Oxygen concentrator with beds' duty cycle control and self-test

• US 5,858,063 A
• Filed: 06/03/1997
• Issued: 01/12/1999
• Est. Priority Date: 06/03/1997
• Status: Expired due to Term

• Current Assignee: Carleton Life Support Systems, Inc. (Cobham PLC)
• Original Assignee: Litton Systems Incorporated
• Inventors: Molis, William David, Frantz, Richard Kent, Cao, Tuan Quoc, Hager, Charles Bradley, Crome, Victor Paul, Hart, Russell Frank
• Primary Examiner(s): SPITZER, ROBERT H
• Application Number:
  US08/868,419
• Time in Patent Office: 588 Days
• Field of Search: 95/8, 95/11, 95/96-98, 95/102, 95/105, 95/130, 96/111, 96/115, 96/117, 96/130, 96/144
• US Class Current: 95/11
• CPC Class Codes: B01D 2256/12 Oxygen
• CPC Class Codes: B01D 2257/102 Nitrogen
• CPC Class Codes: B01D 2259/402 using two beds
• CPC Class Codes: B01D 2259/4575 in aeroplanes or space ships
• CPC Class Codes: B01D 53/0454 Controlling adsorption controlling temperature swing adsorption B01D53/0462, controlling pressure swing adsorption B01D53/047
• CPC Class Codes: B01D 53/047 Pressure swing adsorption
• CPC Class Codes: B64D 10/00 Flight suits helmets in general A42B3/00; breathing helmets A62B18/00
• CPC Class Codes: B64D 2013/0677 comprising on board oxygen generator systems

Abstract

A method of controlling an oxygen concentrator having a first sieve bed operated over successive control periods according to a duty cycle for alternately pressurizing and flushing the first sieve bed and a second sieve bed operated over the successive control periods according to a reciprocal of the duty cycle is disclosed. The duty cycle and the reciprocal duty cycle are adjusted during every second one of the successive control periods to change the pressurizing relative to the flushing of the first sieve bed and to change the flushing relative to the pressurizing of the second sieve bed, for reducing concentration of oxygen produced. The duty cycle and the reciprocal duty cycle are adjusted during remaining control periods to change the flushing relative to the pressurizing of the first sieve bed and to change the pressurizing relative to the flushing of the second sieve bed, such that water vapor is purged from the first and second sieve beds after pressurizing thereof. A pressure-swing adsorption (PSA) subsystem performance check is disclosed. This test is performed as part of a maintenance BIT (Built-In-Test) function. After verifying that the oxygen sensor accuracy is acceptable using prior art techniques, a set of bleed valves are opened to load the oxygen concentrator at a specific flow. The oxygen concentration is then checked via the sensor to determine whether the PSA subsystem is operating to within a predetermined concentration level.

Claims

1. A method of controlling performance of an oxygen concentrator having a first molecular sieve bed which is operated over successive control periods according to a duty cycle, said duty cycle including time periods for alternately pressurizing and flushing said first molecular sieve bed, and a second molecular sieve bed which is operated over the successive control periods, said duty cycle including time periods having a length which is a reciprocal of said time periods of the first molecular sieve bed during a particular control period for alternately flushing and pressuring said second molecular sieve bed, the method comprising the steps of:

a) adjusting said time periods during successive duty cycles and successive time periods during the reciprocal duty cycle during every second one of said successive control periods to change the time period for pressurizing relative to the time period for flushing of said first molecular sieve bed and to change the time period for the flushing relative to the time period for the pressurizing of the second molecular sieve bed, thereby degrading performance of the oxygen concentrator for reducing concentration of oxygen produced by the oxygen concentrator; and

b) adjusting the time period during the duty cycle and the time period during the reciprocal duty cycle during remaining control periods to change the time period for the flushing relative to the time period for the pressurizing of the first molecular sieve bed and to change the time period for the pressurizing relative to the flushing of the second molecular sieve bed, such that water vapor is purged from the first and the second molecular sieve beds after pressurizing thereof.

2. The method of claim 1, wherein the duty cycle pressurizing and flushing is adjusted within a range of from 50--50% for highest performance to 80%-20%for lowest performance.

3. The method of claim 1, wherein step a) comprises prolonging the time period.

4. The method of claim 3, wherein each of the time periods of a duty cycle during a control period is the same.

5. The method of claim 1, wherein step a) comprises shortening the time period.

6. The method of claim 5, wherein each of the time periods of a duty cycle during a control period is the same.

7. The method of claim 1, wherein the time period is shortened when the oxygen concentration reaches a predetermined minimum level.

8. The method of claim 1, wherein the time period is lengthened when the oxygen concentration reaches a predetermined maximum level.

9. An aircraft oxygen system for providing a controlled concentration of oxygen to the cabin of said aircraft, comprising:

a) an air inlet;

b) an exhaust port;

c) a slide valve connected to said air inlet and said exhaust port;

d) first and second molecular sieve beds each having an inlet connected to said slide valve and an outlet to said cabin; and

e) a controller for operating said slide valve over successive control periods at high altitudes according to a duty cycle for alternately pressurizing and flushing said first molecular sieve bed and a reciprocal of said duty cycle for alternately flushing and pressurizing said second molecular sieve bed to generate oxygen enriched product gas, said duty cycle including time periods having a length for said first molecular sieve bed and a time period for the second molecular sieve bed which is a reciprocal of the length of the time period for said first molecular sieve bed, said controller controlling said slide valve by adjusting said duty cycle and said reciprocal duty cycle during every second one of said successive control periods to change the time period of the first molecular sieve bed for pressurizing relative to said flushing of said first molecular sieve bed and to change the time period of the second molecular sieve bed flushing relative to said pressurizing of said second molecular sieve bed, thereby changing the concentration of oxygen in said product gas, such that water vapor is purged from said first and second molecular sieve beds after pressurizing thereof.

10. The aircraft oxygen system of claim 9, further comprising an oxygen sensor for measuring oxygen concentration of said product gas produced by said first and second molecular sieve beds and communicating said oxygen concentration to said controller for controlling said duty cycle and said reciprocal duty cycle.

11. The aircraft oxygen system of claim 10, further comprising a built-in-test system for applying ambient air to said oxygen sensor for a first predetermined time period, comparing the oxygen concentration in the ambient air detected by said sensor to a predetermined threshold value and in the event said oxygen concentration is not below said predetermined threshold value then activating an alarm to indicate malfunction of said sensor.

12. The aircraft oxygen system of claim 11, further comprising an oxygen concentrator performance check system for applying a predetermined flow of said product gas from said first and second molecular sieve beds for a further predetermined time period, comparing the oxygen concentration of said product gas at said outlet detected by said sensor to a further predetermined threshold value and in the event said oxygen concentration is not above said further predetermined threshold value then activating an alarm to indicate malfunction of said molecular sieve beds.

13. The aircraft oxygen system of claim 9, wherein said slide valve is connected to a pair of opposing air cylinders which are alternately pressurized and vented by a pair of pilot operated solenoid valves connected to said controller, such that when a first one of said cylinders is pressurized the other one of said cylinders is vented and said slide valve is pushed in a first direction for pressurizing said first molecular sieve bed and flushing said second molecular sieve bed and when the other one of said cylinders is pressurized the first one of said cylinders is vented and said slide valve is pushed in an opposite direction for pressurizing said second molecular sieve bed and flushing said first molecular sieve bed.

14. The system of claim 9, wherein the time period for pressurizing of the first molecular sieve bed is changed to a longer time period.

15. The system of claim 9, wherein the time period for pressurizing of the first molecular sieve bed is changed to a shorter time period.

16. The system of claim 9, wherein the time period for pressurizing is shortened when the oxygen concentration of the product gas reaches a predetermined minimum level.

17. The system of claim 9, wherein the time period for flushing the first molecular sieve bed is lengthened when the oxygen concentration of the product gas reaches a predetermined maximum level.