NITROGEN BUBBLER SYSTEM IN FUEL TANK AND METHOD

• US 20140252171A1
• Filed: 03/08/2013
• Published: 09/11/2014
• Est. Priority Date: 03/08/2013
• Status: Active Grant

• Current Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Pratt & Whitney Canada Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: DOOLEY, Kevin Allan, WADDLETON, David, BUSH, Thomas A.
• Granted Patent: US 9,096,326 B2
• Time in Patent Office: Days
• US Class Current: 244/129.2
• CPC Class Codes: B01D 19/00 Degasification of liquids
• CPC Class Codes: B64D 37/32 Safety measures not otherwise provided for, e.g. preventing explosive conditions extinguishing or preventing fires in aircraft A62C

Abstract

An assembly of fuel tank and bubbler system comprises a fuel tank defining a storage volume adapted to receive fuel therein. The fuel tank comprises at least one fuel inlet, at least one fuel outlet, and at least one gas inlet adapted to be connected to an inert gas source to feed inert gas to fill an ullage in the storage volume. A bubbler system has at least one pipe extending into the fuel tank and adapted to be immersed into the fuel of the fuel tank. The pipe has a porous structure. The pipe is adapted to be connected to an inert gas source to inject inert gas via the porous structure into the fuel of the fuel tank. A method for treating fuel in a fuel tank is also provided.

Claims

1. An assembly of fuel tank and bubbler system comprising:

a fuel tank defining a storage volume adapted to receive fuel therein, the fuel tank comprising at least one fuel inlet, at least one fuel outlet, and at least one gas inlet adapted to be connected to an inert gas source to feed inert gas to fill an ullage in the storage volume; and

a bubbler system having at least one pipe extending into the fuel tank and adapted to be immersed into the fuel of the fuel tank, the pipe having a porous structure, the at least one pipe adapted to be connected to an inert gas source to inject inert gas via the porous structure into the fuel of the fuel tank.

2. The assembly according to claim 1, wherein the bubbler system has a bubbler inlet connected to an upper part of the tank and adapted to be in fluid communication with the ullage, the bubbler inlet being in fluid communication with the at least one pipe to inject the inert gas from the ullage into the fuel.

3. The assembly according to claim 2, further comprising a gas circulating pump in the bubbler system, between the bubbler inlet and the at least one pipe.

4. The assembly according to claim 1, further comprising a wall in the storage volume between the at least one pipe and the at least one fuel outlet, the wall having ports sized to allow fuel to pass therethrough and to limit bubble circulation therethrough.

5. The assembly according to claim 1, wherein the at least one pipe is generally horizontal in the tank.

6. The assembly according to claim 1, wherein the inert gas is Nitrogen in Oxygen-depleted air.

7. An aircraft comprising:

a fuel tank defining a storage volume adapted to receive fuel therein, the fuel tank comprising at least one fuel inlet, at least one fuel outlet, and at least one gas inlet adapted to be connected to an inert gas source to feed inert gas to fill an ullage in the storage volume; and

a bubbler system having at least one pipe extending into the fuel tank and adapted to be immersed into the fuel of the fuel tank, the pipe having a porous structure, the at least one pipe adapted to be connected to an inert gas source to inject inert gas via the porous structure into the fuel of the fuel tank.

8. The aircraft according to claim 7, wherein the bubbler system has a bubbler inlet connected to an upper part of the tank and adapted to be in fluid communication with the ullage, the bubbler inlet being in fluid communication with the at least one pipe to inject inert gas from the ullage into the fuel.

9. The aircraft according to claim 8, further comprising a gas circulating pump in the bubbler system, between the bubbler inlet and the at least one pipe.

10. The aircraft according to claim 7, further comprising a wall in the storage volume between the at least one pipe and the at least one fuel outlet, the wall having ports sized to allow fuel to pass therethrough and to limit bubble circulation therethrough.

11. The aircraft according to claim 7, wherein the at least one pipe is generally horizontal in the tank.

12. The aircraft according to claim 7, wherein the inert gas is Nitrogen in Oxygen-depleted air.

13. A method for treating fuel in a fuel tank comprising:

injecting an inert gas in a fuel tank to fill an ullage formed in the fuel tank above a fuel level;

injecting an inert gas into the fuel to dissolve nitrogen into the fuel; and

blocking gas bubbles in the fuel from an outlet of the tank.

14. The method according to claim 13, wherein injecting inert gas into the fuel comprises sucking the inert gas from the ullage.

15. The method according to claim 14, wherein sucking the inert gas air from the ullage comprises activating a gas circulating pump.

16. The method according to claim 13, wherein injecting an inert gas in the fuel tank and into the fuel comprises injecting Oxygen-depleted air, whereby the inert gas is Nitrogen.