发明名称 УНИВЕРСАЛЬНАЯ ГЕНЕРИРУЮЩАЯ УСТАНОВКА ТЕПЛОВОГО ГАЗОВОГО ПОТОКА НА ТАНКОВОМ ШАССИ
摘要 FIELD: military equipment, in particular, vehicles for treatment of outer surfaces of equipment and armament, structures, roads, etc, by a directed fast high-temperature gas flow at chemical decontamination, radioactive decontamination and disinfection. ^ SUBSTANCE: the universal generating set is positioned on a rotary platform of a base tank chassis. A turbojet engine is used as the generator of heat gas flow. The turbojet engine together with the systems servicing it is positioned in an armored hull mounted on a rotary platform. The armored hull has a box shape with a rigid frame on the bottom, welded spatial framework formed by longitudinal beams and vertical posts welded to the frame, armored walls linked with the frame and framework, and a detachable cover of a trapezoidal shape in cross-section. A bed for installation of the turbojet engine is positioned inside the hull in its central axis, and two rows of inner lateral ribs are installed, they adjoin the side walls of the hull with formation of six compartments for tanks with fuel and working fluid. The armored hull is installed on remote blades of the rotary platform for circular scanning of the terrain from the commander-operator's seat and boarding of the commander-operator through the manhole of the rotary platform irrespective of its position relative to the tank chassis. An armored door with a port located in the upper part for installation of the air intake device for supply of the turbojet engine is installed in the rear wall. Handrails-steps are welded on the sides of the door, and a bracket of the antenna inlet of the communication means is installed. A recess for the manhole of the rotary platform is made in the front part of the armored hull in the central axis, the hull roof is made of detachably fastened armored plates on the framework, they are provided with handrails on its sides. A frame with rotary wings is made in the area above the door. ^ EFFECT: enhanced convenience of operation and servicing of the turbojet engine and of all its systems with preservation of protection at the tank level. ^ 4 cl, 7 dwg
申请公布号 RU2004126621(A) 申请公布日期 2006.02.20
申请号 RU20040126621 申请日期 2004.09.01
申请人 Федеральное государственное унитарное предпри тие Конструкторское бюро транспортного машиностроени  (RU);Общество с ограниченной ответственностью Научно-производственное предпри тие "Авиакон" (RU) 发明人 Бесман Ростислав Степанович (RU);Болдырев Александр Петрович (RU);Гоцулова Нина Иосифовна (RU);Гейко Ольга Владимировна (RU);Жуков Альберт Иосифович (RU);Паршаков Станислав Леонидович (RU);Полканова Екатерина Анатольевна (RU)
分类号 F41H7/00;A61L2/00 主分类号 F41H7/00
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