Check valve for overflow oil line when pressure fill fittings are remote

Patent metadata

Field	Value
Publication number	US-10514107-B2
Application number	US-201715620180-A
Country	US
Kind code	B2
Filing date	Jun 12, 2017
Priority date	Jun 12, 2017
Publication date	Dec 24, 2019
Grant date	Dec 24, 2019

Abstract

An oil tank for a gas turbine engine includes a top and a bottom disposed vertically beneath the top. An overfill return passage extends from the bottom of the oil tank toward the top of the oil tank. An outlet is formed on the bottom of the oil tank and inside the overfill return passage. A check valve is inside the overfill return passage and is connected to the outlet. The check valve includes a seat circumscribing the outlet and a plug inside the overfill return passage. The plug has a lower density than an oil disposed inside the oil tank. The check valve does not include a spring such that the plug is configured to translate freely inside the overfill return passage.

First claim

The invention claimed is:

1. An oil tank for a gas turbine engine, wherein the oil tank comprises:
a top;
a bottom disposed vertically beneath the top;
an overfill return passage extending from the bottom of the oil tank toward the top of the oil tank;
an outlet formed on the bottom of the oil tank and inside the overfill return passage; and
a check valve inside the overfill return passage and connected to the outlet, wherein the check valve comprises:
a seat circumscribing the outlet;
a plug inside the overfill return passage, wherein the plug has a lower density than an oil disposed inside the oil tank; and
a plug retainer inside the overfill return passage and positioned vertically between the plug and the top of the oil tank, wherein the plug retainer and the seat trap the plug inside the overfill return passage, and
wherein the check valve does not include a spring such that the plug is configured to translate freely between the seat and the plug retainer.

2. The oil tank of claim 1 further comprising:
an inlet formed in the bottom of the oil tank and outside of the overfill return passage.

3. The oil tank of claim 2 further comprising:
a second check valve connected to the inlet, wherein the second check valve comprises a ball and a spring configured such that the spring biases the ball against the inlet to block the inlet.

4. The oil tank of claim 3 , wherein the plug is a hollow metal ball.

5. The oil tank of claim 3 , wherein the plug is a bullet with a cylindrical body connected to a rounded mate face that corresponds with a sealing face of the seat.

6. The oil tank of claim 5 , wherein the overfill return passage comprises:
a plurality of guide ribs extending between the seat and the plug retainer, wherein each of the plurality of guide ribs are spaced from one another along a circumference of the overfill return passage.

7. The oil tank of claim 6 , wherein the bullet is hollow and is formed from metal.

8. An oil tank for a gas turbine engine, wherein the oil tank comprises:
a top;
a bottom disposed vertically beneath the top;
an overfill return passage extending from the bottom of the oil tank toward the top of the oil tank;
an outlet formed on the bottom of the oil tank and inside the overfill return passage; and
a check valve inside the overfill return passage and connected to the outlet, wherein the check valve comprises:
a seat circumscribing the outlet;
a plug inside the overfill return passage, wherein the plug has a lower density than an oil disposed inside the oil tank; and
wherein the check valve does not include a spring such that the plug is configured to translate freely inside the overfill return passage.

9. The oil tank of claim 8 , wherein the overfill return passage comprises:
a plug retainer inside the overfill return passage and positioned vertically between the plug and the top of the oil tank, wherein the plug retainer and the seat trap the plug inside the overfill return passage.

10. The oil tank of claim 9 further comprising:
an inlet formed proximate the bottom of the oil tank and outside of the overfill return passage.

11. The oil tank of claim 10 further comprising:
a second check valve connected to the inlet, wherein the second check valve comprises a ball and a spring configured such that the spring biases the ball against the inlet to block the inlet.

12. The oil tank of claim 11 further comprising:
a second outlet formed in the bottom or a side of the oil tank outside of the overfill return passage.

13. The oil tank of claim 12 further comprising:
an air outlet formed in the oil tank vertically above a top edge of the overfill return passage.

14. The oil tank of claim 13 further comprising:
a second inlet formed on the oil tank outside of the overfill return passage.

15. The oil tank of claim 9 , wherein the plug retainer comprises an inside diameter smaller than an inside diameter of the overfill return passage.

16. The oil tank of claim 15 , wherein the plug retainer is a snap ring.

17. The oil tank of claim 8 , wherein the plug is a hollow metal ball.

18. The oil tank of claim 8 , wherein the plug is a hollow bullet with a cylindrical body connected to a rounded mate face that corresponds with a sealing face of the seat.

Assignees

• United Technologies Corp

Inventors

• Stachowiak David Allen

Classifications

• F16N2280/00

  Valves · CPC title

• F16N2210/08

  Aircraft · CPC title

• F16N23/00

  Special adaptations of check valves (check valves in general F16K) · CPC title

• F16N19/00

  Lubricant containers for use in lubricators or lubrication systems · CPC title

• F01M11/04

  Filling or draining lubricant of or from machines or engines · CPC title