IP Library › Granted Patent US 10,981,655
Granted Patent B2
US 10,981,655 · App. 16/198,014 · Granted Apr 20, 2021

Carbon dioxide adsorber for aircraft

Inventors: Lance R. Bartosz (Granby, MA); Catherine Thibaud (Cork, IE)
Assignee: HAMILTON SUNDSTRAND CORPORATION
B64D13/06B01D53/047B01D2253/10B01D2257/504B01D2259/4575B64D2013/0637B64D2013/0688
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Quick Facts
Patent No.
US 10,981,655
App. No.
16/198,014
Granted
Apr 20, 2021
Kind
B2
Abstract

A system for processing recirculation air recovered from an aircraft cabin includes a mixing chamber and a carbon dioxide removal system. The carbon dioxide removal system has an inlet for recovered recirculation air from the aircraft cabin, an outlet to the mixing chamber; at least two assemblies of carbon dioxide sorbent that are thermally linked, a CO 2 outlet valve; and a controller for managing desorption of carbon dioxide from the sorbent depending on aircraft status. The mixing chamber has an inlet from the carbon dioxide removal system, an inlet from an environmental control system, and an outlet connected to the aircraft cabin.

Claims (18)

1. A system for processing recirculation air recovered from an aircraft cabin comprising:

a mixing chamber and a carbon dioxide removal system,

wherein the carbon dioxide removal system has an inlet for recovered recirculation air from the aircraft cabin, at least two assemblies of carbon dioxide sorbent that are thermally linked; an outlet to the mixing chamber; a CO 2 outlet valve and a controller for managing desorption of carbon dioxide from the sorbent depending on aircraft status, and

further wherein the mixing chamber has an inlet from the carbon dioxide removal system, an inlet from an environmental control system, and an outlet connected to the aircraft cabin.

2. The system of claim 1 , wherein the assemblies are thermally linked by a thermoelectric device.

3. The system of claim 1 , wherein the assemblies are passively thermally linked.

4. The system of claim 1 , wherein the assemblies are interleaved.

5. The system of claim 1 , wherein the carbon dioxide sorbent comprises a solid amine sorbent.

6. The system of claim 1 , further comprising an ambient outlet valve.

7. A method for processing recovered recirculation air discharged from an aircraft cabin comprising:

supplying recovered recirculation air from the aircraft cabin to a carbon dioxide removal system having at least two thermally linked assemblies of carbon dioxide sorbent;

removing carbon dioxide from the recovered recirculation air to form processed recirculation air;

removing carbon dioxide from the carbon dioxide sorbent;

mixing the processed recirculation air with conditioned fresh air; and

sending the mixture to the aircraft cabin, wherein the removal of carbon dioxide from the carbon dioxide sorbent is by reduced pressure, elevated temperature or both and the method of removal is determined the by aircraft status.

8. The method of claim 7 , wherein reduced pressure is provided by ambient air when the ambient air has a pressure less than the cabin air.

9. The method of claim 7 , wherein the at least two thermally linked assemblies are interleaved.

10. The method of claim 7 , wherein the at least two assemblies of carbon dioxide sorbent comprise a solid amine sorbent.

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 22, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 055672/0189 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 20, 2020
From: UNITED TECHNOLOGIES RESEARCH CENTRE IRELAND, LIMITED
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 052710/0448 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 27, 2018
From: BARTOSZ, LANCE R.
To: HAMILTON SUNSTRAND CORPORATION
Reel/Frame 047589/0108 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 27, 2018
From: THIBAUD, CATHERINE
To: UNITED TECHNOLOGIES RESEARCH CENTRE IRELAND, LIMITED
Reel/Frame 047589/0150 →
Continuity (1)
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