IP Library Granted Patent US 7,625,435
Granted Patent B2
US 7,625,435 · App. 11/534,256 · Granted Dec 1, 2009

Electrostatic air/oil separator for aircraft engine

Assignee: Pratt & Whitney Canada Corp.
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Quick Facts
Patent No.
US 7,625,435
App. No.
11/534,256
Granted
Dec 1, 2009
Kind
B2
Abstract

An air/oil separator for use in a gas turbine engine includes a labyrinth path having an air/oil inlet, air outlet and oil outlet, a device for creating an electrical field within the labyrinth path and a device for creating a suction action at the oil outlet to draw liquid oil from the labyrinth path and for delivering the liquid oil under pressure to a pressurized source of oil in the engine.

Claims (18)

1. An air/oil separator for use in a gas turbine engine comprising

a labyrinth path having an air/oil inlet, air outlet and oil outlet, and including first and second sets of electrically conductive members, electrically insulated one set from another;

a source of DC voltage electrically connected to the respective first and second sets of electrically conductive members for creating an electrical field within the labyrinth path; and

a jet pump for creating a suction action at the oil outlet to draw liquid oil from the labyrinth path and for delivering the liquid oil under pressure to a pressurised source of oil in the engine.

2. The air/oil separator as defined in claim 1 wherein the electrically conductive members of the labyrinth path comprise first and second sets of electrically conductive cylinders alternately positioned in a co-axial relationship.

3. An air/oil separator for use in a gas turbine engine comprising:

a casing including an air/oil inlet, air outlet and oil outlet;

first and second sets of electrically conductive partitioning members alternately positioned within the casing to define a fluid passage through the casing; the first set of electrically conductive partitioning members being grounded and the second set of electrically conductive partitioning members being electrically charged; and

a jet pump connected to the oil outlet to draw liquid oil from the passage and deliver same to an oil tank of the engine.

4. The air/oil separator as defined in claim 3 wherein the first and second sets of partitioning members comprise first and second sets of electrically conductive interleaved plates.

5. The air/oil separator as defined in claim 3 wherein the casing is electrically conductive and is grounded.

6. The air/oil separator as defined in claim 5 wherein the first set of members are attached to the casing and the second set of the members are supported within but insulated from the casing.

7. The air/oil separator as defined in claim 6 wherein the air/oil inlet is located in a middle portion at a side wall of the casing, the air outlet is located at a top wall of the casing and the oil outlet is located at a bottom wall of the casing.

8. The air/oil separator as defined in claim 3 wherein the first and second sets of partitioning members comprise first and second sets of electrically conductive cylinders alternately positioned in a co-axial relationship.

9. The air/oil separator as defined in claim 8 wherein the casing is electrically conductive and cylindrical.

10. The air/oil separator as defined in claim 9 wherein the cylinders are positioned co-axially within the cylindrical casing, the first set of cylinders being directly supported on a first end of the casing and the second set of the cylinders being supported on but electrically insulated from a second end of the casing.

11. The air/oil separator as defined in claim 8 wherein the air/oil inlet is adapted to direct a fluid flow directly into an inside of an innermost cylinder.

12. The air/oil separator as defined in claim 8 wherein the casing further accommodates an elongate, electrically conductive member positioned co-axially with the cylinders, the elongate, electrically conductive member having an electric polarity opposite to an electric polarity of an immediately surrounding cylinder.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 22, 2006
From: DOOLEY, KEVIN ALLAN
To: PRATT & WHITNEY CANADA CORP.
Reel/Frame 018290/0026 →
Continuity (1)
Related Publication 20080072755A1 · Mar 27, 2008