Lamination-proof structure of laser shock processing

A technology of laser shock and protective layer, applied in laser welding equipment, welding equipment, metal processing equipment, etc., can solve problems such as difficult solid support, high shock wave reflection coefficient, and poor protection effect

Inactive Publication Date: 2009-05-27
BEIJING AVIATION MFG ENG INST CHINA AVIATION NO 1 GRP
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  • Summary
  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0004] In order to prevent back delamination, the method of back support can be used, but for curved surface structures, it is difficult to have matching solid supports. In addition, for shock waves, the support body and the supported body need to be closely bonded to be effective; liquid is also used. The method of absorbing waves on the back, but because the acoustic impedance of the liquid is quite different from that of the solid material, the reflection coefficient of the shock wave is still very high, so the protection effect is not very good

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  • Lamination-proof structure of laser shock processing

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Embodiment Construction

[0013] The technical solution of the present invention will be further described in detail below with reference to the accompanying drawings and embodiments:

[0014] See attached figure 1 As shown in the laser shock treatment of the anti-spam structure, the material of the metal target 4 is titanium alloy, aluminum alloy or stainless steel, and it is characterized in that: the back of the metal target 4 is covered with a layer of the metal target 4 material Protective layer 5 made of materials with close acoustic resistance, single-layer or multi-layer aluminum foil tape with a thickness of 0.2mm~0.5mm;

[0015] When the absorbing layer of the reflective area 6 is peeled off and overlaps with the next strengthening area by 50%, the absorbing layer needs to be replaced.

[0016] When laser shock processing metal materials, the laser 1 passes through the confinement layer 2 and reaches the absorption layer 3 and then generates a shock wave, which is directed to the metal target 4. ...

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Abstract

The invention relates to an anti-spallation structure processed by laser shock processing, metal target material is titanium alloy, aluminium alloy or stainless steel; wherein, the back of the metal target material is coated with a protection layer made of a material which has an acoustic resistance close to the acoustic resistance of the metal target material, namely a single-layer or multiple-layer aluminium foil tapes with the thickness between 0.2 and 0.5 millimetres; when spallation occurs in a wave-absorbing layer of a reflection area and the reflection area overlaps on the area to be reinforced next time for 50%, the wave-absorbing layer needs to be changed. The technical proposal of the invention has excellent effects on thin wall structure processed by laser shock processing or parts which have thick sections but are close to the inner wall.

Description

Technical field [0001] The invention is a spall prevention structure for laser shock treatment, belonging to laser processing technology, and relates to a spall prevention measure for laser shock treatment. Background technique [0002] Most engineering materials are more resistant to compression than tensile. They can often withstand considerable compressive stress, but cannot withstand large tensile stress. Therefore, in the laser shock treatment, the intensity of the shock wave must be controlled to obtain plastic strain and residual compressive stress on the front surface of the material, and the strong tensile wave cannot be generated when reflected on the back surface to cause the material to spall. [0003] However, when processing thin-walled structures by laser shock, the attenuation of the shock wave is relatively small during the propagation process. When the pressure wave with a large amplitude propagates to the back of the structure, the reflection of the wave occurs...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23K26/00B23K26/18B23K26/38
Inventor 邹世坤曹子文
Owner BEIJING AVIATION MFG ENG INST CHINA AVIATION NO 1 GRP
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