Patent ID: 8763423

Claim:
An aviation cargo container temperature control system for use in a flat-pack aviation cargo container having a base and at least one side wall and a cover, the aviation cargo container temperature control system comprising: at least one sleeve foldable between an unfolded and a compressed state and having first and second major planes and at least one temperature control pack, the sleeve being attachable prior to use along one of its major planes to a major plane of an inside wall of the flat-pack aviation cargo container, each sleeve being operable in a compressed state to permit the flat-pack aviation cargo container, the sleeve being detachable between uses, the sleeve container to be collapsed and in an unfolded state to retain a temperature control pack within, to maintain a temperature of an atmosphere within the flat-pack aviation cargo container, when closed, by virtue of heat transfer between the temperature control pack and the atmosphere of the flat-pack aviation cargo container; and to prevent contact of the temperature control pack with any product being transported in the flat-pack aviation cargo container.