Oil supply assembly for gas turbine engine

Patent metadata

Field	Value
Publication number	US-10697370-B2
Application number	US-201816117756-A
Country	US
Kind code	B2
Filing date	Aug 30, 2018
Priority date	Aug 30, 2018
Publication date	Jun 30, 2020
Grant date	Jun 30, 2020

Abstract

An oil supply system includes an oil supply assembly in a turbine engine. The assembly includes scavenge cavity and an oil supply tube located in and protected by a strut in the turbine engine to supply oil to a bearing chamber.

First claim

What is claimed is:

1. An oil supply system for a gas turbine engine comprising:
an oil supply reservoir,
a bearing chamber, and
an oil supply assembly interconnecting the oil supply reservoir and the bearing chamber, the oil supply assembly having a strut having a scavenge cavity extending longitudinally along a length of the strut, the scavenge cavity housing an oil supply tube and an oil return tube in its interior and terminating in a fitting that opens into a scavenge pipe to return oil to the oil supply reservoir wherein each of the oil supply and oil return tubes terminate at a point where the scavenge cavity has a maximum diameter and the fitting extends partially into the scavenge cavity.

2. The oil supply system of claim 1 , wherein the fitting further comprises an oil supply pipe that couples to the oil supply tube at one end and couples to the fitting via a seal component located between a flanged portion of the oil supply pipe and a surface of the fitting.

3. The oil supply system of claim 1 , wherein the fitting includes an opening flush with a top surface of the fitting and the scavenge pipe is located below the opening so that all the fluid in the scavenge cavity is taken up by the scavenge pipe.

4. The oil supply system of claim 3 , further comprising a pump coupled to one of the scavenge pipe and the oil supply pipe.

5. The oil supply system of claim 1 , wherein the oil supply tube and the oil return tube are positioned in parallel within the scavenge cavity.

6. The oil supply system of claim 1 , wherein the oil supply tube comprises a double-walled tube with an inner tube, an outer tube and an insulative air-gap therebetween.

7. An oil supply assembly for a gas turbine engine comprising:
a strut with an interior scavenge cavity extending longitudinally in the interior of the strut defining a first diameter at an upper end and a second diameter at a lower end,
an oil supply tube extending through the scavenge cavity and an oil return tube extending through the scavenge cavity, and
a scavenge pipe fitting configured to couple to the second diameter at the lower end of the strut having a scavenge pipe coupled to the scavenge pipe fitting in spaced apart relation to the oil return tube so that any oil that escapes from the oil supply tube, along with oil in the return tube is removed from the strut via the scavenge pipe wherein each of the oil supply and oil return tubes terminate at a point where the scavenge cavity has a maximum diameter and the scavenge pipe fitting extends partially into the scavenge cavity.

8. The oil supply assembly of claim 7 , wherein the second diameter is greater than the first diameter.

9. The oil supply assembly of claim 7 , wherein the scavenge pipe fitting further comprises an oil supply pipe that extends through the scavenge pipe fitting, into the scavenge cavity and is coupled to the oil supply tube.

10. The oil supply assembly of claim 9 , wherein the oil supply pipe comprises a flange extending around an exterior of the pipe, and a sliding seal positioned between the flange and the scavenge pipe fitting to provide a sliding surface of the oil supply pipe within the strut.

11. The oil supply assembly of claim 7 , wherein the oil supply tube and the oil return tube are positioned in parallel within the scavenge cavity.

12. The oil supply assembly of claim 7 , wherein the oil supply tube comprises a double-walled tube with an inner tube, an outer tube and an insulative air-gap therebetween.

13. The oil supply assembly of claim 7 , wherein the oil return tube comprises a double-walled tube with an inner tube, an outer tube and an insulative air-gap therebetween.

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Mckenney Tony

Classifications

• F01D9/06

  Fluid supply conduits to nozzles or the like · CPC title

• F01D25/16

  Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F05D2260/98

  Lubrication · CPC title

• F01D25/18 Primary

  Lubricating arrangements (of machines or engines in general F01M) · CPC title