IP Library Granted Patent US 8,051,952
Granted Patent B2
US 8,051,952 · App. 12/359,558 · Granted Nov 8, 2011

Deoiling device and turbomachine comprising this device

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Quick Facts
Patent No.
US 8,051,952
App. No.
12/359,558
Granted
Nov 8, 2011
Kind
B2
Abstract

The invention relates to a deoiling device. It comprises a tube ( 46 ), a first bearing ( 16 ) and a second bearing ( 18 ), the first and second bearings being placed in an oil chamber ( 20 ) in which an oil fog is maintained by rotation of the bearings. A deoiler ( 30 ) is provided in one wall of the oil chamber. The deoiler centrifuges oil in suspension in air and allows a deoiled air flow to pass inside the tube. The tube ( 46 ) comprises a closing cap ( 48 ) fitted with one or several outlet orifices ( 50 ) in its upper part designed to evacuate air, and an oil drain orifice ( 52 ) in its lower part.

Claims (6)

1. Deoiling device comprising a tube ( 46 ), a first bearing ( 16 ) and a second bearing ( 18 ), the first and second bearings ( 16 , 18 ) being placed in an oil chamber ( 20 ) in which an oil fog is maintained by rotation of the bearings, a deoiler ( 30 ) being provided in one wall of the oil chamber, the deoiler centrifuging oil in suspension in air and allowing a deoiled air flow to pass inside the tube ( 46 ), characterised in that the tube ( 46 ) comprises a closing cap ( 48 ) fitted with one or several outlet orifices ( 50 ) in its upper part to evacuate air and an oil drain orifice ( 52 ) in its lower part.

2. Deoiling device according to claim 1 , characterised in that the tube is composed of a low pressure shaft ( 44 ) extended by a hollow shaft ( 46 ) that fits onto the low pressure shaft.

3. Deoiling device according to claim 1 , characterised in that the tube is composed of a central ventilation tube ( 32 ).

4. Deoiling device according to any one of claims 1 to 3 , characterised in that the oil drain orifice is connected through a pipe ( 55 ) to an oil recovery reservoir ( 56 ).

5. Double flow turbomachine comprising a primary flow and a secondary flow and comprising a deoiling device according to one of claims 1 to 3 , characterised in that the air orifices ( 50 ) are extended by ducts ( 54 ) that bring air into the primary flow of the turbomachine.

6. Turbomachine comprising a plug and comprising a deoiling device according to one of claims 1 to 3 , characterised in that the outlet orifices ( 50 ) provided in the cap ( 48 ) open up directly in the plug.

Assignments (2)
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 →