Additive-based electroforming manufacturing methods for producing turbomachine components and other metallic articles are provided, as are metallic articles manufactured utilizing such manufacturing methods. In various embodiments, the method includes the step or process of additively manufacturing a sacrificial tooling structure having a component-defining surface region. A metallic body layer or shell is deposited over the component-defining surface region utilizing an electroforming process such that a geometry of the component-defining surface region is transferred to the body layer. The tooling structure is chemically dissolved, thermally decomposed, or otherwise removed, while the metallic body layer is left substantially intact. After tooling structure removal, the metallic body layer is further processed to complete fabrication of the metallic component. In certain implementations, the method may further include the step or process of depositing an electrically-conductive base coat over the component-defining surface region of the tooling structure for usage in the subsequently-performed electroforming process.

Additive-based electroforming manufacturing methods for producing turbomachine components and other metallic articles are provided, as are metallic articles manufactured utilizing such manufacturing methods. In various embodiments, the method includes the step or process of additively manufacturing a sacrificial tooling structure having a component-defining surface region. A metallic body layer or shell is deposited over the component-defining surface region utilizing an electroforming process such that a geometry of the component-defining surface region is transferred to the body layer. The tooling structure is chemically dissolved, thermally decomposed, or otherwise removed, while the metallic body layer is left substantially intact. After tooling structure removal, the metallic body layer is further processed to complete fabrication of the metallic component. In certain implementations, the method may further include the step or process of depositing an electrically-conductive base coat over the component-defining surface region of the tooling structure for usage in the subsequently-performed electroforming process.

According to a first aspect of the present disclosure, there is provided an additive manufacturing method. In the method, regions of successively-deposited layers of granular construction material are bound together so as to form a three-dimensional structure of bound material extending through and between the layers. The method comprises depositing a first granular construction material as a layer into a build region. The method comprises selectively binding regions of the first granular construction material together to form bound regions within the layer. The method comprises removing unbound granular construction material from the layer so as to provide at least one void in the layer. The method comprises depositing a second granular construction material into the build region so as to fill the at least one void. The method comprises selectively binding regions of the second granular construction material together to form bound regions within the layer. In the method, the second granular construction material is different from the first granular construction material. The method is repeated to form the object. An apparatus suitable for implementing the method is also disclosed.

According to a first aspect of the present disclosure, there is provided an additive manufacturing method. In the method, regions of successively-deposited layers of granular construction material are bound together so as to form a three-dimensional structure of bound material extending through and between the layers. The method comprises depositing a first granular construction material as a layer into a build region. The method comprises selectively binding regions of the first granular construction material together to form bound regions within the layer. The method comprises removing unbound granular construction material from the layer so as to provide at least one void in the layer. The method comprises depositing a second granular construction material into the build region so as to fill the at least one void. The method comprises selectively binding regions of the second granular construction material together to form bound regions within the layer. In the method, the second granular construction material is different from the first granular construction material. The method is repeated to form the object. An apparatus suitable for implementing the method is also disclosed.

A method of manufacturing a gas turbine engine element, for example a shroud segment. An insert has at least one elongated feature received in a mold cavity. A powder injection molding feedstock is injected. When the green part is disengaged from the mold, each elongated feature is slid out of the green part to define a respective elongated passage. The cross-sectional dimension of the elongated feature may be 0.020 inches or less, and/or a ratio between the length and cross-sectional dimension of the elongated feature may be at least 25. The method may include, after debinding and sintering, projecting a coating material while defining an obstruction between source of coating material and the open end of each elongated feature with a shoulder of the element to prevent the coating material from reaching the open end, followed by machining to remove at least a part of the shoulder.

The inventive concept relates to a method for manufacturing a metal based component (100, 200) having a cavity (103, 203). The method comprises the steps of: providing a plurality of individual segments (110, 210) corresponding to different portions of the metal based component; arranging the plurality of segments in a stack (120, 220) in such a way that the shape of the stack corresponds to the shape of the metal based component, and that a void (130, 230) is formed in the stack, wherein the shape of at least a portion of the void corresponds to the shape of the cavity; filling at least the first 10 portion of the void with an incompressible filler (140, 240); removing gas from the stack; subjecting the stack to a hot pressing process to form the metal based component comprising the cavity; removing at least a part of the incompressible filler from the metal based component.

A method for producing, by a metal powder injection moulding (MIM) technique, a part formed of at least one metal and/or at least one metal alloy including at least one internal cavity. A green core of a mixture of at least one powder of at least one ceramic and of a thermoplastic binder is used.

A method for producing, by a metal powder injection moulding (MIM) technique, a part formed of at least one metal and/or at least one metal alloy including at least one internal cavity. A green core of a mixture of at least one powder of at least one ceramic and of a thermoplastic binder is used.

In some examples, an additive manufacturing technique for forming a vacuum insulator. For example, a method including forming an article including a first layer, a second layer, and at least one support member extending between the first and second layer by depositing a filament via a filament delivery device, wherein the filament includes a sacrificial binder and a powder, and wherein the first layer, second layer, and at least one support member define an open cavity within the article; removing the binder; and sintering the article to form the vacuum insulator, wherein the vacuum insulator defines a vacuum environment in the cavity.

In some examples, an additive manufacturing technique for forming a vacuum insulator. For example, a method including forming an article including a first layer, a second layer, and at least one support member extending between the first and second layer by depositing a filament via a filament delivery device, wherein the filament includes a sacrificial binder and a powder, and wherein the first layer, second layer, and at least one support member define an open cavity within the article; removing the binder; and sintering the article to form the vacuum insulator, wherein the vacuum insulator defines a vacuum environment in the cavity.