ES196462A3 - IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS - Google Patents

IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS

Info

Publication number
ES196462A3
ES196462A3 ES0196462A ES196462A ES196462A3 ES 196462 A3 ES196462 A3 ES 196462A3 ES 0196462 A ES0196462 A ES 0196462A ES 196462 A ES196462 A ES 196462A ES 196462 A3 ES196462 A3 ES 196462A3
Authority
ES
Spain
Prior art keywords
gas
improvements introduced
oil
oil rotary
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
ES0196462A
Other languages
Spanish (es)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RIBAS PES AMADEO TURNEU ORTA V
Original Assignee
RIBAS PES AMADEO TURNEU ORTA V
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RIBAS PES AMADEO TURNEU ORTA V filed Critical RIBAS PES AMADEO TURNEU ORTA V
Priority to ES0196462A priority Critical patent/ES196462A3/en
Publication of ES196462A3 publication Critical patent/ES196462A3/en
Expired legal-status Critical Current

Links

Abstract

Perfeccionamientos introducidos en el mecanismo de los quemadores rotativos de gas-oil aplicables a calderas u hornos de pequeñas industrias consistentes en el acoplamiento de una turbina de aire al dispositivo inyector del chorro de combustible en forma tal que la afluencia de los dos componentes de la mezcla el gas-oil y el aire llegan a la boquilla de expulsión en forma concéntrica y allí experimentan el aumento de volatilización en una doble cámara de aire donde acude la proyección del mismo por la disposición de la boquilla en forma de embudo que recoge la corriente originada por las aspas del ventilador que es solidario por eje común al motor generador.Improvements introduced in the mechanism of rotary gas-oil burners applicable to boilers or furnaces of small industries, consisting of the coupling of an air turbine to the fuel jet injector device in such a way that the influx of the two components of the mixture Gas-oil and air reach the ejection nozzle in a concentric manner and there they experience increased volatilization in a double air chamber where it is projected by the funnel-shaped nozzle that collects the current generated. by the fan blades that are attached to the generator motor through a common axis.

ES0196462A 1951-02-08 1951-02-08 IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS Expired ES196462A3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES0196462A ES196462A3 (en) 1951-02-08 1951-02-08 IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES0196462A ES196462A3 (en) 1951-02-08 1951-02-08 IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS

Publications (1)

Publication Number Publication Date
ES196462A3 true ES196462A3 (en) 1951-06-16

Family

ID=37828045

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0196462A Expired ES196462A3 (en) 1951-02-08 1951-02-08 IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS

Country Status (1)

Country Link
ES (1) ES196462A3 (en)

Similar Documents

Publication Publication Date Title
ES196462A3 (en) IMPROVEMENTS INTRODUCED IN THE MECHANISM OF THE GAS-OIL ROTARY BURNERS
GB922069A (en) Combustion chamber for a gas turbine engine
GB737081A (en) Improvements relating to jet propulsion engines
GB699267A (en) Improvements in or relating to combustion turbine units
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB706841A (en) Improvements relating to turbine jet propulsion power units
CH250481A (en) Gas turbine combustion chamber with insert irradiated by the flame on the inside and cooled by air on the outside.
GB579511A (en) Improvements in or relating to jet-propulsion apparatus for aircraft
GB637223A (en) Improvements in and relating to combustion units particularly for use in gas turbinesystems
ES172978U (en) Burner for gas flame. (Machine-translation by Google Translate, not legally binding)
ES196482A1 (en) IMPROVEMENTS INTRODUCED IN THE GAS-OIL AND FUEL-OIL BURNERS
GB554709A (en) Means for disposing of gases released from the water of a gas scrubber
SU75129A1 (en) Coal Burners
GB299217A (en) Improved gas burner with tangential supply nozzles
ES189613A1 (en) A DEVICE BY WHICH A FUEL ECONOMY IS OBTAINED IN THE EXPLOSION ENGINES, AVOIDING THE FIRE OF THE CARBURETOR BY FLAME RETREAT, WINNING AT THE SAME TIME IN POWER
GB574313A (en) Improvements in or relating to gas burners
GB578503A (en) Improvements in or relating to the propulsion of ships in water
GB407158A (en) Improvements in and relating to steam generators
GB465691A (en) Improvements in and connected with fuel burners
GB312588A (en) Improvements in burners for powdered fuel
GB123575A (en) Method of and Apparatus for Arresting Sparks and Economizing Fuel in Furnaces.
ES188434A1 (en) IMPROVEMENTS IN THE HAIR DRYERS
CH263387A (en) Ignition device with a low-voltage arc igniter on the combustion chamber of a gas turbine.
ES154571A1 (en) GASOGEN APPLIANCE APPLICABLE TO ALL KINDS OF ENGINES