FIELD: process engineering.
SUBSTANCE: invention relates to ejection of various fluids, particularly, water by blown airflow and can be used in enforcement of law, environmental protection and agriculture. Proposed device comprises several extra satellites, each including one premixing chamber. Said satellites are arranged around secondary air cowling. Engine comprises fluid ejector making a compressed airflow generator, secondary air being ejected at high flow rate in secondary air channel. Compressed air bleed pipe or pipes are connected to said channel. Dual-flow reactor makes the airflow generator and includes fluid flow ejector. Proposed method comprises creating blown airflow by bypass gas turbine engine. Said engine is supplied with ambient air and includes secondary compressed air channel. Said channel is arranged around central housing supplied with primary compressed air. Blower driven by motor or gas turbine engine is built in central housing. Compressed air is bled in secondary compressed air channel to supply one or several premixing chambers. Chambers are supplied with fluid to be ejected for it to be sprayed together with bled compressed air in ambient medium.
EFFECT: higher efficiency of mixing, high-quality sprayed air and fluid, higher efficiency of fire extinguishing.
14 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
BYPASS GAS-TURBINE ENGINE EQUIPPED WITH PRE-COOLER | 2007 |
|
RU2411389C2 |
TURBOJET ENGINE COMPRISING THERMOELECTRIC GENERATORS | 2013 |
|
RU2631847C2 |
TAIL CONE FOR ROTARY GAS TURBINE ENGINE WITH MICRO-JETS | 2012 |
|
RU2605869C2 |
AIRCRAFT BYPASS GAS TURBINE ENGINE FURNISHED WITH PRECOOLER | 2007 |
|
RU2382221C1 |
GAS EXHAUST NOZZLE AND MULTIFLOW TURBOJET ENGINE | 2011 |
|
RU2575503C2 |
SIMPLIFIED CONTROL BYPASS GAS-TURBINE ENGINE WITH MEANS OF EXTRACTION OF EXCESS AIR | 2002 |
|
RU2222708C2 |
TURBOFAN ENGINE WITH PRECOOLER | 2006 |
|
RU2376205C1 |
JET GAS-TURBINE LOCOMOTIVE | 2003 |
|
RU2251505C1 |
AIR FILTERING DEVICE AT INPUT OF INTERNAL COMBUSTION ENGINE WITH VENTILATION DEVICE | 2010 |
|
RU2561774C2 |
AIR ENGINE DESIGN | 2004 |
|
RU2355902C2 |
Authors
Dates
2014-03-27—Published
2010-03-09—Filed