IP Library › Granted Patent US 9,623,982
Granted Patent B2
US 9,623,982 · App. 14/949,916 · Granted Apr 18, 2017

On-board aircraft nitrogen enriched air and cooling fluid generation system and method

Inventor: Anurag Sharma (Bangalore, IN)
Assignee: AIRBUS GROUP INDIA PRIVATE LIMITED
B64D37/32B01D53/227B64D13/08F25J1/005F25J1/0015F25J1/0052F25J1/0062F25J1/0065F25J1/0204F25J1/0275B01D2259/4575F25J2205/80F25J2210/40F25J2220/40F25J2220/44F25J2260/44
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Quick Facts
Patent No.
US 9,623,982
App. No.
14/949,916
Granted
Apr 18, 2017
Kind
B2
Abstract

An on-board aircraft nitrogen enriched air and cooling fluid generation system and method are disclosed. In one embodiment, the system includes a first heat exchanger which is configured to receive pressurized air from a source of pressurized air. Further, the first heat exchanger cools the pressurized air to a temperature in the range of −120° C. to −70° C. Furthermore, the system includes a separation unit is configured and dimensioned to communicate with the first heat exchanger. The separation unit generates nitrogen enriched air from the cooled air at the temperature range of −120° C. and −70° C.

Claims (26)

1. An on-board aircraft system, comprising:

a first heat exchanger configured to receive pressurized air from a source of pressurized air, wherein the first heat exchanger cools the pressurized air to a temperature in the range of −120° C. to −70° C.; and

a separation unit configured and dimensioned to communicate with the first heat exchanger and to generate nitrogen enriched air from the cooled air at the temperature range of −120° C. and −70° C.

2. The system of claim 1 , further comprising:

a second heat exchanger coupled to the separation unit to liquefy at least a portion of the generated nitrogen enriched air by cooling the portion of the generated nitrogen enriched air to a temperature in the range of −210° C. to −195° C.; and

a nitrogen storage container to store the liquefied portion of the nitrogen enriched air.

3. The system of claim 2 , wherein the first heat exchanger and the second heat exchanger comprise one of a liquid helium heat exchanger and a neon heat exchanger.

4. The system of claim 1 , wherein the source of pressurized air is disposed between the first heat exchanger and an air supply source to generate the pressurized air from air supplied from the air supply source, wherein the air supply source is selected from the group consisting of cabin air, bleed air and ram air.

5. The system of claim 1 , wherein the separation unit comprises at least two separation membranes, wherein one of the at least two separation membranes binds byproducts and lets nitrogen pass to generate the nitrogen enriched air, while the other separation membrane of the at least two separation membranes uses the cooled air to purge the byproducts.

6. The system of claim 5 , further comprising:

a sensor coupled to the separation unit, wherein the sensor measures oxygen content in the generated nitrogen enriched air and when said oxygen content raises above a predetermined threshold value, reverses operation of the at least two separation membranes.

7. The system of claim 6 , wherein the at least two separation membranes comprise one of low temperature ceramic separation membranes, gas chromatographic separation membranes, perovskite separation membranes, and zeolite separation membranes.

8. A method for on-board generation of nitrogen enriched air in an aircraft, comprising:

feeding pressurized air into a first heat exchanger to cool the pressurized air to a temperature in the range of −120° C. to −70° C.; and

feeding the cooled air at the temperature range of −120° C. and −70° C. into a separation unit and generating nitrogen enriched air from the cooled air.

9. The method of claim 8 , further comprising:

liquefying at least a portion of the generated nitrogen enriched air by cooling the portion of the generated nitrogen enriched air to a temperature in the range of −210° C. to −195° C. in a second heat exchanger; and

storing the liquefied portion of the nitrogen enriched air in a nitrogen storage container.

10. The method of claim 9 , wherein the first heat exchanger and the second heat exchanger comprise one of a liquid helium heat exchanger and a neon heat exchanger.

11. The method of claim 8 , wherein the pressurized air is generated from air supplied from an air supply source, and wherein the air supply source is selected from the group consisting of cabin air, bleed air and ram air.

12. The method of claim 8 , wherein the separation unit comprises at least two separation membranes.

13. The method of claim 12 , wherein generating the nitrogen enriched air from the cooled air comprises:

binding byproducts and letting nitrogen pass in one of the at least two separation membranes to generate the nitrogen enriched air, while purging the byproducts using the cooled air in other separation membrane of the at least two separation membranes.

14. The method of claim 13 , further comprising:

measuring oxygen content in the generated nitrogen enriched air using a sensor and reversing operation of the at least two separation membranes when said oxygen content raises above a predetermined threshold value.

15. The method of claim 14 , wherein the at least two separation membranes comprise one of low temperature ceramic separation membranes, gas chromatographic separation membranes, perovskite separation membranes, and zeolite separation membranes.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 24, 2015
From: SHARMA, ANURAG
To: AIRBUS GROUP INDIA PRIVATE LIMITED
Reel/Frame 037124/0383 →
Priority Claims (1)
IN 140/CHE/2015 · Jan 8, 2015 · national
Continuity (1)
Related Publication 20160200446A1 · Jul 14, 2016