| 摘要 |
containers for transportation of special cargoes, mainly of the rocket-space equipment in the moisture-temperature conditions and air purity. SUBSTANCE: isothermal container has a body with a load-carrying structure and heat insulation. The upper part of the body and the container walls have a skin located outside the heat insulation and forming air spaces with the latter. The above air spaces are interconnected, and the load-carrying structure of the body has members separating the air spaces into ducts. The ducts located in the body length are connected through manifolds for communication with the atmosphere. The container is provided at least with one exhaust fan made for connection the manifold located in the upper part of the container body. The container body may be made of two horizontally detachable parts that are made with a tight seal and interconnected with the aid of locking devices. EFFECT: ensured the preset temperature condition the container cargo chamber, enhanced efficiency of protection of the transported cargo against heating. 7 cl, 4 dwg
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