Air/oil separator apparatus and method

Patent metadata

Field	Value
Publication number	US-12168239-B2
Application number	US-202117643544-A
Country	US
Kind code	B2
Filing date	Dec 9, 2021
Priority date	Dec 10, 2020
Publication date	Dec 17, 2024
Grant date	Dec 17, 2024

Abstract

An air/oil separator is provided. The air/oil separator includes an oil manifold having a first air/oil inlet and a second air/oil inlet; a first separation chamber in communication with the first air/oil inlet; and a second separation chamber separate from the first separation chamber, the second separation chamber in communication with the second air/oil inlet.

First claim

The invention claimed is:

1. An air/oil separator, comprising:
an air manifold having an air outlet and an air manifold centerline axis;
an oil manifold having a first air/oil inlet and a second air/oil inlet, the oil manifold extending circumferentially about the air manifold centerline axis and an entirety of the oil manifold extending radially outward of the air manifold;
a first rotating separation chamber defined by a first body, the first rotating separation chamber having a first rotating separation chamber bottom exiting hole and a first rotating separation chamber oil outlet channel fluidly coupled to the first rotating separation chamber bottom exiting hole, the first rotating separation chamber being in communication with the first air/oil inlet and the air outlet, and the first body being configured to induce a rotation of an air/oil mixture in the first rotating separation chamber to separate air of the air/oil mixture from oil of the air/oil mixture and to guide the air towards the air outlet and the oil towards the first rotating separation chamber bottom exiting hole; and
a second rotating separation chamber defined by a second body, the second rotating separation chamber having a second rotating separation chamber bottom exiting hole and a second rotating separation chamber oil outlet channel fluidly coupled to the second rotating separation chamber bottom exiting hole, the second rotating separation chamber being separate from the first rotating separation chamber and in communication with the second air/oil inlet and the air outlet, and the second body being configured to induce a rotation of the air/oil mixture in the second rotating separation chamber to separate the air of the air/oil mixture from the oil of the air/oil mixture and to guide the air towards the air outlet and the oil towards the second rotating separation chamber bottom exiting hole,
wherein the air manifold centerline axis is parallel to a centerline axis of the first rotating separation chamber bottom exiting hole or the second rotating separation chamber bottom exiting hole, and
wherein the first rotating separation chamber oil outlet channel and the second rotating separation chamber oil outlet channel are separate and are each fluidly coupled between their respective bottom exiting hole and an oil tank.

2. The air/oil separator of claim 1 , wherein the first air/oil inlet is disposed tangentially along a wall of the first rotating separation chamber and configured to receive a first air/oil mixture and induce a circular motion of the first air/oil mixture within the first rotating separation chamber.

3. The air/oil separator of claim 2 , wherein a first oil portion exits the first rotating separation chamber through the first rotating separation chamber bottom exiting hole through the first rotating separation chamber oil outlet channel and to the oil tank.

4. The air/oil separator of claim 3 , wherein a first air portion exits the first rotating separation chamber at a top location and flows to the air outlet of the air manifold.

5. The air/oil separator of claim 1 , wherein the second air/oil inlet is disposed tangentially along a wall of the second rotating separation chamber and configured to receive a second air/oil mixture and induce a circular motion of the second air/oil mixture within the second rotating separation chamber.

6. The air/oil separator of claim 5 , wherein a second oil portion exits the second rotating separation chamber through the second rotating separation chamber bottom exiting hole through the second rotating separation chamber oil outlet channel and to the oil tank.

7. The air/oil separator of claim 6 , wherein a second air portion exits the second rotating separation chamber at a top location and flows to the air outlet of the air manifold.

8. The air/oil separator of claim 1 , further comprising:
a third rotating separation chamber separate from the first rotating separation chamber and the second rotating separation chamber.

9. The air/oil separator of claim 8 , wherein the oil manifold includes a third air/oil inlet, and the third rotating separation chamber is in communication with the third air/oil inlet.

10. A gas turbine engine comprising:
a compressor section configured to compress air flowing therethrough to provide a compressed air flow; and
a combustor configured to combust a mixture fuel and the compressed air flow to generate combustion products;
a turbine section having at least one turbine driven by the combustion products; and
the air/oil separator of claim 1 .

11. The gas turbine engine of claim 10 , further comprising:
an oil circuit coupled to the air/oil separator; and
at least one of a power gear box, a pitch change mechanism for a variable pitch fan, or an electric machine coupled to the oil circuit.

12. An air/oil separator, comprising:
an air manifold having an air outlet and an air manifold centerline axis;
an oil manifold having a first air/oil inlet and a second air/oil inlet, the oil manifold extending circumferentially about the air manifold centerline axis and an entirety of the oil manifold extending radially outward of the air manifold;
a first rotating separation chamber defined by a first body and being in communication with the air outlet and the first air/oil inlet, the first body being configured to induce a rotation of an air/oil mixture in the first rotating separation chamber to separate air of the air/oil mixture from oil of the air/oil mixture and to guide the air towards the air outlet; and
a second rotating separation chamber separate from the first rotating separation chamber, the second rotating separation chamber being defined by a second body_and in communication with the air outlet and the second air/oil inlet, the second body being configured to induce a rotation of the air/oil mixture in the second rotating separation chamber to separate the air of the air/oil mixture from the oil of the air/oil mixture and to guide the air towards the air outlet.

13. The air/oil separator of claim 12 , wherein the first air/oil inlet is disposed tangentially along a wall of the first rotating separation chamber and configured to receive a first air/oil mixture and induce a circular motion of the first air/oil mixture within the first rotating separation chamber.

14. A method of separating oil from air, the method comprising:
providing the air/oil separator of claim 12 ;
directing a first air/oil mixture to the first rotating separation chamber; and
simultaneously directing a second air/oil mixture to the second rotating separation chamber.

15. The method of claim 14 , wherein the first air/oil inlet is disposed tangentially along a wall of the first rotating separation chamber and configured to receive the first air/oil mixture and induce a circular motion of the first air/oil mixture within the first rotating separation chamber, wherein a first oil portion exits the first rotating separation chamber at a bottom location, and wherein a first air portion exits the first rotating separation chamber at a top location.

16. A gas turbine engine comprising:
a compressor section configured to compress air flowing therethrough to provide a compressed air flow; and
a combustor configured to combust a mixture fuel and the compressed air flow to generate combustion products;
a turbine section having at least one turbine driven by the combustion products;
an oil circuit for providing oil to a system of the gas turbine engine; and
the air/oil separator of claim 11 coupled to the oil circuit.

17. The gas turb

Assignees

• Ge Avio Srl

Inventors

• Baraggia Au Yeung Saypen
• Molesini Pietro
• Manzoni Miriam
• De Bellis Fabio

Classifications

• F05D2260/98

  Lubrication · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C7/06 Primary

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title

• B04C5/04

  Tangential inlets · CPC title

• B01D45/16

  generated by the winding course of the gas stream {, the centrifugal forces being generated solely or partly by mechanical means, e.g. fixed swirl vanes} · CPC title