Aircraft fuel tank inerting system

Patent metadata

Field	Value
Publication number	US-9834314-B2
Application number	US-201514831038-A
Country	US
Kind code	B2
Filing date	Aug 20, 2015
Priority date	Aug 22, 2014
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

An aircraft fuel tank inerting system and a method of inerting an aircraft fuel tank.
The aircraft fuel tank inerting system having an on-board inerting gas generation system arranged in fluid communication between a fuel tank vent system and an aircraft fuel tank.

First claim

The invention claimed is:

1. An aircraft fuel tank inerting system having an on-board inerting gas generation system arranged in fluid communication between a fuel tank vent system and the aircraft fuel tank, wherein the fuel tank vent system includes a NACA duct arranged to supply the on-hoard inerting gas generation system with atmospheric air and wherein the on-board inerting gas generation system additionally comprises an air pressure reduction device.

2. The aircraft fuel inerting system of claim 1 wherein the on-board inerting gas generation system comprises an air separation module.

3. The aircraft fuel inerting system of claim 1 wherein the air pressure reduction device is a venturi based vacuum generator.

4. The aircraft fuel inerting system of claim 1 wherein the air pressure reduction device is a vacuum pump.

5. The aircraft fuel inerting system of claim 1 wherein the fuel tank vent system includes a flame arrestor.

6. The aircraft fuel inerting system of claim 1 having an air separation module filter arranged in fluid communication between the fuel tank vent system and the on-board inciting gas generation system.

7. An aircraft fuel tank inerting system having an on-board inerting gas generation system arranged in fluid communication between a fuel tank vent system and the aircraft fuel tank, the aircraft fuel tank inerting system further comprising an alternate vent pathway between the fuel tank vent system and the aircraft fuel tank.

8. The aircraft fuel inerting system of claim 7 having a climb/dive valve arranged in the alternate vent pathway between the fuel tank vent system and the aircraft fuel tank, bypassing the on-board inerting gas generation system.

9. An aircraft having the aircraft fuel inerting system of claim 1 .

10. A method of inerting an aircraft fuel tank comprising the steps of:
providing an on-board inerting gas generation system in fluid communication between a fuel tank vent system and the aircraft fuel tank;
providing an air pressure reduction device in fluid communication with the on-board inerting gas generation system;
supplying the on-board inerting gas generation system with atmospheric air via the fuel tank vent system, wherein the on-board inerting gas generation system is supplied with atmospheric air via a NACA duct in the fuel tank vent system; and
supplying the aircraft fuel tank with inerted air from the on-board inerting gas generation system.

11. A method of inerting an aircraft fuel tank according to claim 10 further comprising the step of:
providing an air separation module in the on-board inerting gas generation system; wherein the air separation module is supplied with atmospheric air via the NACA duct in the fuel tank vent system and the air separation module exhausts oxygen depleted air to the fuel tank.

12. A method of inerting an aircraft fuel tank according to claim 10 comprising the further steps of:
passing a first proportion of the atmospheric air through the air pressure reduction device to produce a supply of reduced pressure air passing a second proportion of the atmospheric air along one side of a membrane of the air separation module, exposing the other side of the membrane of the air separation module to the reduced pressure air, so that oxygen passes from the air on one side of the membrane to the reduced pressure air on the other side of the membrane and the air separation module exhausts an oxygen depleted air to the fuel tank.

Assignees

• Airbus Operations Ltd

Inventors

• Burnell Stephen
• Leigh Tim

Classifications

• Y02T50/44

  Cross-Sectional Technologies · mapped topic

• B01D53/22

  by diffusion (manufacturing semi-permeable membranes B01D67/00; form, structure or properties of semi-permeable membranes B01D69/00; material for semi-permeable membranes B01D71/00) · CPC title

• B01D2257/104

  Oxygen · CPC title

• B01D19/0031

  by filtration · CPC title

• B64D37/32 Primary

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title