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103results about How to "Reduce stress buildup" patented technology

Preparation method of titanium alloy thin-wall honeycomb structure

ActiveCN104043831AHigh mechanical strengthVarious geometric shapesAlloy substrateLayer thickness
The invention provides a preparation method of a titanium alloy thin-wall honeycomb structure. The preparation method comprises the steps that (a) a titanium alloy thin-wall honeycomb structure model is sliced and layered according to 20-30 mu m layer thickness; (2) titanium alloy powder is uniformly paved on a titanium alloy substrate, a laser beam which is emitted by a laser is used for selectively melting a titanium alloy powder layer according to the determined scan locus of the laser beam to complete the processing of one layer of titanium alloy thin-wall honeycomb structure; (c) the titanium alloy powder is paved on the layer of formed titanium alloy thin-wall honeycomb structure again, the laser beam which is emitted by the laser is used for selectively melting the titanium alloy powder layer according to the determined scan locus of the laser beam; (d) the titanium alloy thin-wall honeycomb structure is processed layer by layer, and the titanium alloy thin-wall honeycomb structure is finally formed. According to the method, the stress accumulation and the deformation of a forming piece in the forming process are reduced, the flexibility degree is high, and a thin-wall honeycomb component with variable honeycomb distance and a three-dimensional dot matrix structure can be prepared.
Owner:CAPITAL AEROSPACE MACHINERY +1
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