IP Library Granted Patent US 7,264,647
Granted Patent B2
US 7,264,647 · App. 10/850,656 · Granted Sep 4, 2007

Device for enriching air with oxygen in an aircraft, and a method for operating the device

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Quick Facts
Patent No.
US 7,264,647
App. No.
10/850,656
Granted
Sep 4, 2007
Kind
B2
Abstract

A device for enriching air with oxygen in an aircraft, and a method for operating the device provides product gas enrichment with oxygen with minimum requirements. An oxygen measurement apparatus analyzing the product gas flow as well as a throughput sensor are provided in combination with a change-over device. A flow connection to an outlet channel is created in a first switch position, and a flow connection to a consumer conduit exists in a second switch position. A device for producing a change-over signal from the first switch position to the second switch position is provided if the determined oxygen output as a product of the product gas flow and the oxygen concentration has reached or exceeded a predefined threshold value.

Claims (38)

1. A device for enriching air with oxygen in an aircraft, the device comprising in series sequence:

a high-pressure source for dispensing air;

a water separator;

two parallel arranged molecular sieve beds for the alternate adsorption and desorption of nitrogen;

a flow transfer means for permitting a rinsing gas flow between the molecular sieve beds;

an oxygen measurement apparatus analyzing the product gas flow enriched with oxygen;

a throughput sensor for detecting the product gas flow; and

a change-over device for the product gas flow exiting from the molecular sieve bed, wherein in a first switch position of the change-over device a flow connection to an outlet channel is created for removing product gas flow with an insufficient oxygen output, and in a second switch position there exists a flow connection to a consumer conduit, and wherein there are provided means for producing a change-over signal from the first to the second switch position upon exceeding a predefined threshold value for the oxygen output, said oxygen output being a product of the oxygen concentration and the product gas flow.

2. A device according to claim 1 , wherein the outlet channel comprise a throttle location.

3. A device according to claim 1 , wherein the outlet channel provides a common flow channel for the product gas flow and the rinsing gas flow.

4. A device according to claim 2 , wherein the outlet channel provides a common flow channel for the product gas flow and the rinsing gas flow.

5. A device according to claim 1 , wherein the outlet channel is adapted to accommodate the condensation water which is separated by the water separator.

6. A device according to claim 2 , wherein the outlet channel is adapted to accommodate the condensation water which is separated by the water separator.

7. A device according to claim 3 , wherein the outlet channel is adapted to accommodate the condensation water which is separated by the water separator.

8. A method for operating a device for enriching air with oxygen in an aircraft, the method comprises the steps of:

providing in series sequence a high-pressure source for dispensing air, a water separator, two parallel arranged molecular sieve beds for the alternate adsorption and desorption of nitrogen and a flow transfer means permitting a rinsing gas flow between the molecular sieve beds;

analyzing a product gas flow which exits from the molecular sieve bed located in the adsorption phase, with an oxygen measurement apparatus;

detecting the product gas flow with a throughput sensor;

detecting the oxygen output;

leading away the product gas into an outlet channel during a readiness phase with which the measured oxygen output lies below a predefined threshold value for the oxygen output;

converting from the readiness phase to an operation phase upon exceeding a predefined threshold value for the oxygen output, said oxygen output being formed as a product of the oxygen concentration and the product gas flow; and

supplying the product gas to a consumer conduit during an operation phase with which the measured oxygen output reaches or exceeds the predefined threshold value, said oxygen output being a product of the oxygen concentration and the product gas flow.

9. A method according to claim 8 , further comprising providing the outlet channel with a throttle location.

10. A method according to claim 8 , further comprising designing the outlet channel as a common flow channel for the product gas flow and the rinsing gas flow.

11. A method according to claim 9 , further comprising designing the outlet channel as a common flow channel for the product gas flow and the rinsing gas flow.

12. A method according to claim 8 , further comprising leading the condensation water separated in the water separator into the outlet channel.

13. A method according to claim 9 , further comprising leading the condensation water separated in the water separator into the outlet channel.

14. A device for enriching air with oxygen in an aircraft, the device comprising:

a high-pressure source for dispensing air;

a water separator;

two parallel arranged molecular sieve beds;

a flow transfer means for permitting a rinsing gas flow between the molecular sieve beds;

an oxygen measurement apparatus for detecting the oxygen output of the product gas flow enriched with oxygen;

a throughput sensor detecting the product gas flow;

a change-over device for product gas flow exiting from the molecular sieve bed, said change-over device switching between an outlet channel flow position for discarding product flow gas with insufficient oxygen output and a consumer conduit flow connection position; and

a control means for controlling said change-over device position whereby said control means compares the oxygen output of the product gas flow to a preset threshold value, said control means sending a change-over signal to switch said change-over device to the consumer conduit flow connection position upon the oxygen output exceeding the predefined threshold value.

15. A device according to claim 14 , wherein the outlet channel comprise a throttle location.

16. A device according to claim 14 , wherein the outlet channel provides a common flow channel for the product gas flow and the rinsing gas flow.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Jan 25, 2019
From: JP MORGAN CHASE BANK, N.A
To: B/E AEROSPACE, INC.
Reel/Frame 049209/0619 →
SECURITY INTEREST Recorded Mar 10, 2015
From: B/E AEROSPACE, INC.
To: JPMORGAN CHASE BANK, N.A.
Reel/Frame 035176/0493 →
RELEASE OF SECURITY INTEREST Recorded Jan 23, 2015
From: JP MORGAN CHASE BANK, N.A.
To: B/E AEROSPACE, INC.
Reel/Frame 034805/0718 →