FIELD: military equipment, in particular, vehicles for treatment of outer surfaces of equipment and armament, structures, roads by a directed fast high-temperature gas flow, as well as for set-up of aerosol curtains.
SUBSTANCE: an arched bed is installed in the generating set in the axis of the armored hull, a turbojet engine is fastened to the bed. The tanks for fuel and working liquid are positioned on its sides with formation of an air cavity forming the longitudinal direction of the blowing off air flow for the outer cooling of the turbojet engine. An ejector made in the form of a probe enveloping the nozzle is fastened on the front plate of the armored hull in alignment with the outlet port of the heat gas flow. The ejector is designed to produce rarefaction in the armored hull and form the blowing off air flow. For intake of supply air of the turbojet engine and extension pipe with a profile made according to the shape of the lemniscate section at the beginning of the flowing part. The pipe air-intake section is brought out to the vertical area of the rear plate of the armored hull and shifted from the intake louvers of the tank engine air supply and cooling systems by a distance providing tank engine operation within the preset operating regimes.
EFFECT: enhanced operating efficiency of the set.
9 cl, 6 dwg
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Authors
Dates
2006-04-10—Published
2004-09-01—Filed