IP Library Granted Patent US 11,058,979
Granted Patent B2
US 11,058,979 · App. 15/875,401 · Granted Jul 13, 2021

Air-oil separator

Inventors: Lanchao Lin (Dayton, OH); Richard Louis Heil (Medway, OH); Jan Zywot (Centerville, OH)
Assignee: GE Aviation Systems LLC
B01D45/16F04B23/02F04B39/16B01D2257/702F01M2013/0427
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Quick Facts
Patent No.
US 11,058,979
App. No.
15/875,401
Granted
Jul 13, 2021
Kind
B2
Abstract

An air-oil separator assembly can include an air-oil mixture inlet, an air outlet, and an oil outlet, a housing defining a cylindrical separating cavity, and an outlet conduit disposed within the separating cavity, wherein, outlet conduit is adapted to receive oil removed by the air-oil separator assembly from a flow containing an air-oil mixture fluid received by the air-oil mixture inlet.

Claims (15)

1. An air-oil separator assembly for a generator comprising:

a first generator compartment having an air-oil mixture fluid at a first pressure;

a second generator compartment separated from the first compartment by a wall and having a second pressure less than the first pressure; and

an air-oil separator disposed within the wall and fluidly connecting the first generator compartment with the second generator compartment, the air-oil separator comprising:

a first housing received by the wall and defining a separating cavity and an axis, the separating cavity fluidly connected with the first generator compartment;

an air outlet conduit disposed within the separating cavity and coaxial with the separating cavity, and fluidly connected with the second generator compartment;

a second dome housing enclosing the separating cavity; and

an oil channel disposed in an inner surface of at least one of the first housing or the second dome housing, the oil channel circumferentially arranged about the inner surface;

wherein the reduced pressure of the second generator compartment draws a flow of the air-oil mixture fluid into the separating cavity, whereby the flow traverses the separating cavity in a first direction parallel to the axis, and whereby the flow is redirected in a second direction by the second dome housing to the air outlet conduit and second generator compartment, the second direction parallel to the axis and opposite to the first direction.

2. The air-oil separator assembly of claim 1 wherein the wall is a generator end cap.

3. The air oil separator assembly of claim 1 wherein the oil channel is normal to the separating cavity, the separating cavity defining a longitudinal axis and the oil channel is circumferentially arranged about a plane normal to the longitudinal axis.

4. The air-oil separator assembly of claim 1 wherein the oil channel is a capillary oil channel.

5. The air-oil separator assembly of claim 1 wherein the housing, separating cavity, and dome housing are adapted to flow the air-oil mixture in a cyclonic fluid flow through the air-oil separator.

6. The air-oil separator assembly of claim 5 wherein the separating cavity defines a cavity wall adapted to flow oil removed by the cyclonic separation.

7. The air-oil separator assembly of claim 5 wherein the oil channel is formed between the first housing and second dome housing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 19, 2018
From: LIN, LANCHAO; HEIL, RICHARD LOUIS; ZYWOT, JAN
To: GE AVIATION SYSTEMS LLC
Reel/Frame 044669/0226 →
Continuity (1)
Related Publication 20190224602A1 · Jul 25, 2019