Airflow management in cabin of aircraft
Cabin air is managed in the aircraft as a function of the minimum requirements for defined air quality needs, temperature control needs, and cabin pressurization needs. Airflow may be varied dynamically as a function of aircraft or cabin altitude, and the minimum requirements for airflow may be determined in real time so as to dynamically set an airflow schedule.
1. A method for controlling airflow in an aircraft, the method comprising:
obtaining a minimum airflow for attaining a target temperature in the aircraft as a function of altitude of the aircraft or cabin;
obtaining a minimum airflow for attaining a target cabin pressure in the aircraft as a function of the altitude of the aircraft or cabin;
obtaining a minimum airflow for attaining a target ratio of fresh outside ambient air to recirculated air, the ratio of fresh outside ambient air to recirculated air defining an air quality for the aircraft;
when the minimum airflow for attaining the target temperature is greater than the minimum airflow for attaining the target cabin pressure and the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target temperature;
when the minimum airflow for attaining the target cabin pressure is greater than the minimum airflow for attaining the target temperature and the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target cabin pressure; and
when the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air is greater than the minimum airflow for attaining the target cabin pressure and the minimum airflow for attaining the target temperature, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air.
2. The method of claim 1 , further comprising:
determining a current altitude of the aircraft or cabin; and
varying the airflow in the cabin as a function of the current altitude.
3. The method of claim 1 , wherein obtaining a minimum airflow for attaining a target temperature comprises:
obtaining a minimum airflow for heating of the aircraft; and
obtaining a minimum airflow for cooling of the aircraft.
4. The method of claim 1 , wherein obtaining a minimum airflow for attaining a target ratio of fresh outside ambient air to recirculated air comprises determining a minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air using an actual occupancy of the aircraft.
5. The method of claim 1 , wherein obtaining a minimum airflow for attaining the target temperature comprises determining the temperature minimum airflow using atmospheric conditions outside of the aircraft.
6. The method of claim 1 , wherein controlling airflow comprises dynamically setting an airflow schedule using a current aircraft altitude and other parameters obtained in real time.
7. The method of claim 1 , further comprising monitoring the ratio of fresh outside ambient air to recirculated air in the aircraft.
8. The method of claim 7 , further comprising:
detecting a drop in the ratio of fresh outside ambient air to recirculated air below a threshold; and
triggering an alert signal indicative of the drop in the ratio of fresh outside ambient air to recirculated air.
9. The method of claim 8 , further comprising modifying the airflow as a function of the drop in the ratio of fresh outside ambient air to recirculated air.
10. The method of claim 9 , wherein modifying the airflow comprises at least one of shutting down at least one air source, shutting down a recirculation system, turning on a new air source, changing the ratio of fresh air to recirculated air distributed in the aircraft, and reducing a total air flow.
11. A system for controlling airflow in an aircraft, the system comprising:
a memory;
a processor coupled to the memory; and
an application stored on the memory and comprising program code executable by the processor for:
obtaining a minimum airflow for attaining a target temperature in the aircraft as a function of altitude of the aircraft or cabin;
obtaining a minimum airflow for attaining a target cabin pressure in the aircraft as a function of the altitude of the aircraft or cabin;
obtaining a minimum airflow for attaining a target ratio of fresh outside ambient air to recirculated air, the ratio of fresh outside ambient air to recirculated air defining an air quality for the aircraft;
when the minimum airflow for attaining the target temperature is greater than the minimum airflow for attaining the target cabin pressure and the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target temperature;
when the minimum airflow for attaining the target cabin pressure is greater than the minimum airflow for attaining the target temperature and the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target cabin pressure; and
when the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air is greater than the minimum airflow for attaining the target cabin pressure and the minimum airflow for attaining the target temperature, controlling the airflow in the aircraft or cabin to be greater than the minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air.
12. The system of claim 11 , wherein the application further comprises program code executable by the processor for:
determining a current altitude of the aircraft; and
varying the airflow in the cabin as a function of the current altitude.
13. The system of claim 11 , wherein obtaining a minimum airflow for attaining a target temperature comprises:
obtaining a minimum airflow for heating of the aircraft; and
obtaining a minimum airflow for cooling of the aircraft.
14. The system of claim 11 , wherein obtaining a minimum airflow for attaining a target ratio of fresh outside ambient air to recirculated air comprises determining a minimum airflow for attaining the target ratio of fresh outside ambient air to recirculated air using an actual occupancy of the aircraft.
15. The system of claim 11 , wherein obtaining a minimum airflow for attaining the target temperature comprises determining the temperature minimum airflow using atmospheric conditions outside of the aircraft.
16. The system of claim 11 , wherein controlling airflow comprises dynamically setting an airflow schedule using a current aircraft altitude and other parameters obtained in real time.
17. The system of claim 11 , further comprising monitoring the ratio of fresh outside ambient air to recirculated air in the aircraft.
18. The system of claim 17 , wherein the application further comprises program code executable by the processor for:
detecting a drop in the ratio of fresh outside ambient air to recirculated air below a threshold; and
triggering an alert signal indicative of the drop in the ratio of fresh outside ambient air to recirculated air.
19. The system of claim 18 , further comprising modifying the airflow as a function of the drop in the ratio of fresh outside ambient air to recirculated air.
20. The system of claim 19 , wherein modifying the airflow comprises at least one of shutting down at least one air source, shutting down a recirculation system, turning on a new air source, changing the ratio of fresh air to recirculated air distributed in the aircraft, and reducing a total air flow.