Aircraft humidifier

Abstract

An aircraft humidifier is engineered as a stand-alone, fully integrated aircraft humidifier that is suitable for providing uniform, non-wetting humidified air disbursed by the aircraft humidifier into ambient air to increase the relative humidity in low humidity environments such as aircraft interiors, including cockpits, cabins, crew rests, cargo holds, and lavatories as well as any other enclosed areas.

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: 
     
         1 . An aircraft humidifier comprising:
 a water filtration system that is suitable to produce filtered water without freezing, the water filtration system operating by static water pressure from an aircraft and including stages selected from a group consisting essentially of reverse osmosis and deionization;   a filtering relay coupled to the water filtration system; and   a duct that is capable of receiving atomized water droplets formed from the filtered water and compressed air to communicate the atomized water droplets to ambient air, the duct including a mouth, throat, neck, and a mix joint to receive the atomized water droplets, which together communicate the atomized water droplets to a chute, C-joint, and canal, which together in turn communicate the atomized water droplets to the ambient air through a posterior air outlet while evaporating remaining atomized water droplets inside the duct.   
     
     
         2 . The aircraft humidifier of  claim 1 , wherein the duct further includes an air cavity and an anterior air inlet, which communicates air through the air cavity into the mix joint, the air cavity including a fan. 
     
     
         3 . The aircraft humidifier of  claim 2 , further comprising a compressor which compresses air to produce the compressed air. 
     
     
         4 . The aircraft humidifier of  claim 2 , further comprising a compressing relay which is coupled to the compressor which compresses air to produce the compressed air. 
     
     
         5 . The aircraft humidifier of  claim 4 , further comprising a pressurized air tank for storing the compressed air produced by the compressor. 
     
     
         6 . The aircraft humidifier of  claim 5 , further comprising a valve which has a capacity to receive the filtered water and communicate the filtered water. 
     
     
         7 . The aircraft humidifier of  claim 6 , further comprising a valve relay which is coupled to the valve. 
     
     
         8 . The aircraft humidifier of  claim 7 , further comprising a nozzle which is suitable for receiving the filtered water from the valve and the compressed air from the compressor, the nozzle communicating the atomized water droplets to the duct. 
     
     
         9 . The aircraft humidifier of  claim 8 , further comprising a sump coupled to the duct, which is capable of collecting moisture leaking from the duct. 
     
     
         10 . The aircraft humidifier of  claim 9 , further comprising a sump moisture sensor coupled to the sump, which has a capacity to detect moisture and communicate such a detection. 
     
     
         11 . The aircraft humidifier of  claim 10 , further comprising a water recycle line coupled to the sump, which is suitable for communicating moisture from the sump back to the water filter system. 
     
     
         12 . An aircraft humidifier comprising:
 a water filtration system that is suitable to produce filtered water without freezing, the water filtration system operating by static water pressure from an aircraft and including stages selected from a group consisting essentially of reverse osmosis and deionization; and   a duct that is capable of receiving atomized water droplets formed from the filtered water and compressed air to communicate the atomized water droplets to ambient air, the duct including a spiral curvilinear passage in its internal surfaces, a portion of which is corrugated to agitate the evaporation of atomized water droplets, the spiral curvilinear passage winding around a center and gradually receding from or approaching the center.   
     
     
         13 . The aircraft humidifier of  claim 12 , wherein the duct further includes an air cavity which includes a fan. 
     
     
         14 . The aircraft humidifier of  claim 13 , further comprising a compressor which compresses air to produce the compressed air. 
     
     
         15 . The aircraft humidifier of  claim 14 , further comprising a compressing relay which is coupled to the compressor which compresses air to produce the compressed air. 
     
     
         16 . The aircraft humidifier of  claim 15 , further comprising a pressurized air tank for storing the compressed air produced by the compressor. 
     
     
         17 . The aircraft humidifier of  claim 16 , further comprising a valve which has a capacity to receive the filtered water and communicate the filtered water. 
     
     
         18 . The aircraft humidifier of  claim 17 , further comprising a valve relay which is coupled to the valve. 
     
     
         19 . The aircraft humidifier of  claim 18 , further comprising a nozzle which is suitable for receiving the filtered water from the valve and the compressed air from the compressor, the nozzle communicating the atomized water droplets to the duct. 
     
     
         20 . The aircraft humidifier of  claim 19 , further comprising an AC power isolator coupled to the filtering relay and the compressing relay.