In-line deaerator device for windmill-auxiliary oil system for fan drive gear system

Patent metadata

Field	Value
Publication number	US-2016245117-A1
Application number	US-201514629834-A
Country	US
Kind code	A1
Filing date	Feb 24, 2015
Priority date	Feb 24, 2015
Publication date	Aug 25, 2016
Grant date	—

Abstract

A lubrication system for a fan drive gear system of a turbofan engine includes an auxiliary pump for communicating lubricant to bearings of a gear system. A deaerator is disposed between a lubricant source and the auxiliary pump for separating gases is contained within the lubricant. The deaerator includes a vane section for inducing a radial flow in the lubricant for separating gas from the lubricant. A gas turbine engine and method are also disclosed.

First claim

What is claimed is:

1 . A lubrication system for a fan drive gear system of a turbofan engine comprising:
an auxiliary pump for communicating lubricant to bearings of a gear system; and a deaerator disposed between a lubricant source and the auxiliary pump for separating gases contained within the lubricant, the deaerator including a vane section for inducing a radial flow in the lubricant for separating gas from the lubricant.

2 . The system as recited in claim 1 , wherein the deaerator includes a first outlet for lubricant disposed radially outside of a second outlet for gas.

3 . The system as recited in claim 2 , wherein the second outlet includes a vent that extends radially out of the deaerator to exhaust gas.

4 . The system as recited in claim 1 , wherein the vane section includes a plurality of vanes extending radially outward transverse to a direction of lubricant flow for inducing a radial component to lubricant flow.

5 . The system as recited in claim 4 , wherein the deaerator comprises a conduit including a chamber between the vane section and the first outlet and the second outlet, wherein the radial flow component induced by the vane section drives the lubricant against the inner walls of the chamber leaving the gas spaced apart from the inner walls.

6 . The system as recited in claim 5 , wherein the radial flow in the lubricant comprises a swirl that drives heavier lubricant against inner walls of the deaerator and leaves the gas to flow about a central line of the conduit.

7 . The system as recited in claim 1 , including a gutter capturing lubricant exhausted from the fan drive gear system, the gutter in communication with the auxiliary pump through the deaerator.

8 . The system as recited in claim 1 , including a bearing supporting at least one gear of the fan drive gear system, wherein the bearing is in communication with an outlet of the auxiliary pump to receive lubricant.

9 . The system as recited in claim 1 , including a mechanical link between a portion of the fan drive gear system and the auxiliary pump for driving the auxiliary pump.

10 . The system as recited in claim 1 , including a valve assembly for directing lubricant from the auxiliary pump to at least one bearing in response to a reduction in lubricant flow from a main lubricant system below a predetermined flow rate.

11 . A gas turbine engine comprising:
a fan including a plurality of fan blades rotatable about an axis; a geared architecture driven by a turbine section for rotating the fan about the axis; a main lubricant system directing lubricant flow to at least one bearing surface of the geared architecture; and an auxiliary lubricant system for directing lubricant flow to the at least one bearing surface responsive to a reduction in lubricant flow from the main lubricant system below a predetermined flow rate, wherein the auxiliary lubricant system includes a deaerator communicating lubricant to an auxiliary pump, the deaerator including a vane section for inducing a radial flow in the lubricant for separating gas from the lubricant prior to entering the auxiliary pump.

12 . The gas turbine engine as recited in claim 11 , wherein the deaerator includes a first outlet for lubricant disposed radially outside of a second outlet for gas.

13 . The gas turbine engine as recited in claim 12 , wherein the second outlet includes a vent that extends radially out of the deaerator to exhaust gas.

14 . The gas turbine engine as recited in claim 13 , wherein the deaerator comprises a conduit including a chamber between the vane section and the first outlet and the second outlet, wherein a radial flow component induced by the vane section drives the lubricant against the inner walls of the chamber leaving the gas spaced apart from the inner walls.

15 . The gas turbine engine as recited in claim 11 , including a bearing supporting at least one gear of the geared architecture, wherein the bearing is in communication with an outlet of the auxiliary pump to receive lubricant.

16 . A method of designing a lubrication system for a fan drive gear system of a turbofan engine comprising:
configuring a main lubricant system for providing lubricant to at least one bearing system during a first engine operating condition; configuring an auxiliary lubricant system for communicating lubricant to the at least one bearing surface during a second engine operating condition, wherein during the second engine operating condition the main lubricant system provides a lubricant flow below a desired lubricant flow rate threshold; and defining a deaerator within the auxiliary lubricant system between a source of captured lubricant and an auxiliary pump for separating gases from the captured lubricant, the deaerator including a vane section for inducing a radial flow in the lubricant for separating gases from the lubricant.

17 . The method as recited in claim 16 , including defining the deaerator to include a first outlet for lubricant disposed radially outside of a second outlet for gas, and configuring the second outlet to include a vent that extends radially out of the deaerator to exhaust gas.

18 . The method as recited in claim 17 , including configuring the deaerator to define a conduit including a chamber between the vane section and the first outlet and the second outlet, wherein a radial flow component induced by the vane section drives the lubricant against the inner walls of the chamber leaving the gas spaced apart from the inner walls.

Assignees

• United Technologies Corp

Inventors

• Parnin Francis
• Sheridan William G
• Groholski John S

Classifications

• F01D25/20 Primary

  using lubrication pumps · CPC title

• F01M2001/1028

  characterised by the type of purification · CPC title

• F01D25/22

  using working-fluid or other gaseous fluid as lubricant · CPC title

• F16H57/0482

  Gearings with gears having orbital motion · CPC title

• F02C7/06

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title