Systems and methods for flammability reduction and ventilation using nitrogen-enriched gas for transportation vehicle protection

Patent metadata

Field	Value
Publication number	US-10286235-B2
Application number	US-201715439615-A
Country	US
Kind code	B2
Filing date	Feb 22, 2017
Priority date	Feb 22, 2017
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

An example unit load device inerting system includes a nitrogen generation system, a first conduit coupled to the nitrogen generation system to carry nitrogen, an inlet located downstream of the first conduit and attached to a unit load device to deliver the nitrogen into the unit load device, an outlet attached to the unit load device, and a second conduit coupled to the outlet to carry gas out of the unit load device. An example method includes flowing nitrogen through a first conduit from a nitrogen generation system to an inlet located downstream of the first conduit and the inlet is attached to a unit load device to deliver the nitrogen into the unit load device, and venting the unit load device to transport gas out of the unit load device through a second conduit coupled to an outlet configured to be attached to the unit load device.

First claim

What is claimed is:

1. A unit load device inerting system comprising:
a nitrogen generation system, wherein the nitrogen generation system is on-board an aircraft;
a first conduit coupled to the nitrogen generation system and configured to carry nitrogen;
an inlet located downstream of the first conduit, wherein the inlet is configured to be attached to a unit load device to deliver the nitrogen into the unit load device;
an outlet configured to be attached to the unit load device;
a second conduit coupled to the outlet, wherein the second conduit is configured to carry a gas out of the unit load device; and
a computer controller coupled to the nitrogen generation system and controlling operation of the nitrogen generation system to deliver the nitrogen into the unit load device (i) prior to take-off of the aircraft in flight, and (ii) for an entire duration of the aircraft in flight except during a portion of a descent.

2. The unit load device inerting system of claim 1 , wherein the unit load device is a cargo container for an aircraft.

3. The unit load device inerting system of claim 1 , further comprising a shutoff valve located downstream of the nitrogen generation system and coupled to the first conduit, wherein the shutoff valve controls flow of nitrogen between the first conduit and a nitrogen inerting system for a fuel tank.

4. The unit load device inerting system of claim 1 , further comprising:
a third conduit coupled to the nitrogen generation system and configured to carry nitrogen into a cargo compartment of an aircraft.

5. The unit load device inerting system of claim 1 , further comprising:
a plurality of inlets located downstream of the first conduit, wherein the inlet is one of the plurality of inlets, and wherein the plurality of inlets are configured to be attached to a plurality of unit load devices to selectively deliver the nitrogen into the plurality of unit load devices.

6. The unit load device inerting system of claim 5 , further comprising:
the computer controller coupled to the plurality of inlets to selectively operate the plurality of inlets to deliver the nitrogen into the plurality of unit load devices based on contents of the plurality of unit load devices.

7. The unit load device inerting system of claim 1 , further comprising:
a plurality of outlets configured to be attached to a plurality of unit load devices, wherein the outlet is one of the plurality of outlets; and
the second conduit coupled to the plurality of outlets, wherein the second conduit is configured to carry the gas out of the plurality of unit load devices.

8. The unit load device inerting system of claim 1 , further comprising:
a temperature sensor located downstream of the unit load device; and
the computer controller receiving an output of the temperature sensor and sending a notification based on a temperature detected above a threshold temperature.

9. The unit load device inerting system of claim 1 , further comprising:
a smoke sensor located downstream of the unit load device; and
the computer controller receiving an output of the smoke sensor and sending a notification based on smoke being detected.

10. The unit load device inerting system of claim 1 , further comprising:
a disconnect device coupled to the inlet enabling reversible attachment of the inlet to the unit load device; and
a disconnect device coupled to the outlet enabling reversible attachment of the outlet to the unit load device.

11. A unit load device inerting system comprising:
a unit load device having an inlet port positioned on a first wall of the unit load device and an outlet port positioned on a second wall of the unit load device;
a nitrogen generation system coupled to the inlet port of the unit load device to deliver nitrogen into the unit load device, wherein the nitrogen generation system is on-board an aircraft;
an outlet configured to be attached to the outlet port of the unit load device;
a conduit coupled to the outlet to carry a gas out of the unit load device; and
a computer controller coupled to the nitrogen generation system and controlling operation of the nitrogen generation system to deliver the nitrogen into the unit load device (i) prior to take-off of the aircraft in flight, and (ii) for an entire duration of the aircraft in flight except during a portion of a descent.

12. The unit load device inerting system of claim 11 , wherein the unit load device has a top and a bottom, and wherein the inlet port is positioned proximal to the bottom.

13. The unit load device inerting system of claim 11 , wherein the unit load device has a top and a bottom, and wherein the outlet port is positioned proximal to the top.

14. The unit load device inerting system of claim 11 , wherein the unit load device is substantially rectangular in shape, and wherein the inlet port is positioned diagonally across the unit load device from the outlet port.

15. A method comprising:
flowing nitrogen through a first conduit from a nitrogen generation system to an inlet located downstream of the first conduit, wherein the nitrogen generation system is on-board an aircraft and wherein the inlet is configured to be attached to a unit load device to deliver the nitrogen into the unit load device;
continuously flowing the nitrogen to deliver the nitrogen into the unit load device (i) prior to take-off of the aircraft in flight, and (ii) for an entire duration of the aircraft in flight except during a portion of a descent; and
venting the unit load device to transport a gas out of the unit load device through a second conduit coupled to an outlet configured to be attached to the unit load device.

16. The method of claim 15 , wherein a plurality of inlets are located downstream of the first conduit, wherein the inlet is one of the plurality of inlets, and wherein the plurality of inlets are configured to be attached to a plurality of unit load devices, the method further comprising:
selecting one or more unit load devices of the plurality of unit load devices to which to deliver the nitrogen based on contents of the plurality of unit load devices.

Assignees

• Boeing Co

Inventors

• Smith David
• Ferguson Douglas

Classifications

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title

• A62C3/08 Primary

  in aircraft {(A62C3/0207 takes precedence)} · CPC title

• A62C37/36

  an actuating signal being generated by a sensor separate from an outlet device · CPC title

• B65D19/38

  Details or accessories · CPC title

• A62C3/002 Primary

  for warehouses, storage areas or other installations for storing goods · CPC title