DEVICE TO EJECT FLUID BY BLOWN AIRFLOW Russian patent published in 2014 - IPC B05B7/00 

Abstract RU 2510296 C2

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

Similar patents RU2510296C2

Title Year Author Number
BYPASS GAS-TURBINE ENGINE EQUIPPED WITH PRE-COOLER 2007
  • Port Alen
  • Pra Dam'En
RU2411389C2
TURBOJET ENGINE COMPRISING THERMOELECTRIC GENERATORS 2013
  • Sharre Zhan-Zhak
  • Bensajed Moez
  • Missu Mark
  • Potte Fransis
  • Ribero Stefan
  • Tabar Romen
RU2631847C2
TAIL CONE FOR ROTARY GAS TURBINE ENGINE WITH MICRO-JETS 2012
  • Kont Per
  • Vjuillmen Aleksandr Alfred Gaston
  • Kenig Maksim
  • Dzhordan Piter
  • Zherve Iv
RU2605869C2
AIRCRAFT BYPASS GAS TURBINE ENGINE FURNISHED WITH PRECOOLER 2007
  • Port Alen
  • Pra Dam'En
RU2382221C1
GAS EXHAUST NOZZLE AND MULTIFLOW TURBOJET ENGINE 2011
  • Bodar Gijom
  • Vjuill'Men Aleksandr Al'Fred Gaston
RU2575503C2
SIMPLIFIED CONTROL BYPASS GAS-TURBINE ENGINE WITH MEANS OF EXTRACTION OF EXCESS AIR 2002
  • Bro Mishel' Zhil'Ber
  • Bross'E Paskal' Noehl'
RU2222708C2
TURBOFAN ENGINE WITH PRECOOLER 2006
  • Port Alen
RU2376205C1
JET GAS-TURBINE LOCOMOTIVE 2003
  • Fishbejn B.D.
RU2251505C1
AIR FILTERING DEVICE AT INPUT OF INTERNAL COMBUSTION ENGINE WITH VENTILATION DEVICE 2010
  • Deskjub Oliv'E P'Er
RU2561774C2
AIR ENGINE DESIGN 2004
  • Stretton Richard Dzhoffri
RU2355902C2

RU 2 510 296 C2

Authors

Ehtsheparr Bernar

Dates

2014-03-27Published

2010-03-09Filed