FIELD: mechanical engineering. SUBSTANCE: thermocutter head includes nozzle, gas generator with combustion chamber and prechamber, fuel supply line for tangential supply of fuel relative to walls of gas generator, oxidizer supply line and igniter; prechamber has three stages. Diameters of stages increase in succession towards combustion chamber. Oxidizer supply line is brought in communication with stages of larger and smaller diameters by means of passages. Fuel supply line is brought in communication with stage of average diameter; igniter is located in stage of smaller diameter, thus making it possible to use different fuels and oxidizers without readjustment of components of device. EFFECT: completeness of combustion; reduction of overall dimensions and mass. 6 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
BURNER FOR CUTTING METALLIC MATERIAL AND FOR TREATING SURFACE | 2002 |
|
RU2201319C1 |
HEAD OF HEAT TORCH | 1995 |
|
RU2109213C1 |
HEAD OF HEAT TORCH | 1995 |
|
RU2109214C1 |
METHOD FOR THERMOABRASIVE CLEANING OF ARTICLE SURFACES AND APPARATUS FOR PERFORMING THE SAME | 2002 |
|
RU2201329C1 |
BURNER AND BURNER OPERATION METHOD (VERSIONS) | 2008 |
|
RU2381417C1 |
CUTTING TORCH HEAD | 1993 |
|
RU2037100C1 |
BURNER OF THERMIC GAS JET CUTTER | 2000 |
|
RU2169648C1 |
AUTOMATIC STORAGE-TYPE ELECTRIC WATER HEATER | 1998 |
|
RU2135904C1 |
GAS GENERATOR | 2015 |
|
RU2587510C1 |
AIRCRAFT GAS TURBINE ENGINE AND METHOD OF ITS SPEEDUP | 2014 |
|
RU2562822C2 |
Authors
Dates
1998-04-20—Published
1995-11-10—Filed