Build plate integrated into additive manufactured component
During a formation method, a build plate is arranged within a build space. A first object is built onto the build plate within the build space using an additive manufacturing process. The object is fused to the build plate during the additive manufacturing process. At least the build plate is machined to form a component that includes a portion of the build plate and at least a portion of the first object.
1. A formation method, comprising:
arranging a build plate within a build space;
building a first object onto the build plate within the build space using an additive manufacturing process, the object fused to the build plate during the additive manufacturing process; and
machining at least the build plate to form a component comprising a portion of the build plate and at least a portion of the first object, the machining comprising removing a bottom portion of the build plate from the build plate to provide a second build plate that is discrete from the component.
2. The formation method of claim 1 , wherein the building of the object comprises building the first object layer-by-layer onto the build plate using the additive manufacturing process.
3. The formation method of claim 1 , wherein the additive manufacturing process comprises a powder bed fusion process.
4. The formation method of claim 1 , wherein the building of the first object comprises:
disposing a first layer of powder onto the build plate within the build space; and
selectively solidifying the first layer of powder using an energy beam to form a first portion of the first object that is fused to the build plate.
5. The formation method of claim 4 , wherein the building of the first object further comprises:
disposing a second layer of powder within the build space; and
selectively solidifying the second layer of powder using the energy beam to form a second portion of the first object that is fused to the first portion of the first object.
6. The formation method of claim 1 , further comprising:
building a second object onto the build plate within the build space using the additive manufacturing process;
the second object fused to the build plate during the additive manufacturing process; and
the component further comprising at least a portion of the second object.
7. The formation method of claim 6 , wherein the second object is discrete form the first object.
8. The formation method of claim 6 , wherein the build plate structurally connects the second object to the first object.
9. The formation method of claim 6 , wherein the second object circumscribes and is spaced radially outboard from the first object.
10. The formation method of claim 6 , wherein
the at least a portion of the first object forms a part of a gas turbine engine;
the at least a portion of the second object forms a part of a vehicle body in which the gas turbine engine is housed; and
the portion of the build plate forms a support structure extending between and connected to the gas turbine engine and the vehicle body.
11. The formation method of claim 10 , wherein the part of the gas turbine engine comprises an inlet section of the gas turbine engine.
12. The formation method of claim 1 , wherein
the at least a portion of the first object forms a part of a gas turbine engine case; and
the portion of the build plate forms a bulkhead projecting radially out from the gas turbine engine case.
13. The formation method of claim 1 , further comprising:
arranging the second build plate within the build space;
building a second object onto the second build plate within the build space using the additive manufacturing process, the second object fused to the second build plate; and
machining at least the second build plate to form a second component comprising a portion of the second build plate and at least a portion of the second object.
14. The formation method of claim 1 , wherein the machining comprises removing a peripheral portion of the build plate to form an outer peripheral boundary of the component.
15. The formation method of claim 1 , wherein the machining comprises forming one or more apertures into the build plate.
16. The formation method of claim 1 , wherein
the build plate comprises build plate material; and
the first object comprises object material that is different than the build plate material.
17. The formation method of claim 1 , wherein the build plate and the first object comprise a common material.
18. The formation method of claim 1 , wherein
an aircraft assembly includes an aircraft body, a gas turbine engine and a support structure;
the gas turbine engine comprises an engine case, and the gas turbine engine is housed within the aircraft body;
the support structure extends between and is connected to the aircraft body and the engine case, the support structure supports the gas turbine engine within the aircraft body, and the support structure and the engine case are included in a monolithic body; and
the monolithic body comprises the component.
19. The formation method of claim 18 , wherein
the engine case forms an outer flowpath wall;
the gas turbine engine further comprises an inner flowpath wall and a plurality of vanes connected to and extending between the inner flowpath wall and the outer flowpath wall; and
the inner flowpath wall and the plurality of vanes are included in the monolithic body.
20. The formation method of claim 1 , wherein
an aircraft assembly includes an intake section for a gas turbine engine and a bulkhead projecting out from the intake section;
the intake section includes an outer flowpath wall, an inner flowpath wall and a plurality of vanes connected to and extending between the inner flowpath wall and the outer flowpath wall;
the bulkhead is formed integral with the intake section as a single, unitary body; and
the single, unitary body comprises the component.