Low power nitrogen enriched air generation system

• US 6,913,636 B2
• Filed: 12/17/2002
• Issued: 07/05/2005
• Est. Priority Date: 12/17/2002
• Status: Expired due to Term

• Current Assignee: Hamilton Sundstrand Corporation (Rtx Corporation)
• Original Assignee: Hamilton Sundstrand Corporation (Rtx Corporation)
• Inventors: Defrancesco, Gregory, Hipsky, Harold W., Zywiak, Thomas
• Primary Examiner(s): Spitzer, Robert H.
• Application Number:
  US10/322,015
• Publication Number:
  US 20040112220A1
• Time in Patent Office: 931 Days
• Field of Search: 95/8, 95/14, 95/15, 95/17, 95/19, 95/39, 95/41, 95/54, 951/30, 951/38, 96/4, 96 7- 9, 961/08, 96130-133, 961/38
• US Class Current: 95/8
• CPC Class Codes: A62B 7/14 for high-altitude aircraft
• CPC Class Codes: B64D 2013/0677 comprising on board oxygen generator systems
• 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

Abstract

An inerting system provides air with reduced oxygen content by flowing and directing air through an air separation module. Optimal working pressure for the air separation module is obtained with two compressors. A first compressor elevates air from the aircraft cabin to a second pressure. The second pressure is at an intermediate level below the working pressure of the air separation module. A second compressor elevates air from the second pressure to the working pressure. The second compressor is driven by air that is exhausted through a turbine. The pressure difference between air at the working pressure and air required by the fuel distribution system is used to power the turbine and drive the second compressor.

Claims

1. A method of removing oxygen from air within a fuel distribution system comprising the steps of:

a. compressing air from a first pressure to a second pressure higher than the first pressure with a first compressor;

b. compressing air at said second pressure to a third pressure higher than said second pressure with a second compressor;

c. removing oxygen from said air with an air separation module;

d. driving said second compressor with energy recovered from said air at said third pressure by a turbine receiving air at said third pressure at an inlet and exhausting air at a fourth pressure lower than said third pressure to the fuel distribution system.

2. The method of claim 1, further including the step of cooling air exhausted from said first compressor with a heat exchanger.

3. The method of claim 1, including the step of filtering contaminants from said air before removing oxygen.

4. The method of claim 1, wherein said third pressure is a pressure greater than a pressure capacity of said first compressor.

5. The method of claim 1, wherein said third pressure is an optimum working pressure for said air separation module.

6. An inerting system for a fuel distribution system for reducing combustibility by reducing air oxygen content comprising:

a first compressor drawing in air at a first pressure and exhausting air at a second pressure greater than said first pressure,

a second compressor driven by a turbine drawing air from said first compressor at said second pressure and exhausting air at a third pressure greater than said second pressure; and

an air separation module for removing oxygen from said air, said air separation module receiving air at said third pressure from said second compressor;

said turbine including an inlet and an outlet, said inlet receiving air at said third pressure and said outlet exhausting oxygen depleted air at a fourth pressure lower than said third pressure to the fuel distribution system.

7. The system of claim 6, including a motor for driving said first compressor.

8. The system of claim 6, including a first heat exchanger for cooling air exhausted from said first compressor.

9. The system of claim 6, including a second heat exchanger for cooling air exhausted from said second compressor.

10. The system of claim 6, including a water collection device for removing water from air exhausted from said second compressor.

11. The system of claim 6, including a filter for collecting contaminates in said air before entering said air separation module.

12. The system of claim 6, including a third heat exchanger for heating air before entering said turbine.

13. The system of claim 6, wherein the fuel distribution system is a fuel tank, said system replacing air within said fuel tank with oxygen depleted air to reduce combustibility.

14. The system of claim 6, wherein said turbine is powered by air at said third pressure to drive said second compressor increasing the pressure of air entering said air separation module to optimize oxygen removal.

15. The system of claim 6, including a controller, and an electrically actuated control valve for controlling air flow.

16. The system of claim 15, including a bypass circuit for bypassing air around said second heat exchanger in response to a temperature of said air being within a predetermined range.

17. The system of claim 15, including an oxygen sensor in communication with said controller for monitoring oxygen content exiting said air separation module.

18. The system of claim 15, including a flow measurement device for measuring airflow exhausted from said turbine to said fuel distribution system.