-oil separator having:
a first separator rotatable about a rotation axis and having an air-oil mixture inlet and an air-oil mixture outlet, the first separator configured to separate an air-oil mixture having a first oil concentration;
a matrix separator having a porous media and configured to separate an air-oil mixture having a second oil concentration less than the first oil concentration, the matrix separator rotatable about the rotation axis, the matrix separator having an air-oil mixture inlet, the matrix separator disposed at least partially concentrically within the first separator and at least partially axially overlapping the first separator;
a wall disposed radially between the first separator and the matrix separator and extending axially relative to the rotation axis, a radial passage extending through the wall, the air-oil mixture outlet of the first separator fluidly connected to the air-oil mixture inlet of the matrix separator via the radial passage; and
at least one passage extending radially outwardly from the matrix separator across the first separator, the at least one passage fluidly connecting the matrix separator to an environment outside the air-oil separator.

### Claim 2 (depends on 1)

The gas turbine engine of claim 1, wherein the first separator and the matrix separator are disposed within a casing, the casing being secured to a shaft of the gas turbine engine, the casing rotating integrally with the first separator and the matrix separator.

### Claim 3 (depends on 2)

The gas turbine engine of claim 2, wherein the first separator has an oil outlet corresponding to apertures defined through an outer circumferential wall of the casing, the oil outlet fluidly connected to both of the at least one passage and the first separator.

### Claim 4 (depends on 1)

The gas turbine engine of claim 1, wherein the at least one passage includes a plurality of passages circumferentially distributed around the rotation axis.

### Claim 5 (depends on 1)

The gas turbine engine of claim 1, wherein the first separator is a bladed separator having blades protruding from a hub, the wall corresponding to the hub, the at least one passage extending within a thickness of one of the blades, between a pressure side and a suction side of the one of the blades.

### Claim 6 (depends on 5)

The gas turbine engine of claim 5, wherein an axial length of the blades of the rotor relative to the rotation axis is less than that of the porous media relative to the rotation axis.

### Claim 7 (depends on 6)

The gas turbine engine of claim 6, wherein a gap extends from the blades to a rear end of the matrix separator, another matrix separator being located within the gap, the other matrix separator configured to separate an air-oil mixture having a third oil concentration being more than the second oil concentration and less than the first oil concentration.

### Claim 8 (depends on 1)

The gas turbine engine of claim 1, wherein the first separator is an outward matrix separator, the air-oil separator further having a bladed separator located upstream of the outward matrix separator, the bladed separator including a rotor having radially extending blades, the rotor configured for rotation about the rotation axis, the bladed separator having an air-oil mixture outlet fluidly connected to the air-oil mixture inlet of the first separator.

### Claim 9 (depends on 1)

The gas turbine engine of claim 1, wherein the porous media is a sponge.

### Claim 10

A gas turbine engine having a shaft, the gas turbine engine comprising an air-oil separator secured to the shaft for rotation about a rotation axis, the air-oil separator having: a first separator rotatable about the rotation axis and configured to separate an air-oil mixture having a first oil concentration; and a matrix separator rotatable about the rotation axis and configured to separate an air-oil mixture having a second oil concentration less than the first oil concentration, the matrix separator having a porous media, the matrix separator disposed at least partially concentrically within the first separator, one of the first separator and the matrix separator disposed around the other of the first separator and the matrix separator, the air-oil separator defining a flow path extending from an air-oil mixture inlet of the first separator to an air outlet of the air-oil separator, the flow path extending in a radial direction relative to the rotation axis when passing from the first separator to the matrix separator through at least one radial passage fluidly connecting the first separator to the matrix separator, the radial passage extending through a wall disposed radially between the first and matrix separators, at least one passage extending radially outwardly from the matrix separator across the first separator, the at least one passage fluidly connecting the matrix separator to an environment outside the air-oil separator.

### Claim 11 (depends on 10)

The gas turbine engine of claim 10, wherein the at least one passage includes a plurality of passages circumferentially distributed around the rotation axis.

### Claim 12 (depends on 10)

The gas turbine engine of claim 10, wherein the first separator is a bladed separator having blades protruding from a hub, the wall corresponding to the hub, the at least one passage extending within a thickness of one of the blades, between a pressure side and a suction side of the one of the blades.

### Claim 13 (depends on 12)

The gas turbine engine of claim 12, wherein an axial length of the blades of the rotor relative to the rotation axis is less than that of the porous media relative to the rotation axis.

### Claim 14 (depends on 13)

The gas turbine engine of claim 13, wherein a gap extends from the blades to a rear end of the matrix separator, another matrix separator being located within the gap, the other matrix separator configured to separate an air-oil mixture having a third oil concentration being more than the second oil concentration and less than the first oil concentration.

### Claim 15 (depends on 10)

The gas turbine engine of claim 10, wherein the first separator is an outward matrix separator, the air-oil separator further having a bladed separator located upstream of the outward matrix separator, the bladed separator including a rotor having radially extending blades, the rotor configured for rotation about the rotation axis, the bladed separator having an air-oil mixture outlet fluidly connected to an air-oil mixture inlet of the first separator.

### Claim 16 (depends on 10)

The gas turbine engine of claim 10, wherein the porous media is a sponge.

### Claim 17 (depends on 10)

The gas turbine engine of claim 10, wherein the first separator has an oil outlet corresponding to apertures defined through an outer circumferential wall of a casing, the first and matrix separators located within the casing, the casing being secured to the shaft of the gas turbine engine, the casing rotating integrally with the first and matrix separators, the oil outlet fluidly connected to both of the at least one passage and the first separator.