A high-
combustion and high-velocity
oxygen-
fuel spray gun device, comprising a coaxial stabilizer (1), a
combustion chamber (2), a coupler (4) and a
gun barrel (8), wherein the front end of the
combustion chamber (2) is of a Laval
nozzle structure; the coaxial stabilizer (1) is hermetically connected to the rear end of the
combustion chamber (2) and is provided with a bore pressure-measuring tube (9), an ignition needle (10), a fuel needle (11), a first
oxygen input tube (12) and a second
oxygen input tube (13); the coupler (4) is axially provided with a central through hole and an outer water-cooled through hole, one end of the coupler (4) is hermetically connected to an outlet of the Laval
nozzle structure of the
combustion chamber (2), and the other end of the coupler (4) is hermetically connected to the
gun barrel (8) to integrally form a spray gun body; an inner axial through hole of the
gun barrel (8) widens from the rear end to the front end; the interior of the
combustion chamber (2), the central through hole of the coupler (4) and the interior of the gun
barrel (8) jointly form a
flame channel; a spray gun housing (3) is sleeved outside the combustion chamber (2); a gun
barrel housing (7) is sleeved outside the gun
barrel (8); two ends of the spray gun housing (3) are hermetically fixed to the coaxial stabilizer (1) and the coupler (4); two ends of the gun barrel housing (7) are hermetically fixed to ends of the coupler (4) and the gun barrel (8); a water-cooled channel is formed between the spray gun housing (3), the gun barrel housing (7) and the spray gun body; and the coupler (4) is radially provided with a
powder feeding needle (6) to feed a carrier gas, which carries a spray
powder, and
hydrogen into the
flame channel of the central through hole. Further disclosed is a working method for the high-combustion and high-velocity oxygen-
fuel spray gun device. By introducing
hydrogen and oxygen to carry out high-velocity combustion at the coupler (4), a bor