Abstract: A computing system may include an access engine and a toolpath reordering engine. The access engine may be configured to access an original layer toolpath for slice of a 3D CAD object as well as a heat criticality measure for the original layer toolpath. The heat criticality measure may specify a heat impact for different points on the multiple toolpath segments of the original layer toolpath for the 3D printing of the physical part using the original layer toolpath. The toolpath reordering engine may be configured to reorder the multiple toolpath segments into a modified layer toolpath, and the modified layer toolpath may have a heat criticality measure with a lesser heat impact on the physical part than the heat criticality measure for the original layer toolpath.

Abstract: A method and apparatus for designing and manufacturing a component in a computer-aided design and manufacturing environment is disclosed. A method includes obtaining a geometric model of a component from a geometric model database, and determining at least one orientation parameter value associated with the geometric model of the component. The at least one orientation parameter value is associated with an orientation parameter that defines orientation of the component during additive manufacturing of the component. The method includes performing volumetric analysis of the component based on the at least one orientation parameter value associated with the component using the geometric model of the component.

Abstract: A computing system may include an access engine and a defect detection engine. The access engine may be configured to access a slice contour of a given layer of a 3-dimensional (3D) object designed for manufacture through an additive manufacturing process and obtain hatch tracking for the slice contour, the hatch tracking representative of an energy path to melt metal powder for constructing the given layer through the additive manufacturing process. The defect detection engine may be configured to construct, from the slice contour, an as-built image for the given layer by rendering the hatch tracking in the slice contour; construct, from the slice contour, an idealized image for the given layer; and identify defects in the given layer via image analysis between the as-built image and the idealized image.

Abstract: A computer-implemented method of calculating a gap distance between a support structure and a component which is to be build up additively by powder bed fusion, includes: a) providing a component design of the component, b) selecting at least on support surface of the component based on the provided component design and a process analysis, wherein the support surface requires support during the buildup, c) providing a support design of a support structure for supporting the component during the buildup, d) recording CAM-data for the buildup of the component, and, e) calculating an optimal gap distance to be hold during the buildup between the support structure and the support surface, wherein the calculation is based on the selected support surface and the recorded CAM-data, wherein the gap distance is further rated to be large enough to avoid a structural connection between the support surface and the support structure.

Abstract: A method for heating a base material in additive manufacturing includes a) providing an energy beam for the heating of the base material, wherein the base material is arranged to at least partly form a manufacturing plane, and b) irradiating the manufacturing plane for the heating with the energy beam under scaled irradiation parameters, wherein the scaled irradiation parameters are derived in that irradiation parameters for fusing the base material are scaled by a scaling factor, and wherein the scaling factor includes a quotient of a heating beam diameter and a fusion beam diameter.

Abstract: An irradiating method for the additive production of a component in order to heal structural defects in an additively constructed structure for the component. The method includes the providing of a laser or electron beam and the selective irradiating of a defect region of an additively constructed layer of the structure by the laser or electron beam according to a predetermined, in particular closed trajectory, which defines the defect region, wherein the defect region contains a structural defect. A method for additive production, a correspondingly produced component and a computer program product utilize the method.