A fin block is provided for a calibrating device for the calibrating of an extruded profile. The fin block includes a fin structure, which has a plurality of fins which are spaced apart from one another by grooves and are arranged in longitudinal direction of the fin block, wherein the fins of the fin structure have a variable dimension in longitudinal direction of the fin block. Further, there is provided a method for the production of the above-mentioned fin block and a calibrating device, which includes a plurality of the above-mentioned fin blocks. Furthermore, there is provided a system for the additive manufacture of the above-mentioned fin block, a corresponding computer program and corresponding data set.

In a method of providing a flow for a process chamber of a device for producing a three-dimensional object by layer-wise application and selective solidification of a building material in a build area a process gas is supplied to the process chamber in a lower altitude region of the process chamber, wherein the process chamber includes a gas inlet for introducing the process gas into the process chamber and a gas outlet for discharging the process gas from the process chamber. The gas inlet and the gas outlet are provided in the lower altitude region of the process chamber and the process gas flows in a main flow from the gas inlet to the gas outlet, and wherein a secondary flow is located in a sub-region of the lower altitude region, which sub-region is located above a bottom surface of the process chamber surrounding the build area.

In the present disclosure, systems and apparatuses for enabling modular attachment of a plurality of devices are described. In one aspect, an apparatus may include a center rail having a distal end and a proximal end. The apparatus may further include a first flange coupled with the proximal end and a second flange coupled with the distal end. The apparatus may further include a collar disposed around the center rail and between the first flange and the second flange. The apparatus may further include at least one arm connected with the collar, and the at least one arm may be configured to connect with a modular attachment.

A method for producing a support structure in the additive manufacturing of a component, includes: a) providing a geometry for the component having a region to be supported, b) providing a support structure for the region of the component, c) defining an irradiation pattern for an irradiation of layers of a raw material for the support structure, wherein surface vectors for an irradiation for a structure of the component extend into a region of the support structure, wherein common surface vectors are defined for the component and for the support structure, and d) selective irradiation of layers of the raw material for the component and the provided support structure according to the defined irradiation pattern.

A method for manufacturing a blade in composite material with added metal leading edge for gas turbine aeroengine, the method including producing a batch of plurality of blade bodies in composite material; creating a digital model of a blade body from a blade in the batch of plurality of blade bodies; creating a digital model of a theoretical final blade including a leading edge; generating a digital model of a leading edge from the digital model of a blade body and final blade model; manufacturing at least one leading edge via additive manufacturing from the generated leading edge digital model; bonding each manufactured leading edge onto a blade body from the batch of plurality of blade bodies.

A method for manufacturing a blade in composite material with added metal leading edge for gas turbine aeroengine, the method including producing a batch of plurality of blade bodies in composite material; creating a digital model of a blade body from a blade in the batch of plurality of blade bodies; creating a digital model of a theoretical final blade including a leading edge; generating a digital model of a leading edge from the digital model of a blade body and final blade model; manufacturing at least one leading edge via additive manufacturing from the generated leading edge digital model; bonding each manufactured leading edge onto a blade body from the batch of plurality of blade bodies.

Disclosed is a method for forming an orthopaedic implant. The method comprises determining one or more parameters of a bone, of a subject, to which the implant is to be attached, and calculating specifications based on parameters. That calculation includes calculating a mechanical property relating to elasticity of the implant, a length of the implant, and positions of two or more fixation locations by which to fix the implant to the bone. The method further comprises forming the implant based on the specifications, wherein each fixation location comprises a longitudinal axis through the implant, and calculating specifications comprises calculating a trajectory for the longitudinal axis of the respective fixation location.

A novel process for creating porous structures via additive manufacturing processes such as material deposition or powder bed fusion additive manufacturing is provided. The process reduces the computational requirement for generation of the porous structure geometry and for processing the porous structure geometry to generate CNC code. The process provides reduced file size for CNC code and avoids large files which may exceed capacity of manufacturing machines. The process also significantly reduces the time required to manufacture the porous structure on an additive manufacturing machine.

Model data is obtained, defining parts to be generated by a three-dimensional printer. A sprue is determined to connect the parts, and a label is automatically generated on the sprue which identifies the parts connected to the sprue. Modified model data is generated representing the parts and the sprue.

One or more embodiments of the present disclosure relate to partitioning of objects for additive manufacture. A method may include defining one or more partition lines in an object of a build file. The build file may comprise instructions for additively manufacturing the object. The method may also include generating part build files based on the build file and the one or more partition lines. The part build files may comprise instructions for additively manufacturing parts of the object. The method may also include generating a physical instance of each part of the object according to the part build files. The method may also include assembling the physical instances of the parts into a physical instance of the object. The method may also include applying heat to the physical instance of the object. Related devices, systems and methods are also disclosed.