发明名称 |
Method for extinguishing fires from an aircraft and related device |
摘要 |
The present invention comprises supplying a liquid onto the source of a fire from an aircraft (7), wherein said liquid is supplied in the form of gas-droplet stream (8) obtained by dispersion in a gas flow and by acceleration of the dual-phase flow in a gas-dynamics nozzle (4). The pressure at the inlet of the nozzle (4) as well as the relative concentration of liquid in the dual-phase flow are selected according to conditions enabling the formation of a dual-phase low-dispersion and high-speed flow which has a high extinguishing-substance concentration and remaining stable when submitted to interference. The fire-extinguishing device of the present invention comprises a liquid supply system (1), a gas supply system (2), a mixing chamber (3) for the gas and the liquid as well as a gas-dynamics nozzle (4), wherein all these members are arranged onboard an aircraft (7). The gas-dynamics nozzle supplies the liquid towards the area of the fire source and is connected to a vessel through a duct. The mixing chamber (3) is further provided with a liquid dispersion system. <IMAGE> |
申请公布号 |
AU2645499(A) |
申请公布日期 |
1999.08.23 |
申请号 |
AU19990026454 |
申请日期 |
1999.02.01 |
申请人 |
NAUCHNO-ISSLEDOVATELSKY INSTITUT NIZKIKH TEMPERATUR PRI MAI (MO |
发明人 |
JURY VLADIMIROVICH ZUEV;ALEXANDR VLADIMIROVICH KARPYSHEV;IGOR ALEXANDROVICH LEPESHINSKY |
分类号 |
A62C31/00;A62C3/02;A62C99/00;B64D1/16 |
主分类号 |
A62C31/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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