Aircraft aircrew life support systems

• US 4,919,124 A
• Filed: 12/12/1988
• Issued: 04/24/1990
• Est. Priority Date: 12/18/1987
• Status: Expired due to Fees

• Current Assignee: Honeywell Normalair-Garrett Ltd. (Honeywell International Inc.)
• Original Assignee: Honeywell Normalair-Garrett Ltd. (Honeywell International Inc.)
• Inventors: Cassidy, Ronald F., Stevenson, George F.
• Primary Examiner(s): Burr, Edgar S.
• Assistant Examiner(s): Lewis, Aaron J.
• Application Number:
  US07/282,571
• Time in Patent Office: 498 Days
• Field of Search: 128/202.26, 128/205.11, 128/205.24
• US Class Current: 128/202.26
• CPC Class Codes: A62B 7/14 for high-altitude aircraft
• CPC Class Codes: A62B 9/022 Breathing demand regulators SCUBA diving regulators B63C11/22
• CPC Class Codes: B64D 13/00 Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space , or structural parts of the aircraft treatment rooms with artificial climate for medical purposes A61G10/02; respiratory apparatus in general A62B; for vehicles in general B60H

Abstract

An aircrew life support system has an on-board oxygen generating system (OBOGS) connected for delivering oxygen-enriched product gas to a breathing demand regulator and a plenum storage container. The concentration of oxygen in the product gas is sensed by a gas concentration sensor which supplies signals to an electronic control unit (ECU). The ECU outputs signals for switching a control valve which controls product gas to be delivered to the regulator from either the OBOGS or the storage container. The ECU also outputs signals to a charge valve which is opened to allow product gas from the OBOGS to charge the storage container when product gas enriched with oxygen above a predetermined concentration is being delivered by the OBOGS and there is excess capacity over the demand requirements at the regulator. The breathing demand regulator provides for mixing of the OBOGS product gas or of the stored gas with cabin air to provide a breathing gas matched to physiological requirements under all operational conditions, both normal and emergency and, especially to provide for long-term sea level breathing from the stored gas when the OBOGS in not operating.

Claims

1. An aircraft aircrew life support system comprising an onboard oxygen generating system (OBOGS) for delivering oxygen-enriched product gas, breathing demand regulator means connected for receiving oxygen-enriched product gas, said regulator means including means for permitting aircraft cabin air to enter said regulator means and mix with said OBOGS product gas in one operating mode of said regulator means and mode switching means for switching said regulator means betwen a mode in which undiluted OBOGS product gas is delivered in response to breathing demands and a mode in which OBOGS product gas diluted with aircraft cabin air is delivered in response to breathing demands, plenum storage means connected for receiving OBOGS product gas and for supplying said gas to said regulator means, gas concentration sensor means connected for sensing concentration of oxygen in product gas delivered by said OBOGS and adapted to output oxygen concentration signals, an OBOGS product gas supply valve adapted for controlling said OBOGS product gas to be delivered to said regulator means from said OBOGS or said plenum storage means, a plenum storage charge valve adapted for controlling charging of said plenum storage means by said OBOGS product gas, and electronic control means connected for receiving oxygen concentration signals form said gas concentration sensor means and mode signals from said mode switching means and adapated to compute said signals and output control signals to said OBOGS product gas supply valve and said pelnum storage charge valve, whereby when oxygen concentration in product gas delivered by said OBOGS is sensed to have fallen below a predetermined minimum concentration percentage or on failure of OBOGS product gas supply said product gas supply valve is switched to inhibit the flow of product gas from the OBOGS to said regulator and to connect said regulator means with said plenum storage means, and when oxygen concentration is said OBOGS product gas is sensed to be above the predetermined minimum concentration percentage and said regulator means is in a mode in which OBOGS product gas diluted with aircraft cabin air is being delivered in response to breathing demands said plenum storage charge valve is switched to permit OBOGS product gas to charge said plenum storage means.

2. A system as claimed in claim 1, wherein the control valve and the charge valve are solenoid operated valves having their solenoids connected for receiving signals from an electronic control means.

3. A system as claimed in claim 2, wherein the electronic control means comprises a microprocessor.

4. A system as claimed in claim 3, wherein the microprocessor is connected for receiving signals representative of system ambient and system inlet conditions, and breathing demand flow rate.

5. A system as claimed in claim 3, wherein the microprocessor is programmed with a mathematical model of the gas concentration process.

6. A system as claimed in claim 1, wherein the gas concentration sensor means comprises a flueric partial pressure sensor located in a pressurised chamber which is held at substantially constant pressure irrespective of aircraft operating altitude.

7. A system as claimed in claim 1, wherein the OBOGS comprises two molecular sieve beds and a surge chamber for storing a volume of product gas delivered by the sieve beds.

8. A system as claimed in claim 7, wherein the two sieve beds are provided in concentric sieve beds which together with the surge chamber are housed internally of the plenum storage means.