Combustibly inert air supply system and method

• US 4,378,920 A
• Filed: 07/15/1980
• Issued: 04/05/1983
• Est. Priority Date: 07/15/1980
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Runnels, Joe N., Fagerlund, Kenneth R.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US06/169,140
• Time in Patent Office: 994 Days
• Field of Search: 244/135 A, 244/129.2, 137/8, 137/113, 137/209, 137/206, 137/207, 137/599, 137/599.1, 137/568, 137/569, 222/399, 222/61, 60/39.12, 55/21, 55/66, 55/158, 55/57, 55/58, 55/385 R, 55/518, 55/431, 55/468, 55/267, 220/88 B, 220/88 R, 169/45
• US Class Current: 244/135.00R
• CPC Class Codes: B64D 37/32 Safety measures not otherwise provided for, e.g. preventing explosive conditions extinguishing or preventing fires in aircraft A62C
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 137/3127 With gas maintenance or application
• CPC Class Codes: Y10T 137/86043 Reserve or surge receiver

Abstract

Compressed air is directed through an inert gas generator which removes oxygen to produce a nitrogen enriched, combustibly inert air or gas. The converter is sized to only meet the relatively low flow rate requirements of the system during which times the combustibly inert air or gas is delivered directly to a utilization site. The system further includes a high pressure storage container in which a pressurized precharge of the combustibly inert air or gas is stored. Combustibly inert air is released from such high pressure storage container for providing the higher flow rate requirements of the system. The system may be used aboard an aircraft for inerting fuel tanks. It may include a separate compressor for filling the high pressure storage container.

Claims

1. A combustibly inert gas supply system, comprising:

a first source of combustibly inert gas comprising an inert gas generator, said generator including an inlet for compressed atmospheric air, an outlet, and flow-through means between the inlet and outlet for converting the compressed air into combustibly inert gas;

first conduit means for delivering compressed air to the inlet;

second conduit means for delivering inert gas to a utilization site;

a second source of combustibly inert gas comprising storage means for storing inert gas at a high pressure;

third conduit means leading from the outlet to the second conduit means;

fourth conduit means leading from the storage means to the second conduit means;

fifth conduit means leading from the third conduit means to the fourth conduit means, and including a compressor for charging the high pressure storage means;

regulator means for switching between said first and second sources and for supplying said second source from said first source.

2. The system of claim 1, said regulator means comprising first valve means in the second and fourth conduit means, for preventing forward flow though said second conduit means and reverse flow through said fourth conduit means, during operation of the compressor to supply said second source, and second valve means in the third and fifth conduit means, for preventing reverse flow through the third conduit means to the generator and reverse flow through the fifth conduit means to the compressor, during periods of discharge from the high pressure storage means.

4. The inert gas supply system of claims 1 or 3 wherein said utilization site is a fuel tank.

5. The inert gas supply system of claims 1 or 3 further comprising at least one branch conduit means leading from said storage means to at least one further utilization site.

6. The system of claims 1 or 3, wherein the inert gas generator is a hollow fiber generator.

7. The system of claims 1 or 7, wherein the inert gas generator is a molecular sieve generator.

3. A combustibly inert gas supply system for use aboard an aircraft which includes at least one gas turbine engine having a first compressor, comprising:

a first source of combustibly inert gas comprising an inert gas generator, said generator including an inlet for compressed air, an outlet for combustibly inert air, and flow-through means between the inlet and outlet for converting the compressed air into combustibly inert gas;

first conduit means for delivering compressed air to the inlet;

second conduit means for delivering inert gas to a utilization site;

a second source of combustibly inert gas comprising storage means for storing inert gas at a high pressure;

third conduit means leading from the outlet to the second conduit means;

fourth conduit means leading from the storage means to the second conduit means;

fifth conduit means leading from the third conduit means to the fourth conduit means, and including a second compressor for charging the high pressure storage means;

turbine means drivingly connected to the second compressor;

sixth conduit means for delivering compressed atmospheric air to the turbine means for powering same;

seventh conduit means for delivering compressed air from the first compressor to both the first conduit means and the sixth conduit means;

regulator means for switching between said first and second sources in dependence upon the inert gas flow demand of the utilization site, and for supplying said second source from said first source.

8. A method of supplying combustibly inert gas at both low and high flow rates with a substantial saving in equipment weight, comprising the steps of:

providing a noncombusting, inert gas generator sized to meet low system flow rate demand;

using said inert gas generator to produce a nitrogen enriched, combustibly inert gas by withdrawing oxygen from flowing, compressed, atmospheric air;

delivering the inert gas, as it is produced by the generator, directly to the utilization site during system flow rate demand periods that are less than or equal to said low system flow rate;

providing at least one high pressure inert gas storage container;

compressing some of the inert gas from the generator and storing it in the storage container at a high pressure; and

selectively delivering inert gas to the utilization site from the container during system flow rate demand periods that are higher than said low system flow rate.

9. The method of claim 8, wherein said utilization site is a fuel tank.

10. The method of claim 8, wherein the inert gas generator is a hollow fiber generator.

11. The method of claim 8, wherein the inert gas generator is a molecular sieve generator.

12. The method of claim 9, further comprising sensing said higher flow rate demand at the fuel tank and in response to such demand delivering inert gas from the container to the fuel tank at the required flow rate.