Method for producing hollow, large dimensional turbomachine components
A turbine, large-scale technology, applied in the direction of turbines, mechanical equipment, process efficiency improvement, etc., can solve problems such as high thermally induced stress deformation
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[0018] In order to reduce manufacturing cost and manufacturing time, and to achieve enhanced manufacturing flexibility of large thin-walled turbine components, the methods disclosed herein provide steps aimed at reducing or avoiding thermally induced deformation of the final part, such as buckling, so that A net or near net shape part is obtained at the end of the manufacturing process.
[0019] Since thermally induced deformation is concentrated at one or both end portions of a component produced by additive manufacturing, the methods disclosed herein provide for the production of semi-finished components including at least one end portion to be removed therefrom. Such sacrificial end portions may be designed such that inadmissible deformations (ie, those that would be unacceptable in the finished product) are located entirely in the sacrificial end portion, which is removed when the part cools. In some embodiments, the sacrificial end portion is configured to reinforce the c...
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