8/22/2019 WSJ-M module

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Special modular system for fire extinguishing and liquidation of natural and industrial disastersWATER STORM 

WSJ-M module

Purpose:1.  Precipitation and neutralization of ammonia and other toxic gases from the atmosphere.2.  Fire extinguishing of oil and gas fountains on land and at sea.3.  Cooling process of structures in large industrial enterprises at fires and accidents.

4. 

Neutralization of toxic substances on the surface of the earth in case of accidents.5.  Creating protective horizontal shields of water in the atmosphere to precipitate the gas andvertical shields to protect against fire and thermal emission.

Key features to maximize the performance:

1.  The range of gas-water mixture exceeds over 150 meters horizontally and vertically.2.  Area coverage - unlimited.3.  The volume of gas-water mixture (liters per second) is more than 8 million.4.  The volume of dispersed water per second is up to 200 kg.

The control system of the jet engine and the fuel system is a fully automatic and digital system. Themonitoring sensors are of European industrial standards.

The control system of the gas sectors, engine rotation and water volume is absolutely automaticwith manual or semi-automatic control options with the remote control unit. The control system hasartificial intellect and special infra-red cameras to estimate the situation before the start of the jetengine and further motor control for various scenarios. Scenarios are developed on the basis of thesimulation program at the conditions of the fire development or an industrial accident.

 A special pumping station conducts water supply for the WSJ-M and is capable of using any water

source within a radius of three kilometers from the accident area, including the sea, lake, river,pond, water tower and a fire hydrant.

8/22/2019 WSJ-M module

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 Engine:

M-701C turbojet engine designed and built by Walter Aircraft Engines (Czechia) for the military jettrainer aircraft Aero L-29 Delfín (English: Dolphin, NATO reporting name: Maya).

General characteristics

•  Type: Single shaft centrifugal turbojet engine•  Length: 2,067 mm (81.38 in)•  Diameter: 896 mm (35.28 in) (Max width): Max height 928 mm (36.53 in)• 

Dry weight: 330 kg (728 lb)

Components

•  Compressor: Single-stage centrifugal•  Combustors: 7 straight flow combustion chambers•  Turbine: Single-stage axial-flow with 61 blades

Performance

•  Maximum thrust: 8.75 kN (1,962 lbf) (Take-off power -15,500 rpm), 7.87 kN (1,764 lbf)

(Rated power - 14,950 rpm)•  Overall pressure ratio: 4.3:1•  Specific fuel consumption: 1.14 (at rated power)