TY - JOUR
T1 - Operational characteristics of a periodic plasma torch
AU - Kuo, Spencer
AU - Bivolaru, Daniel
AU - Carter, Campbell D.
AU - Jacobsen, Lance
AU - Williams, Skip
N1 - Funding Information:
Manuscript received March 14, 2003; revised December 8, 2003. This work was supported by the Air Force Office of Scientific Research under Grant AFOSR-F49620–01-1–0392 and Laboratory Task LRIR-02VS02COR. S. P. Kuo and D. Bivolaru are with the Department of Electrical and Computer Engineering, Polytechnic University, Brooklyn, NY 11201 USA (e-mail: [email protected]). C. D. Carter and L. Jacobsen are with the Air Force Research Laboratory, Propulsion Directorate, Wright-Patterson AFB, OH 45433 USA. S. Williams is with the Air Force Research Laboratory, Space Vehicles Directorate, Hanscom AFB, MA 01731 USA. Digital Object Identifier 10.1109/TPS.2004.826041
PY - 2004/2
Y1 - 2004/2
N2 - Development of a plasma torch, which is intended as an ignition aide within a supersonic combustor, is studied. The high-voltage discharge and plasma plume generated by the torch module are described in a quiescent environment and in a supersonic crossflow. Voltage-current characteristics of the discharge and optical images of the plasma plume are used to characterize the operation of the torch module. The principal advantages of this torch module are its compact design, durability, and operational flexibility. The torch module can be operated in periodic or pulsed modes, depending on the power supply used. In the periodic mode presented in this paper, the capacitors are charged at the line frequency of 60 Hz resulting in a cyclical discharge at a frequency of 120 Hz. In this mode, peak and average powers reaching 8 and 2.8 kW, respectively, are demonstrated. The energy can be as high as 46 J per cycle, which is mainly limited by the power handling capability of the power supply. The penetration height and the volume of torch plume into a Mach 2.5 supersonic flow, typical for a supersonic combustor startup condition (vis-à-vis the cross-flow velocity), are investigated. In addition, ignition of ethylene fuel in a Mach 2 supersonic flow with a total temperature of 590 K and pressure of 5.4 atm is demonstrated.
AB - Development of a plasma torch, which is intended as an ignition aide within a supersonic combustor, is studied. The high-voltage discharge and plasma plume generated by the torch module are described in a quiescent environment and in a supersonic crossflow. Voltage-current characteristics of the discharge and optical images of the plasma plume are used to characterize the operation of the torch module. The principal advantages of this torch module are its compact design, durability, and operational flexibility. The torch module can be operated in periodic or pulsed modes, depending on the power supply used. In the periodic mode presented in this paper, the capacitors are charged at the line frequency of 60 Hz resulting in a cyclical discharge at a frequency of 120 Hz. In this mode, peak and average powers reaching 8 and 2.8 kW, respectively, are demonstrated. The energy can be as high as 46 J per cycle, which is mainly limited by the power handling capability of the power supply. The penetration height and the volume of torch plume into a Mach 2.5 supersonic flow, typical for a supersonic combustor startup condition (vis-à-vis the cross-flow velocity), are investigated. In addition, ignition of ethylene fuel in a Mach 2 supersonic flow with a total temperature of 590 K and pressure of 5.4 atm is demonstrated.
KW - Ignition aide
KW - Plasma jet
KW - Plasma torch module
KW - Supersonic combustor
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U2 - 10.1109/TPS.2004.826041
DO - 10.1109/TPS.2004.826041
M3 - Article
AN - SCOPUS:2442570711
SN - 0093-3813
VL - 32
SP - 262
EP - 268
JO - IEEE Transactions on Plasma Science
JF - IEEE Transactions on Plasma Science
IS - 1 III
ER -