Method and apparatus for welding
A welding method and scanning direction technology, which is applied in the field of welding and welding devices, can solve problems such as easy cracks, and achieve the effects of stable melting width, high-quality welding, and low cost
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Embodiment approach 1
[0056] Next, Embodiment 1 according to the present invention will be described with reference to the drawings.
[0057] figure 1 It is a figure which shows the welding method in this embodiment.
[0058] Such as figure 1 As shown, in the welding method of this embodiment, the member 102 and the member 103 are overlapped. A laser beam 101 is irradiated onto the surface of a member 102 . The surface of the component 102 is scanned with the laser beam 101 in the direction of the arrow. At the same time, a small hole 105 is formed in the members 102 and 103 immediately below the portion irradiated with the laser beam 101 (hereinafter referred to as an irradiation spot). Around the small hole 105, there is formed a melting portion 104 where the members 102, 103 are in a molten state. Thereby, the members 102 , 103 are welded by the laser beam 101 .
[0059] Hereinafter, the spot intensity refers to the beam intensity at the irradiation point. The "spot diameter" refers to ...
Embodiment 1
[0070] Next, an example (hereinafter referred to as example 1) in this embodiment will be described.
[0071] In this embodiment, the member 102 is a metal plate formed of nickel and having a plate thickness of 0.2 mm. The member 103 is a metal plate made of copper and having a plate thickness of 0.5 mm. The spot diameter of the beam portion 101a is 0.4 mm. The spot diameter of the beam portion 101b is 0.05 mm. The spot intensity of the beam portion 101a is 300W. The spot intensity of the beam portion 101b is 600W. The spot center of the beam portion 101b was shifted from the spot center of the laser beam 101 toward the rear in the scanning direction by 0.05 mm. The laser beam 101 is continuously irradiated onto the surface of the member 102 . The surface of the member 102 is scanned with the laser beam 101 at a scanning speed of 100 mm / sec.
[0072] In this embodiment, based on these conditions, the members 102, 103 were overlap-welded with the laser beam 101. FIG.
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Embodiment approach 2
[0089] Next, Embodiment 2 according to the present invention will be described with reference to the drawings. In addition, the same reference numerals are assigned to the same constituent elements as those in Embodiment 1, and description thereof will be omitted.
[0090] Figure 5 It is a figure which shows the welding method in this embodiment.
[0091] Such as Figure 5 As shown, in the welding method of this embodiment, the end of the member 102 is butted against the end of the member 103 . The laser beam 201 is irradiated to the mating portions of the members 102, 103 so that the beam portions 201b, 201c are respectively arranged on the members 102, 103 so as to sandwich the mating surfaces. The abutting portion of the components 102, 103 is scanned with the laser beam 201 in the direction of the arrow so that the beam portion 201b, 201c does not intersect the abutting surface. Thereby, the members 102 and 103 are welded by the laser beam 201 .
[0092] Figure 6A , ...
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Abstract
Description
Claims
Application Information
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