Claims
- 1. A plasma gas arc welding torch, comprising
- a. an annular nozzle body having a first orifice in a front end of the body and an axially extending first plenum chamber formed within said nozzle body in communication with said orifice, said first orifice having an axis,
- b. an axially extending electrode disposed within said chamber in alignment with said first orifice,
- c. means connected to the electrode for supplying electricity to the electrode to form an arc extending from the electrode through the first orifice to a workpiece positioned in front of the torch,
- d. a second plenum chamber formed by and between a pair of spaced inner and outer cups surrounding the forward end of the nozzle body, said cups having forward ends extending beyond the forward end of the nozzle body, the forward ends of the cups being directed radially inward toward the axis of the orifice and terminating in a circumferentially extending joining wall, said wall facing and being spaced from the axis of the orifice, said wall being provided with a plurality of spaced second orifices, said cups being spaced from the nozzle body to form a third plenum chamber between the nozzle body and the inner cup, said third plenum chamber having an annular third orifice surrounding the first orifice, said torch having therein a first passageway for feeding an inert gas to the first plenum chamber to form a plasma exiting from said nozzle through said first orifice, said torch having a third passageway for feeding an inert gas through the third plenum chamber to exit from the third orifice and form a column of blanketing gas surrounding said plasma, said torch having a second passageway for feeding an inert gas through the second plenum chamber to exit through said second orifices in the joining wall and impinge on the column of gas to constrict said column of gas.
- 2. In a welding torch as recited in claim 1, wherein said first orifice has a smaller cross sectional area than said first plenum chamber, whereby inert gas exiting from said first orifice increases in velocity.
ORIGIN OF THE INVENTION
The invention described herein was made in performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; 42 U.S.C. 2457).
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