| 摘要 |
A movable dehumidification apparatus for an aircraft according to the present invention includes a first air inlet into which outside air is introduced; a dehumidification rotor that performs dehumidification by adsorbing moisture in the air introduced into the first air inlet; a dehumidification unit that includes a first air outlet for discharging the air dehumidified by the dehumidification rotor to an object to be dehumidified; a drying unit that dries the moisture adsorbed to the dehumidification rotor; and a heat exchange unit that is provided between the dehumidification rotor and the first air outlet and includes a thermo-electric element for cooling the air dehumidified by the dehumidification rotor through heat exchange, and a heat pipe. |
