Abstract: An environment control system for a body of an aircraft that provides controlled ventilation of the interior space of an aircraft body, facilitating reduction of volatile organic compounds (VOCs) within cabin air, dehumidifying and reducing moisture condensation and thus corrosion and other moisture related problems within the envelope, allowing increased humidification of cabin air, and allowing suppression of fires within the envelope. The environment control system includes at least a cabin and an envelope. It includes supply means for supplying a flow of dry ventilation air to the aircraft body. An airflow control device is capable of dividing the flow of ventilation air onto an envelope ventilation air stream and a cabin ventilation air stream. An envelope ventilation duct system directs the envelope ventilation air stream into the envelope, and a cabin duct system directs the cabin ventilation air stream into the cabin.

Abstract: A continuous building basement wall and floor cavity, formed by the foundation wall and floor enclosure on the outside, and an attached inner air and vapor barrier structure, insulated as appropriate, is drained and ventilated to inhibit and prevent soil moisture and gases, such as radon and methane, from entering the basement living space. The air exhausted from the cavity can be drawn from the basement living space, as well as from the surrounding soil and the outdoors. This ventilation of the cavity serves to thermally condition the basement enclosure structure and, coincidentally, to beneficially augment the ventilation rate of the living space. Cavity exhaust air can be used for combustion air supply and heat recovery pruposes. Such a cavity can be economically constructed, using novel modifications to current construction practices, in both new and existing building structures.