Study on Laser Keyhole Behavior in High-efficiency Low Power Pulsed Laser-TIG Hybrid Welding Process

2016 ◽  
Vol 52 (2) ◽  
pp. 41 ◽  
Author(s):  
Chenbin LI
2016 ◽  
Vol 1138 ◽  
pp. 147-152
Author(s):  
Aurel Valentin Bîrdeanu

The development and implementation into a high number of industrial applications of materials categorized as (Advanced) High Strength Steels (AHSS) due to their high performance per cost ratio is more and more present and this trend is also combined with the development and implementation of new joining technologies and processes, including laser-arc hybrid processes.The paper presents the results of applying Pulsed LASER-(micro)TIG hybrid welding process, for realizing overlap joints for Zn-coated (A)HSS materials in dissimilar configurations, joints that were presented as designed based on UltraLight Steel Auto Body (ULSAB) principles.The influence of main hybrid welding process parameters was investigated in order to establish if one can obtain joints with high values for the shear strength resistance for some of the actually used dissimilar steel combinations based on designs applied throughout ULSAB project and the autos built following these principles.


2008 ◽  
Vol 36 (4) ◽  
pp. 1937-1943 ◽  
Author(s):  
Liming Liu ◽  
Ruisheng Huang ◽  
Gang Song ◽  
Xinfeng Hao

2012 ◽  
Vol 212 (4) ◽  
pp. 890-902 ◽  
Author(s):  
Aurel-Valentin Bîrdeanu ◽  
Cristian Ciucă ◽  
Alexandru Puicea

2008 ◽  
Vol 6 (1) ◽  
pp. 47-50 ◽  
Author(s):  
黄瑞生 Ruisheng Huang ◽  
刘黎明 Liming Liu ◽  
张帆 Fan Zhang

2021 ◽  
Vol 11 (14) ◽  
pp. 6549
Author(s):  
Hui Liu ◽  
Ming Zeng ◽  
Xiang Niu ◽  
Hongyan Huang ◽  
Daren Yu

The microthruster is the crucial device of the drag-free attitude control system, essential for the space-borne gravitational wave detection mission. The cusped field thruster (also called the High Efficiency Multistage Plasma Thruster) becomes one of the candidate thrusters for the mission due to its low complexity and potential long life over a wide range of thrust. However, the prescribed minimum of thrust and thrust noise are considerable obstacles to downscaling works on cusped field thrusters. This article reviews the development of the low power cusped field thruster at the Harbin Institute of Technology since 2012, including the design of prototypes, experimental investigations and simulation studies. Progress has been made on the downscaling of cusped field thrusters, and a new concept of microwave discharge cusped field thruster has been introduced.


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