Dehumidifier quilt systems and methods
A method for dehumidifying a perforated acoustic skin includes disposing a sheet of material over a perforated acoustic skin, sealing a periphery of the sheet of material to the perforated acoustic skin to form a cavity between the sheet of material and the perforated acoustic skin, disposing at least one dehumidifier in fluid communication with the cavity, and activating the dehumidifier to remove moist air from a core of the perforated acoustic skin. The dehumidifier(s) may be mounted to the sheet of material.
1. A method for dehumidifying a perforated acoustic skin, the method comprising:
disposing a sheet of material over the perforated acoustic skin, the perforated acoustic skin comprising a plurality of perforations in fluid communication with a core of the perforated acoustic skin;
sealing a periphery of the sheet of material to the perforated acoustic skin to form a cavity between the sheet of material and the perforated acoustic skin;
disposing a dehumidifier in fluid communication with the cavity, the dehumidifier comprises at least one of a refrigeration dehumidifier or an absorption/adsorption dehumidifier;
activating the dehumidifier to remove moist air from the core; and
removing the sheet of material from the perforated acoustic skin before a subsequent flight of an aircraft upon which the perforated acoustic skin is located.
2. The method of claim 1 , wherein the perforated acoustic skin is located on an aircraft nacelle.
3. The method of claim 1 , further comprising detecting a humidity level within the cavity.
4. The method of claim 1 , further comprising detecting a first humidity level above a first predetermined threshold, wherein the activating the dehumidifier is in response to the detecting the first humidity level.
5. The method of claim 4 , further comprising:
detecting a second humidity level below a second predetermined threshold; and
deactivating the dehumidifier in response to the detecting the second humidity level.
6. The method of claim 1 , further comprising routing a condensed moisture to a location located externally from an aircraft nacelle.
7. The method of claim 1 , wherein the sheet of material comprises a water repellant material.
8. The method of claim 1 , wherein the sheet of material comprises a first surface opposing a second surface, and a seal located on the second surface and extending around a periphery of the sheet of material.
9. The method of claim 8 , wherein the least one dehumidifier is in fluid communication with the second surface.
10. The method of claim 9 , wherein the at least one dehumidifier is configured to be sealed from the first surface with the seal.
11. The method of claim 8 , wherein the sheet of material comprises at least one of a plastic film or a tightly woven fabric.
12. The method of claim 8 , wherein the seal comprises an adhesive.
13. The method of claim 6 , wherein the condensed moisture is routed to the location located externally from the aircraft nacelle via an outlet tube extending from the dehumidifier.
14. The method of claim 8 , wherein the at least one dehumidifier is mounted to the sheet of material.
15. The method of claim 4 , wherein the first humidity level is detected with a humidity sensor in electronic communication with the dehumidifier.
16. The method of claim 15 , wherein the activating the dehumidifier is performed by a controller in electronic communication with the dehumidifier.
17. The method of claim 1 , wherein the method is performed between flights of the aircraft while the aircraft is stationary on a ground surface.
18. The method of claim 1 , further comprising disposing the dehumidifier in the cavity.