Systems and methods for limiting infiltration of cabin air into the flight deck of an aircraft

Patent metadata

Field	Value
Publication number	US-11325712-B2
Application number	US-201816181197-A
Country	US
Kind code	B2
Filing date	Nov 5, 2018
Priority date	Nov 5, 2018
Publication date	May 10, 2022
Grant date	May 10, 2022

Abstract

Systems and methods for limiting infiltration of cabin air into the flight deck of an aircraft, where the systems include at least one upper nozzle disposed adjacent to and above an outer upper edge of a flight deck doorway and directed downwardly, and at least one lower nozzle disposed adjacent to and below an outer lower edge of the flight deck doorway and directed upwardly; a conduit system to deliver air from a flight deck air supply to the upper and lower nozzles; and an airflow controller configured to provide sufficient air flow from the flight deck air supply to the upper and lower nozzles to create directional airstreams across the gaps between the closed flight deck door and the upper and lower edges of the flight deck doorway, so that the airstreams limit infiltration of cabin air into the flight deck via the gaps.

First claim

What is claimed is:

1. A system for limiting infiltration of cabin air from a passenger cabin into a flight deck of an aircraft, comprising:
at least one upper nozzle disposed adjacent to and above an outer upper edge of a flight deck doorway and directed downwardly, and at least one lower nozzle disposed adjacent to and below an outer lower edge of the flight deck doorway and directed upwardly, wherein the flight deck doorway has an inner side facing the flight deck and an outer side facing the passenger cabin, and wherein the at least one upper nozzle and the at least one lower nozzle are adjacent the outer side of the flight deck doorway;
a conduit system configured to deliver air from a flight deck air supply to the upper and lower nozzles; and
an airflow controller configured to provide sufficient air flow from the flight deck air supply to the upper and lower nozzles to create directional airstreams across gaps existing between a closed flight deck door and the upper and lower edges of the flight deck doorway, limiting infiltration of cabin air into the flight deck.

2. The system of claim 1 , wherein the at least one upper nozzle and the at least one lower nozzle are configured so that the directional airstreams they create extend across an entire width of the flight deck doorway.

3. The system of claim 1 , wherein each of the upper and lower nozzles is substantially slot-shaped.

4. The system of claim 3 , wherein the gaps include an upper gap and a lower gap, wherein the at least one upper nozzle is comprised of a single slot disposed along an entire width of the upper gap, and wherein the at least one lower nozzle is comprised of a single slot disposed along an entire width of the lower gap.

5. The system of claim 1 , further comprising air pressure sensors configured to determine a flight deck air pressure measurement and a cabin air pressure measurement for the airflow controller; and the airflow controller is configured to determine a difference in the cabin air pressure and the flight deck air pressure, and from the determined difference to further determine a sufficient amount of air flow to supply from the flight deck air supply to the upper and lower nozzles to limit infiltration of cabin air into the flight deck.

6. The system of claim 5 , wherein the airflow controller is configured to calculate an inflow rate around the flight deck door based upon the difference in air pressure between the cabin and the flight deck; and
the airflow controller is further configured to operate system components to provide a sufficient rate of air flow to the upper and lower nozzles that is at least twice as much as the calculated inflow rate.

7. The system of claim 5 , wherein the airflow controller is configured to measure the difference in cabin air pressure and flight deck air pressure, and vary the air flow to the upper and lower nozzles in response to changes in the difference in cabin air pressure and flight deck air pressure in real time.

8. The system of claim 1 , wherein the airflow controller is configured to provide sufficient air flow to the upper and lower nozzles to establish directional airstreams that flow across the gaps at the upper and lower edges of the flight deck door at a flow rate based on a sensed pressure differential between the flight deck and cabin, to limit cabin air infiltration through the gaps into the flight deck to less than 2% of the flight deck air supply.

9. The system of claim 1 , wherein the conduit system further comprises a variable-speed fan configured to deliver air from the flight deck air supply to the upper and lower nozzles; and the airflow controller is configured to provide the sufficient air flow to the upper and lower nozzles by controlling fan speed.

10. The system of claim 1 , further comprising:
a cabin air pressure sensor;
a flight deck air pressure sensor; and
an air delivery system including the at least one upper nozzle, the at least one lower nozzle, and the conduit system, the air delivery system being configured to deliver air from the flight deck air supply to create air curtains across an upper gap between the outer upper edge of the flight deck doorway and the flight deck door, and across a lower gap between the outer lower edge of the flight deck doorway and the flight deck door; and
wherein the airflow controller includes a processor coupled to the cabin air pressure sensor and the flight deck air pressure sensor, and configured to control the air delivery system; wherein the processor is configured to:
measure a cabin air pressure using the cabin air pressure sensor;
measure a flight deck air pressure using the flight deck air pressure sensor;
calculate a difference between the measured cabin air pressure and the measured flight deck air pressure;
predict an inflow rate of cabin air into the flight deck based upon the calculated air pressure difference; and
create a sufficient air flow from the air delivery system that the air curtains created thereby limit an infiltration of cabin air into the flight deck.

11. The aircraft system of claim 10 , wherein the processor predicts the inflow rate of cabin air into the flight deck using a lookup table correlating the difference between cabin air pressure and flight deck air pressure with an inflow rate of cabin air via the upper gap and the lower gap.

12. The aircraft system of claim 11 , wherein the processor is further configured to create an air flow from the air delivery system that is at least twice the inflow rate of cabin air via the upper gap and lower gap.

13. The aircraft system of claim 10 , wherein the at least one upper nozzle is disposed adjacent to and above the upper gap and is directed downwardly to create the air curtain across the upper gap, and wherein at least one lower nozzle is disposed adjacent to and below the lower gap and is directed upwardly to create the air curtain across the lower gap.

14. The aircraft system of claim 13 , wherein the air delivery system includes a variable-speed fan, and the processor is configured to control the variable-speed fan so that sufficient air is delivered to the at least one upper nozzle and the at least one lower nozzle to limit the infiltration of cabin air into the flight deck.

15. The aircraft system of claim 10 , wherein the processor is configured to create a sufficient air flow from the air delivery system that the resulting air curtains limit the infiltration of cabin air into the flight deck to less than 2% of the flight deck air supply.

16. The aircraft system of claim 10 , further comprising a flight deck particulate sensor coupled to the processor, wherein the processor is configured so that if the flight deck particulate sensor detects increased particulates in the flight deck air supply, the air flow from the air delivery system to the air curtains is increased.

17. The aircraft system of claim 10 , wherein the processor is configured to receive a communication from a particulate sensor located within the passenger cabin that indicates a detection of smoke or specific airborne particles, and the processor is configured to responsively determine a speed for operating a fan of the air delivery system so as to establish an increased airflow rate to create higher speed air curtains to inhibit cabin air infiltration through the upper and lower gaps and into the flight deck.

18. A method of limiting infiltration of cabin air into the flight deck of the aircraft of claim 1 , the method comprising:
measuring a cabin air pressure;
measuring a flight deck air pressure;
determin

Assignees

• Boeing Co

Inventors

• Vandyke Bryce Avery
• Richardson Marcus Karel
• Imada Brian Tatsuo
• Brown Myles
• Loukusa Steven Michael

Classifications

• B64D13/04 Primary

  Automatic control of pressure · CPC title

• F24F2009/007

  using more than one jet or band in the air curtain · CPC title

• F24F9/00 Primary

  Use of air currents for screening, e.g. air curtains · CPC title

• F24F2009/005

  combined with a door · CPC title

• B64D2013/0655

  with zone or personal climate controls · CPC title