Oil discharge device and turbomachine comprising such a device

Patent metadata

Field	Value
Publication number	US-9897004-B2
Application number	US-201113988960-A
Country	US
Kind code	B2
Filing date	Nov 25, 2011
Priority date	Nov 26, 2010
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A device for discharging oil from an oil chamber located in a downstream part of a gas turbine engine, the device including: a mechanism discharging at least part of the oil contained in the chamber to exterior of the engine; and a drive mechanism for driving the oil, which allows passage of an air flow that assists in driving the discharge of the oil to the exterior of the engine. The drive mechanism includes: a ventilation port in the downstream part of the engine, such that the oil passes through the ventilation port; and a guide element arranged such that, after the oil has passed through the ventilation port, the oil is directed towards a downstream bleed area of the low-pressure turbine. A turbomachine can include such an oil discharge device.

First claim

The invention claimed is:

1. A turbomachine comprising an oil discharge device situated in a downstream part of the turbomachine, the oil discharge device including:
an oil discharge system configured to allow at least some of the oil contained in the oil chamber to be discharged to outside the turbomachine when a level in the oil chamber exceeds a threshold level; and
an oil entrainment device configured to allow therethrough a stream of air with a flow which contributes to driving the discharged oil to outside the turbomachine,
wherein the oil entrainment device comprises:
a vent opening made in the downstream part of the turbomachine so that the discharged oil passes through the vent opening, and
a guide element arranged so that the discharged oil, having passed through the vent opening, is directed toward a downstream bleed zone of a low-pressure turbine, the vent opening opening out to the downstream bleed zone, and the downstream bleed zone being situated adjacent to and downstream of a final disk of the low-pressure turbine to avoid oil being present upstream of the final disk of the low-pressure turbine,

wherein the downstream part comprises a stationary downstream stator element and a rotatable low-pressure turbine element respectively connected to one another,
wherein the downstream bleed zone is situated upstream of an extremity of the stationary downstream stator element that is located on a side of the downstream bleed zone,
wherein the oil discharge system comprises a configuring of the stationary downstream stator element and the rotatable low-pressure turbine element to form a first zone of sealing between the stationary downstream stator element and the rotatable low-pressure turbine element so that the oil is discharged toward the rotatable low-pressure turbine element,
wherein, when the level in the oil chamber does not exceed the threshold level, the stream of air passes through the vent opening into the downstream bleed zone so as to generate an overpressure in the downstream bleed zone, and
wherein the vent opening is defined by the stationary downstream stator element, an axis of the vent opening extending in a radial direction perpendicular to a longitudinal axis of the turbomachine.

2. The turbomachine as claimed in claim 1 , wherein the oil is discharged to outside the turbomachine under an effect of gravity and a centrifugal effect of the spinning of the oil on stator and rotor walls respectively.

3. A device for discharging oil from an oil chamber situated in a downstream part of a gas turbine engine, the device comprising:
an oil discharge system configured to allow at least some of the oil contained in the oil chamber to be discharged to outside the gas turbine engine when a level in the oil chamber exceeds a threshold level; and
an oil entrainment device configured to allow therethrough a stream of air with a flow which contributes to driving the discharged oil to outside the gas turbine engine,
wherein the oil entrainment device comprises:
a vent opening made in the downstream part of the gas turbine engine so that the discharged oil passes through the vent opening, and
a guide element arranged so that the discharged oil, having passed through the vent opening, is directed toward a downstream bleed zone of a low-pressure turbine, the vent opening opening out to the downstream bleed zone, and the downstream bleed zone being situated adjacent to and downstream of a final disk of the low-pressure turbine to avoid oil being present upstream of the final disk of the low-pressure turbine,

wherein the downstream part comprises a stationary downstream stator element and a rotatable low-pressure turbine element respectively connected to one another,
wherein the downstream bleed zone is situated upstream of an extremity of the stationary downstream stator element that is located on a side of the downstream bleed zone,
wherein the oil discharge system comprises a configuring of the stationary downstream stator element and the rotatable low-pressure turbine element to form a first zone of sealing between the stationary downstream stator element and the rotatable low-pressure turbine element so that the oil is discharged toward the rotatable low-pressure turbine element,
wherein, when the level in the oil chamber does not exceed the threshold level, the stream of air passes through the vent opening into the downstream bleed zone so as to generate an overpressure in the downstream bleed zone, and
wherein the vent opening is defined by the stationary downstream stator element, an axis of the vent opening extending in a radial direction perpendicular to a longitudinal axis of the gas turbine engine.

4. The device as claimed in claim 3 , wherein the guide element includes a cowling attached to the downstream part of the gas turbine engine.

5. The device as claimed in claim 4 , wherein an extent of the cowling covers substantially a path leading from the vent opening to the downstream bleed zone of the low-pressure turbine.

6. The device as claimed in claim 4 , wherein the cowling has an at least substantially circumferential profile.

7. The device as claimed in claim 3 , wherein dimensions of the vent opening are configured to suit a flow rate of the discharged oil.

8. The device as claimed in claim 3 , wherein the oil chamber is defined in part by the stationary downstream stator element.

9. The device as claimed in claim 8 , wherein the vent opening is made in the stationary downstream stator element.

10. The device as claimed in claim 9 , wherein the oil entrainment device further comprises a configuring of the rotatable low-pressure turbine element, in a second zone of sealing between the stationary downstream stator element and rotatable low-pressure turbine element respectively, so that at least one of the air and the discharged oil is directed toward the vent opening.

11. The device as claimed in claim 3 , wherein the guide element extends radially.

12. The device as claimed in claim 4 , wherein the cowling is a flat sheet, and a material of the cowling is the same as a material of the stationary downstream stator element.

13. The device as claimed in claim 4 , wherein the cowling is a semi-circumferential trough incorporated into the stationary downstream stator element.

14. The device as claimed in claim 3 , wherein the oil is discharged to outside the gas turbine engine under an effect of gravity and a centrifugal effect of the spinning of the oil on stator and rotor walls respectively.

15. The device as claimed in claim 3 , wherein the vent opening is disposed rearward of the final disk of the low-pressure turbine.

16. The device as claimed in claim 3 , wherein the vent opening is positioned radially inward of the final disk of the low-pressure turbine.

Assignees

• Roche Amandine
• Bart Jacques Rene
• Gauthier Gerard Philippe
• Snecma

Inventors

• Roche Amandine
• Bart Jacques Rene
• Gauthier Gerard Philippe

Classifications

• F16N2210/02

  Turbines · CPC title

• F05D2260/98

  Lubrication · CPC title

• F05D2240/55

  Seals · CPC title

• F02C7/14

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · 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