IP Library Granted Patent US 11,407,516
Granted Patent B2
US 11,407,516 · App. 15/949,322 · Granted Aug 9, 2022

Closed or semi-closed loop onboard ceramic oxygen generation system

Inventors: Steven C. Peake (Dubuque, IA); Gary Byrd (Donahue, IA); Courtney J. Monzyk (Davenport, IA); Timothy Raleigh (Long Grove, IA); Chris Fellner (Blue Grass, IA); Gary Wu (Davenport, IA)
B64D13/08A62B7/14B64D13/06B64D2013/0637B64D2013/0662B64D2013/0677B64D2013/0681
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Quick Facts
Patent No.
US 11,407,516
App. No.
15/949,322
Granted
Aug 9, 2022
Kind
B2
Abstract

An onboard rebreathing loop system resident on an aircraft for providing oxygen to aircraft personnel includes a ceramic oxygen generating system (COGS) module configured to receive an inlet air and output a high purity oxygen (O 2 ) gas into a breathing loop and a carbon dioxide (CO 2 ) scrubber module configured to receive exhaled air from the aircraft personnel and output a CO 2 -scrubbed air into the breathing loop. The high purity O 2 gas and CO 2 -scrubbed air are mixed to form a mixed gas having a partial pressure of O 2 suitable for breathing by the aircraft personnel. The onboard rebreathing loop system may further include an odor removal module, an air temperature and/or humidity control module to condition the mixed gas before breathing by the aircraft personnel, and a gas sensor module to confirm the partial pressure of O 2 within the mixed gas before breathing by the aircraft personnel.

Claims (14)

1. An onboard rebreathing loop system resident on an aircraft for providing oxygen to aircraft personnel, the system comprising:

a) a ceramic oxygen generating system (COGS) module having a COGS inlet configured to receive an inlet air and a COGS outlet configured to output a high purity oxygen (O 2 ) gas into a breathing loop,

b) a carbon dioxide (CO 2 ) scrubber module having a scrubber inlet configured to receive exhaled air from the aircraft personnel and a scrubber outlet configured to output a CO 2 -scrubbed air into the breathing loop,

c) a gas sensor module configured to receive a mixed gas of the high purity O 2 gas and the CO 2 -scrubbed air and measure a partial pressure of O 2 within the mixed gas before breathing by the aircraft personnel,

d) a backup oxygen system (BOS) containing high purity backup O 2 gas, and

e) a controller communicatively coupled to the COGS module and the gas sensor module, wherein:

i) the controller instructs the BOS to provide backup O 2 gas directly to the aircraft personnel without entering the breathing loop when the gas sensor module measures the partial pressure of O 2 within the mixed gas to be below a predetermined threshold; and,

ii) the controller instructs the BOS to input backup O 2 gas into the breathing loop when the COGS module is unable to output a required amount of oxygen to maintain the desired partial pressure of O 2 within the mixed gas.

2. The onboard rebreathing loop system of claim 1 further comprising:

e) an odor removal module configured to receive the exhaled air or the CO 2 -scrubbed air and output a reduced-odor gas.

3. The onboard rebreathing loop system of claim 1 further comprising:

e) an air temperature and/or humidity control module configured to receive the mixed gas and condition the mixed gas before breathing by the aircraft personnel.

4. The onboard rebreathing loop system of claim 1 wherein the COGS is configured to recharge the BOS after the oxygen pressure in the BOS is below a predetermined value and there is an excess oxygen production capability of the COGS beyond meeting the demand from maintaining the desired partial pressure of O 2 within the breathing loop.

5. The onboard rebreathing loop system of claim 4 wherein the aircraft includes an oxygen compressor configured to receive a portion of the high purity O 2 gas from the COGS and deliver a high pressure high purity O 2 gas to the BOS to recharge the BOS.

Continuity (2)
Provisional Application 62483755 · Apr 10, 2017
Related Publication 20180290757A1 · Oct 11, 2018