FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to systems for temperature control and climate control of suspended aircraft containers for arrangement of payload. Aviation suspended container comprises aerodynamic housing (1) and climate control system inside housing. Climate control system comprises control unit (3). At that, with control unit (3) there connected are at least one heater (2), at least one passive cooling unit (4), at least one active cooling unit (5) with Peltier element (6), at least one fan (8) and at least two temperature sensors (9) located, respectively, both inside the container and outside.
EFFECT: achieving uniform and efficient heat transfer from inner environment of container to external atmosphere, high-speed operation, reliability and efficiency in any mode of flight of aircraft carrier and maintenance of payload operation in the specified operating temperature range, which prolongs its service life and reduces the number of forced equipment repairs.
5 cl, 1 dwg
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Authors
Dates
2020-08-28—Published
2019-01-09—Filed