An assembly for carrying parts to be sintered through a sintering furnace includes a boat formed of a refractory metal or metal alloy and including a base and, sidewalls, and a plurality of vertically stacked ceramic tiles disposed within the boat, each of the plurality of vertically stacked ceramic tiles sized to carry a plurality of the parts to be sintered through the sintering furnace.

An assembly for carrying parts to be sintered through a sintering furnace includes a boat formed of a refractory metal or metal alloy and including a base and, sidewalls, and a plurality of vertically stacked ceramic tiles disposed within the boat, each of the plurality of vertically stacked ceramic tiles sized to carry a plurality of the parts to be sintered through the sintering furnace.

Methods of fabricating a turbomachine component and turbomachine components are provided. The method includes irradiating a layer of powder in a powder bed to form a fused region. The powder is disposed on a build plate. The method further includes a step of providing a subsequent layer of powder over the powder bed by passing a recoater arm over the powder bed from a first side of the powder bed. The method further includes repeating the irradiating and providing steps until a turbine nozzle assembly is formed on the build plate. The turbine nozzle assembly includes the turbine nozzle and a plurality of heat fins disposed within the turbine nozzle. The plurality of heat fins transfer heat away from a thermally sensitive portion of the turbine nozzle.

A tooling assembly and method of aligning a plurality of components for a repair process in an additive manufacturing machine includes positioning the plurality of components such that a repair surface of each of the plurality of components contacts an alignment plate, e.g., under the force of gravity or using biasing members. The method further includes surrounding the alignment plate with containment walls to define a reservoir around the plurality of components and dispensing a fill material, such as wax or a potting material, into the reservoir which is configured for fixing a relative position of the plurality of components when the fill material is solidified.

Methods of fabricating a turbomachine component and turbomachine components are provided. The method includes irradiating a layer of powder in a powder bed to form a fused region. The powder is disposed on a build plate. The method further includes a step of providing a subsequent layer of powder over the powder bed by passing a recoater arm over the powder bed from a first side of the powder bed. The method further includes repeating the irradiating and providing steps until a turbine nozzle assembly is formed on the build plate. The turbine nozzle assembly includes the turbine nozzle and a plurality of heat fins disposed within the turbine nozzle. The plurality of heat fins transfer heat away from a thermally sensitive portion of the turbine nozzle.

The disclosed technology generally relates to packaging a quartz crystal, and more particularly to bonding a quartz crystal using sintering silver paste. In one aspect, a method of packaging a quartz crystal comprises attaching a quartz crystal to a package substrate using one or more silver paste layers comprising silver particles. The method additionally comprises sintering the silver paste in a substantially oxygen-free atmosphere and at a sintering temperature sufficient to cause sintering of the silver particles. The sintering is such that the quartz crystal exhibits a positive drift in resonance frequency of the quartz crystal over time. The method further comprises hermetically sealing the quartz crystal in the package substrate.

Described is a build chamber for an additive manufacturing apparatus for forming a three-dimensional article layer by layer from a powder. The build chamber comprises a build chamber base body and said build chamber base body is formed by at least two segments telescopically coupled together.

A method for making a product or a part for a product wherein the product or part is made in a process using additive manufacture and requires sintering, the method comprising producing a support component with a shape complementary to the product or part, in an associated process, also using additive manufacture; and supporting the product or part during sintering by fitting the product or part into the complementary shape prior to placing in the furnace for sintering.

A method for making a product or a part for a product wherein the product or part is made in a process using additive manufacture and requires sintering, the method comprising producing a support component with a shape complementary to the product or part, in an associated process, also using additive manufacture; and supporting the product or part during sintering by fitting the product or part into the complementary shape prior to placing in the furnace for sintering.

An example sinter system includes a sinter gas inlet at a sinter furnace for a sinter gas, a tracer gas inlet at the sinter furnace for a tracer gas different from the sinter gas, and an outlet at the sinter furnace to output the sinter gas and the tracer gas. The example sinter system further includes: a support structure to support a sample green object in the sinter furnace, an opening at the support structure connected to the tracer gas inlet, the opening to output the tracer gas into the sinter furnace, and a detector to: determine an amount of the tracer gas flowing through the outlet during a sinter process as a sample green object positioned on the support structure changes shape during the sinter process with respect to the opening and modifies a flow rate of the tracer gas to the outlet; and determine when to stop the sinter process based on a determined amount of the tracer gas.