Oil tank assembly for gas turbine engine

Patent metadata

Field	Value
Publication number	US-10301969-B2
Application number	US-201615349325-A
Country	US
Kind code	B2
Filing date	Nov 11, 2016
Priority date	Nov 11, 2016
Publication date	May 28, 2019
Grant date	May 28, 2019

Abstract

Oil tanks for gas turbine engines and associated assembly methods are disclosed. In one exemplary embodiment, an oil tank is configured to be installed to occupy a radially-inner space defined by an annular radial air inlet duct of a reverse flow gas turbine engine. The oil tank may comprise a first tank portion and a second tank portion assembled together to cooperatively define an interior volume of the tank. An optional intermediate spacer may be disposed between the first tank portion and the second tank portion in order to form an oil tank of a larger size.

First claim

What is claimed is:

1. An oil tank assembly for a gas turbine engine, the oil tank assembly comprising:
a first tank portion with a first interfacing counterpart;
a second tank portion with a second interfacing counterpart; and
a spacer disposed between the first and second interfacing counterparts, the first and the second tank portions and the spacer being assembled together to cooperatively define the oil tank with an internal tank volume of an expanded size,
wherein the first and second interfacing counterparts are configured to interface together without the spacer to permit the first and second tank portions to be assembled without the spacer to cooperatively define the oil tank with an internal tank volume of a reduced size.

2. The oil tank assembly as defined in claim 1 , wherein the first tank portion comprises a tank wall that is substantially axisymmetric about an axis.

3. The oil tank assembly as defined in claim 2 , wherein the first tank portion has an outer periphery that is substantially circular when viewed along the axis.

4. The oil tank assembly as defined in claim 1 , wherein the first interfacing counterpart and the second interfacing counterpart are substantially circular.

5. The oil tank assembly as defined in claim 4 , wherein the first interfacing counterpart comprises a first radially-inwardly-facing sealing surface relative to the axis.

6. The oil tank assembly as defined in claim 5 , comprising a first compressible sealing member disposed between the first radially-inwardly-facing sealing surface of the first interfacing counterpart and the spacer.

7. The oil tank assembly as defined in claim 6 , wherein the spacer comprises a second radially-inwardly-facing sealing surface relative to the axis.

8. The oil tank assembly as defined in claim 7 , comprising a second compressible sealing member disposed between the second radially-inwardly-facing sealing surface of the spacer and the second tank portion.

9. An oil tank kit, the kit comprising:
a first tank portion with a first interfacing counterpart;
a second tank portion with a second interfacing counterpart; and
a spacer configured to be assembled between the first and second interfacing counterparts so that the first tank portion, the second tank portion and the spacer cooperatively define the oil tank with an internal tank volume of an expanded size in a first configuration of the oil tank,
wherein the first and second interfacing counterparts are configured to interface together without the spacer so that the first and second tank portions assembled together without the spacer cooperatively define the oil tank with an internal tank volume of a reduced size in a second configuration of the oil tank.

10. The kit as defined in claim 9 , wherein the first interfacing counterpart and the second interfacing counterpart are substantially circular.

11. The kit as defined in claim 10 , wherein the first interfacing counterpart comprises a first radially-inwardly-facing sealing surface.

12. The kit as defined in claim 11 , comprising a first compressible sealing member configured to be disposed between the first radially-inwardly-facing sealing surface of the first interfacing counterpart and the spacer.

13. The kit as defined in claim 12 , wherein the spacer comprises a second radially-inwardly-facing sealing surface.

14. The kit as defined in claim 13 , comprising a second compressible sealing member configured to be disposed between the second radially-inwardly-facing sealing surface of the spacer and the second tank portion.

15. A method for assembling an oil tank, the method comprising:
receiving a first tank portion;
receiving a second tank portion;
when a first internal tank volume of a first size is desired for the oil tank, assembling the first tank portion with the second tank portion without an intermediate spacer disposed therebetween so that the first tank portion and the second tank portion cooperatively define the first internal tank volume of the first size; and
when a second internal tank volume of a second size greater than the first size is desired for the oil tank, assembling the first tank portion with the second tank portion with the intermediate spacer disposed therebetween so that the first tank portion, the second tank portion and the intermediate spacer cooperatively define the second internal tank volume of the second size.

16. The method as defined in claim 15 , comprising, when the first internal tank volume of the first size is desired, placing a compressible sealing member between the first tank portion and the second tank portion.

17. The method as defined in claim 15 , comprising, when the second internal tank volume of the second size is desired, placing a compressible sealing member between the first tank portion and the intermediate spacer.

18. The method as defined in claim 15 , comprising, when the second internal tank volume of the second size is desired, placing a compressible sealing member between the intermediate spacer and the second tank portion.

Assignees

• Pratt & Whitney Canada

Inventors

• Desjardins Michel
• Bonacorsi Francis

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

• F02C7/06

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

• F05D2260/98

  Lubrication · CPC title

• F01D25/18 Primary

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