22nd International Symposium on Plasma Chemistry July 5-10, 2015; Antwerp, Belgium Stability of an arc generated by a TIG plasma torch K. Takeda and K. Maruyama Faculty of System Science and Technology, Akita Prefectural University, Yurihonjo, Japan Abstract: The transitions from a laminar arc to an unstable one were investigated. Experimental observations revealed that the transition occurred at the Reynolds number of 100 - 200. Plasma gas temperatures in various experimental conditions were estimated, measuring the arc motion driven by an imposed magnetic field. Keywords: transferred arc, stability, Reynolds number, temperature, electromagnetic force 1. Introduction Transferred arcs driven by an alternating magnetic field have been used to apply for various heat treatments of metals [1, 2]. Schematic arrangement for the magnetically driven arc is illustrated in Fig. 1, where a long arc is generated using a TIG (Tungsten Inert Gas) plasma torch. An alternating magnetic field is imposed perpendicularly to the arc. The electromagnetic force induces the oscillatory motion of the arc. Heat flux distribution on the anode material can be controlled by adjusting the magnetic field. The formation of a laminar arc is required for precise processing. However, few studies have been done on the stability of the arc [3]. In this work, the conditions to maintain the arc stable were studied. plasma forming gas Qo arc torch z power supply y The arc columns were observed by a camera, the shutter speed of which was fixed at 1/4000 sec. The arc became unstable with the increase of the gas flow rate as shown in Fig. 2. The fluctuation of the arc voltage was concomitant with the unstable arc column as shown in Fig. 3. Fig. 2. Variation of arc profiles with the increase of gas flow rate for d = 5 mm and I a = 60 A. x vo magnetic field B(t)=Bocos(ω t ) Ia Fig. 3. Fluctuation of arc voltage for various gas flow rates. anode Fig. 1. Schematic illustration of magnetically driven arc. 2. Experiment The stabilities of the arc were mainly investigated under no imposed magnetic field. Experimental conditions are summarized in Table 1. Table 1. Experimental conditions. parameter arc current, I a arc distance, L plasma forming gas gas flow rate, Q nozzle diameter, d P-II-12-14 quantity 40 - 80 [A] 50 [mm] Argon 1 - 12 [NL/min] 3.2, 4, 5 and 6 [mm] The variation of voltage fluctuation was shown in Fig. 4. Critical gas flow rate (Q*) was defined as the gas flow rate at which the arc became unstable. Q* Fig. 4. Definition of the critical gas flow rate; d = 5 mm and I a = 60 A. 1 The critical flow rate depended not only on the nozzle diameter of the torch but also on the arc current. The variation of the critical flow rates with the nozzle diameters and that with the arc currents were plotted in Figs. 5 and 6, respectively. From previous work on the magnetically driven arc [5], it was known that plasma gas velocity was expressed as: v= I a Bo Ya 2 + L2 ( ) Q 2Ya (4) Considering the equation of state for gas, T p is given by Tp = Mpo pd 2 v pMpo I a Bo d 2 Ya 2 + L2 ( ) = R 4 Q 4R 2Ya Q2 (5) where M, R and p o represent mass per mole, gas constant and atmospheric pressure, respectively. One example to estimate the plasma temperature is shown below. This experiment was carried out under the following conditions; nozzle diameter d = 5mm, pressure p 0 = 1 atmosphere, arc current I a = 80 A and gas flow rate Q = 5 NL/min (Q = 1.5x10-4 kg/s). In these conditions, a stable laminar arc was observed. Then alternating field was imposed perpendicularly to the arc. The amplitude (B o ) of the AC magnetic field was 3.7 x 10-3 T. The arc was driven by electromagnetic force and oscillated as shown in Fig. 7. Obtained amplitude of the arc motion (Y a ) was 17x10-3 m. Substituting Y a = 17x10-3 m into Eq. 5, plasma gas temperature was calculated as T p = 9050 K. Fig. 5. Variation of Q* with nozzle diameter. d=5mm Fig. 6. Variation of Q* with arc current. 3. Determination of Reynolds number In the next section, critical Reynolds number (Re*) will be calculated, corresponding to each critical gas flow rate (Q*). Before head, general procedure to determine the Reynolds number will be discussed in this section. 3.1. Relation between Re and Q Using viscosity (µ), nozzle diameter (d) and gas velocity (v), Reynolds number is expressed as Re = ρvd / µ (1) While, gas flow rate is written as Q = (πd 2 / 4) ρv . (2) Then Re is represented in the following form, Re = (π / 4)Q / dµ Fig. 7. Magnetically driven arc for the measurement of plasma gas temperature. 3.3 Determination of viscosity and Reynolds numbe Once the plasma gas temperature is known, the viscosity can be evaluated consulting the known relation between µ and T [4]. For argon plasma gas at T p = 9050 K, its viscosity is µ = 0.28x10-3 kg/(m s). Using known parameters of Q, d and µ, Reynolds number could be calculated as Re = 135 in this case. (3) In order to determine the numerical value of Re, it is important to know the plasma gas temperature (T p ), because viscosity strongly depends on the plasma gas temperature [4]. 3.2. Determination of plasma gas temperature One of the easy ways to estimate the plasma gas temperature is to measure the amplitude of the oscillatory motion (Y a ) in the magnetically driven arc shown in Fig. 1. 2 Ya 4. Critical Reynolds number As shown in Figs. 5 and 6, various critical gas flow rates were obtained for various experimental conditions. In similar procedures mentioned above, critical Reynolds number (Re*) was calculated for each critical gas flow rate (Q*). Obtained critical Reynolds numbers were plotted in Fig. 8. It is well known that the transition from a laminar flow to a turbulent one occurs at the Reynolds number of R e= 2000 ~3000. Different from the laminar/turbulent transition in ordinary fluid dynamics, P-II-12-14 he transition from stable arc to unstable one took place at Re* = 100 ~200. Fig. 8. Critical Reynolds number for arc stability. 5. Summary Stability of an arc was investigated. Experimental observations revealed the following results. 1. An arc changes its profile from a straight column to an irregular one when a flow rate of plasma forming gas exceeds a certain critical value of Q*. 2. Appearance of such unstable arc profile follows unstable fluctuation in the arc voltage. 3. Critical gas flow rate of Q* depends on the nozzle diameter of the plasma torch. 4. The increase of arc current results in the increase of Q*. Stability of the arc was discussed in terms of Reynolds number. With no information of plasma gas temperature, Reynolds number cannot be calculated. In order to estimate the temperature of the plasma gas, a new method was developed, using magnetically driven arc. 5. Transition from a stable arc to an unstable one was governed by Reynolds number. The critical Reynolds number is Re* = 100 ~200. P-II-12-14 6. Acknowledgements The authors would like to express our thanks to Prof M. Sugimoto of Akita Prefectural University for his kind help. 7. References [1] T. Toh, J. Tanaka, J. Muraki, Y. Yamamoto and K. Takeda. ISIJ Int., 45, 947-953 (2005) [2] R. Akiho. M. Sugimoto, K. Takeda, Y. Noguchi and T. Miura. Trans. Japan Soc. Mechanical Engineers Ser. C, 79, 690-703 (2013) [3] K. Maruyama, K. Takeda, M. Sugimoto and Y. Noguchi. J. Phys. Conf. Ser., 550, 012009 (2014) [4] P. Fauchai. Fundamental concepts. in: Int. Summer School on Plasma Chemistry; (IUPAC) 50 (1987) [5] K. Takeda, H. Okubo and M. Sugimoto. J. Phys. Conf. Ser., 550, 012011 (2014) 3
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