Aircraft engine oil filler apparatus

Patent metadata

Field	Value
Publication number	US-10975740-B2
Application number	US-201916460609-A
Country	US
Kind code	B2
Filing date	Jul 2, 2019
Priority date	Jul 2, 2019
Publication date	Apr 13, 2021
Grant date	Apr 13, 2021

Abstract

An aircraft engine oil filler apparatus includes a filler tube configured to be received through a wall of an oil tank such that an open upper end of the filler tube is accessible from outside of the oil tank and a bottom end of the filler tube is disposed inside the oil tank, a valve received in the bottom end of the filler tube and movable between an open position in which the valve hydraulically connects the filler tube to the oil tank, and a closed position in which the valve hydraulically disconnects the filler tube from the oil tank, and a float disposed above the valve and operatively connected to the valve to move the valve from the open position to the closed position when oil inside the oil tank rises to a predetermined level. A method of operation of an oil filler apparatus is also described.

First claim

The invention claimed is:

1. An aircraft engine oil filler apparatus, comprising:
a filler tube configured to be received through a wall of an oil tank of an aircraft engine such that an open upper end of the filler tube is accessible from outside of the oil tank and a bottom end of the filler tube is disposed inside the oil tank;
a valve received at least in part in the bottom end of the filler tube and movable between an open position in which the valve hydraulically connects the filler tube to the oil tank, and a closed position in which the valve hydraulically disconnects the filler tube from the oil tank;
a float disposed above the valve and operatively connected to the valve to move the valve from the open position to the closed position when oil inside the oil tank rises to a predetermined level; and
a dipstick removably received in the filler tube, the dipstick having a length selected such that a bottom end of the dipstick is disposed above the valve.

2. The aircraft engine oil filler apparatus of claim 1 , comprising a link connecting the float to the valve.

3. The aircraft engine oil filler apparatus of claim 2 , wherein the valve includes a ball and a rod translationally received in the filler tube, the rod being connected to the link to translate relative to the filler tube with the float.

4. The aircraft engine oil filler apparatus of claim 3 , wherein the filler tube defines an aperture in the filler tube below the float and the valve includes a closure member disposed below the aperture when the valve is in the open position.

5. The aircraft engine oil filler apparatus of claim 4 , comprising a seat disposed inside the filler tube above the aperture, and the closure member is received in the seat and thereby blocks the filler tube above the aperture when the valve is in the closed position.

6. The aircraft engine oil filler apparatus of claim 5 , where the bottom end of the dipstick is disposed above the seat.

7. An oil tank of an aircraft engine, comprising:
a filler tube received through a wall of the oil tank such that an upper end of the filler tube is accessible from outside of the oil tank and a bottom end of the filler tube is disposed inside the oil tank, the filler tube defining apertures in the bottom end;
a valve received at least in part in the bottom end of the filler tube, the valve being operable between an open position in which the valve hydraulically connects a portion of the filler tube above the apertures to the inside of the oil tank via the apertures, and a closed position in which the valve blocks the apertures and thereby hydraulically disconnects the portion of the filler tube above the apertures from the inside of the oil tank; and
a float disposed inside the oil tank above the valve and operatively connected to the valve to move the valve from the open position to the closed position when oil inside the oil tank rises to a predetermined level.

8. The oil tank of claim 7 , wherein the valve is disposed below the apertures when in the open position and above the apertures when in the closed position.

9. The oil tank of claim 8 , comprising a dipstick removably received in the filler tube such that a bottom end of the dipstick is above the valve both when the valve is in the open position and when the valve is in the closed position.

10. A method of operation of an oil filler apparatus, comprising:
receiving oil into a filler tube of the oil filler apparatus inserted at least in part into an oil tank of an aircraft,
defining a fluid connection between a bottom end of the filler tube and the oil tank for oil to flow through the filler tube to the oil tank;
maintaining oil in the filler tube when the oil in the oil tank is above the bottom end of the filler tube; and
fluidly disconnecting the bottom end of the filler tube from the oil tank when the oil in the oil tank reaches a threshold that is above the bottom end of the filler tube, wherein fluidly disconnecting the bottom end of the filler tube from the oil tank includes seating a closure member against the filler tube, wherein seating the closure member includes telescoping a piston relative to the filler tube.

11. The method of claim 10 , wherein the seating the closure member includes translating the closure member.

12. The method of claim 10 , wherein the seating the closure member includes blocking an inner diameter of the filler tube.

13. The method of claim 10 , wherein the telescoping the piston includes translating a rod in the bottom end of the filler tube.

14. The method of claim 13 , wherein the telescoping the piston includes applying a buoyancy force to the rod to push the closure member with the rod.

15. The method of claim 14 , comprising hydraulically disconnecting the filler tube from the oil tank when pressure in the filler tube is smaller than pressure in the rod.

16. The method of claim 15 , comprising receiving a dipstick in the filler tube after the receiving oil into the filler tube but before the fluidly disconnecting the bottom end of the filler tube from the oil tank.

17. The method of claim 16 , further comprising receiving a cap on the filler tube and wherein the receiving the cap includes receiving the dipstick in the filler tube.

18. The method of claim 15 , wherein the receiving the dipstick occurs after fluidly disconnecting the bottom end of the filler tube from the oil tank.

Assignees

• Pratt & Whitney Canada

Inventors

• Daniel Marion
• Powers Sean
• Beaulieu Rose

Classifications

• F01M11/04 Primary

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

• F01M2011/0433

  with a device defining the lubricant level during filling · CPC title