Environmental control system and methods of operating same

Patent metadata

Field	Value
Publication number	US-9889939-B2
Application number	US-201213490270-A
Country	US
Kind code	B2
Filing date	Jun 6, 2012
Priority date	Jun 6, 2012
Publication date	Feb 13, 2018
Grant date	Feb 13, 2018

Abstract

An environmental control system includes an air supply system coupled to an aircraft. The air supply system includes an external air supply device coupled to the aircraft and a supply duct coupled in flow communication to the external air supply device. An air supply outlet is coupled in flow communication to the supply duct and in flow communication with an occupancy zone and/or a floor distribution section. An air recirculation system is coupled to the floor distribution section. The air recirculation system includes a recirculation supply device coupled to the aircraft and a recirculation duct coupled in flow communication to the recirculated supply device and coupled to the floor distribution section. A recirculation outlet is coupled in flow communication to the recirculation duct and in flow communication with the recirculation zone and/or the floor distribution section.

First claim

What is claimed is:

1. An aircraft comprising:
a fuselage comprising a passenger area and a cargo area, said passenger area having an occupancy zone including locations where passengers are seated and a recirculation zone adjacent to said occupancy zone and including locations where passengers are not seated and does not overlap with said occupancy zone;
a floor distribution section coupled in flow communication to said occupancy zone and said recirculation zone, and defined between an upper floor and a lower floor in said fuselage, wherein said upper floor at least partially defines said passenger area and said lower floor at least partially defines said cargo area;
an air supply system coupled to said aircraft, said air supply system comprising:
an air supply device coupled to said fuselage and configured to supply outside air to said fuselage;
a supply duct coupled in flow communication to said air supply device and extending through said cargo area and into said floor distribution section; and
an air supply outlet coupled in flow communication to said supply duct and in flow communication with said occupancy zone via said floor distribution section, said air supply outlet defined in said upper floor for channeling a flow of outside air supplied by said air supply device into said occupancy zone such that the locations where passengers are seated receive only the flow of outside air; and

an air recirculation system coupled to said aircraft, said air recirculation system comprising:
a recirculation supply device positioned in said cargo area, said recirculation supply device configured to supply recirculated air to said passenger area;
a recirculation duct coupled in flow communication to said recirculated supply device and extending from said cargo area into said floor distribution section; and
a recirculation outlet coupled in flow communication to said recirculation duct and in flow communication with said recirculation zone via said floor distribution section, said recirculation outlet defined in said upper floor for channeling a flow of recirculated air supplied by said recirculation supply device into said recirculation zone such that the flow of recirculated air is channeled into said passenger area only at locations where passengers are not seated.

2. The aircraft of claim 1 wherein said air supply system and said recirculation system are coupled in flow communication to the floor distribution section.

3. The aircraft of claim 2 further comprising a mixer coupled to the floor distribution section.

4. The aircraft of claim 1 further comprising a mixing plenum coupled to the floor distribution section, said mixing plenum is configured to mix external air mass from said air supply system with recirculated air mass from said air recirculation system.

5. The aircraft of claim 4 further comprising a mixer coupled to said mixing plenum.

6. The aircraft of claim 4 wherein said supply duct and said recirculation duct are coupled in flow communication to said mixing plenum.

7. The aircraft of claim 4 further comprising a plurality of ducts coupled in flow communication to said mixing plenum and to said occupancy zone, said plurality of ducts configured to channel a mixed air mass into said occupancy zone.

8. The aircraft of claim 7 further comprising a flow control device coupled to at least one duct of said plurality of ducts.

9. The aircraft of claim 1 further comprising an auxiliary duct coupled in flow communication to said recirculation duct and comprising a flow control device coupled in flow communication to said auxiliary duct.

10. The aircraft of claim 1 further comprising a cargo zone, an exhaust zone and an airflow device coupled in flow communication to said cargo zone and said exhaust zone.

11. An environmental control system for use with an aircraft having a floor distribution section that is coupled in flow communication to an occupancy zone including locations where passengers are seated and a recirculation zone adjacent to the occupancy zone and including locations where passengers are not seated and does not overlap with the occupancy zone, the floor distribution section defined between an upper floor and a lower floor of the aircraft, wherein the upper floor at least partially defines a passenger area in the aircraft and the lower floor at least partially defines a cargo area, said environmental control system comprising:
an air supply system coupled to the aircraft, the air supply system comprising:
an air supply device coupled to and configured to supply outside air to the aircraft;
a supply duct coupled in flow communication to said air supply device and extending through said cargo area and into the floor distribution section; and
an air supply outlet coupled in flow communication to said supply duct and in flow communication with the occupancy zone via the floor distribution section, said air supply outlet defined in said upper floor for channeling a flow of outside air supplied by said air supply device into said occupancy zone such that the locations where passengers are seated receive only the flow of outside air; and

an air recirculation system coupled to the aircraft, the air recirculation system comprising:
a recirculation supply device positioned in said cargo area, said recirculation supply device configured to receive exhaust air exhausted from said passenger area through an upper portion of said aircraft and supply recirculated air to said passenger area;
a recirculation duct coupled in flow communication to said recirculated supply device and extending from said cargo area into said floor distribution section; and
a recirculation outlet coupled in flow communication to said recirculation duct and in flow communication with the recirculation zone via the floor distribution section, said recirculation outlet defined in said upper floor for channeling a flow of recirculated air supplied by said recirculation supply device into said recirculation zone such that the flow of recirculated air is channeled into said passenger area only at locations where passengers are not seated.

12. The environmental control system of claim 11 further comprising a heat exchanger coupled to said recirculation duct.

13. The environmental control system of claim 11 further comprising a controller operatively coupled to said air supply system and said air recirculation system.

14. The environmental control system of claim 11 wherein said air supply outlet is coupled in flow communication to the occupancy zone and said recirculation outlet is coupled in flow communication with the recirculation zone.

15. The environmental control system of claim 11 wherein said air supply system and said recirculation system are coupled in flow communication to the floor distribution section.

16. The environmental control system of claim 11 further comprising a mixing plenum coupled to the floor distribution section, said mixing plenum is configured to mix external air mass from said air supply system with recirculated air mass from said air recirculation system.

17. The environmental control system of claim 11 further comprising a plurality of ducts coupled in flow communication to said mixing plenum and to said occupancy zone, said plurality of ducts configured to channel a mixed air mass into said occupancy zone.

18. A method of controlling airflow within an aircraft having a floor distribution section that is coupled in fluid communication to an occupancy zone including locations where passengers are seated, a recirculation zone adjacen

Assignees

• Zhang Wei
• Space David R
• Boeing Co

Inventors

• Zhang Wei
• Space David R

Classifications

• Y02T50/56

  Cross-Sectional Technologies · mapped topic

• B64D2013/0688

  with means for recirculating cabin air · CPC title

• B64D13/08 Primary

  the air being heated or cooled · CPC title

• Y02T50/50

  On board measures aiming to increase energy efficiency · CPC title