IP Library Granted Patent US 7,690,184
Granted Patent B2
US 7,690,184 · App. 11/774,336 · Granted Apr 6, 2010

Method for treating oil waste in a gas turbine engine

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Quick Facts
Patent No.
US 7,690,184
App. No.
11/774,336
Granted
Apr 6, 2010
Kind
B2
Abstract

A method for treating an airflow, laden with oil, flowing in a tube communicating with a rolling bearing enclosure of a gas turbine engine, wherein the airflow is made to travel into a coking box associated with a heating mechanism, in which the air is heated to a sufficient temperature to coke the oil particles contained in the airflow. Preferably, the solid residues produced by the coking are collected in the coking box.

Claims (11)

1. A method for treating an airflow, laden with oil, flowing in a tube communicating with a rolling bearing enclosure of a gas turbine engine, said method comprising:

inputting said airflow into a coking box;

forcing said airflow inside said coking box by transverse plates inside said coking box so as to follow a path alternatively radially outward and radially inward;

heating the airflow inside the coking box to a sufficient temperature so as to coke the oil contained in the airflow such that the oil of the airflow sustains a thermal oxidation transformation inside said coking box and is transformed partly into vapor and partly into a solid residue.

2. The method as claimed in claim 1 , further comprising collecting in the coking box the solid residue produced by the coking.

3. The method as claimed in claim 1 , wherein said coking box is attached to said tube so that the airflow travels from the tube into the box.

4. The method as claimed in claim 3 for treating said airflow in a gas turbine engine comprising an exhaust cone downstream of a turbine, wherein the coking box is placed in said exhaust cone so that said coking box is heated by the gases in the exhaust cone.

5. The method as claimed in claim 1 , wherein the airflow is heated to a sufficient temperature to pyrolize the solid residue thereby eliminating said solid residue from said coking box.

6. The method as claimed in claim 5 , wherein the airflow is heated by taking hot gases immediately downstream of a turbine.

7. The method as claimed in claim 1 , wherein said coking box has a cylindrical casing with a longitudinal axis, and wherein said method comprises positioning said cylindrical casing such that said longitudinal axis of said cylindrical casing is aligned with a longitudinal axis of said gas turbine engine.

8. The method as claimed in claim 1 , further comprising centrifuging said oil through a grid inside said coking box and collecting said oil into a space between said grid and a casing of said coking box.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 6, 2007
From: GAUTHIER, GERARD PHILIPPE; MOURLAN, JEAN-PIERRE
To: SNECMA
Reel/Frame 019524/0930 →