Method and device for laser shock processing of fastening holes

A technology of laser shock strengthening and fastening holes, which is applied in the field of laser shock strengthening of fastening holes and internal surface strengthening of small-diameter fastening holes, which can solve unfavorable continuous operation, small impact force of hole wall, and increased surface roughness of materials and other problems, to achieve the effect of being conducive to continuous operation, improving fatigue life and strengthening effect

Inactive Publication Date: 2011-01-12
JIANGSU UNIV
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Problems solved by technology

People such as Peter A. Simeone and Apostolos P. karafillis of U.S. General Company declared that the patent No. is the U.S. patent of US 6189356 B1, and the name is called shot peening method and device (Method and Apparatus for Peening), and this patent will be the cone surface The splitter rod extends into one end of the fastening hole, and the pellets are sprayed into the other end of the fastening hole. The inner wall of the fastening hole is shot peened by the conical reflection of the splitter rod, but it leads to an increase in the surface roughness of the material. Will...

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  • Method and device for laser shock processing of fastening holes
  • Method and device for laser shock processing of fastening holes
  • Method and device for laser shock processing of fastening holes

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Embodiment Construction

[0019] The details and working conditions of the specific device proposed by the present invention will be described in detail below in conjunction with the figures.

[0020] The laser shock peening device for fastening holes in the present invention includes: laser, focusing system 1, laser head 4, workpiece 5, energy absorbing rod 6, feed mechanism A7, feed mechanism B9, clamp 8, workbench 10, Control System. Wherein the water inlet 3 is connected to the water pipe, and the water flow enters the water inlet 3 and sprays to the fastening hole through the annular water nozzle 14 at the lower end of the laser head 4, so that the water flow can be evenly injected into the small hole. The energy absorbing rod 6 is placed inside the fastening hole, and the energy absorbing rod 6 is clamped on the feed mechanism A7. The feed mechanism B9 realizes the up and down movement of the workpiece 5 through the clamp 8 .

[0021] See the principle of the present invention figure 2 , the ...

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Abstract

The invention discloses a method and a device for laser shock processing of fastening holes, and relates to the field of processing and manufacturing of the fastening holes. An energy absorbing rod (6) is placed at a proper position in a fastening hole, laser pulse (2) acts on a bevel of a head of the energy absorbing rod (6) to induce the explosion of a plasma (6) to generate a shock wave to act on an inner wall of the fastening hole, so that the fastening hole is processed; and the device comprises a laser, a concentrating system (1), a laser head (4), the energy absorbing rod (6), a feed mechanism A (7), a feed mechanism B (9), a fixture (8) and a workbench (10). The explosive force of the plasma (12) induced by the laser in the fastening hole acts on the inner wall of the hole to make the inner wall of the hole generate certain plastic deformation, so that the residual stress larger than that generated by the common processing is introduced, and the fatigue life of the fastening hole is effectively improved.

Description

technical field [0001] The invention relates to the field of fastening hole processing and manufacturing, in particular to a method and device for laser shock strengthening of fastening holes, and is especially suitable for strengthening the inner surface of small-diameter fastening holes with severe stress concentration. technical background [0002] Fastening holes are typical stress concentration details on aircraft components, which are prone to fatigue cracks under the action of alternating loads, which will greatly reduce the safety, reliability and service life of the whole machine. Therefore, in design, material selection and manufacturing, how to reduce the influence of stress concentration in fastening holes as much as possible, improve the fatigue resistance of aircraft structures, prolong the service life, and ensure the reliability and safety of aircraft structures is an important aspect of design and material research. important research topics for researchers....

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Application Information

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IPC IPC(8): C21D7/00
CPCY02P10/20
Inventor 姜银方钱晓明张永康管海兵张朝阳李志飞
Owner JIANGSU UNIV
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