ADDITIVE MANUFACTURING A PART USING STRUTS
The disclosure presents a combination of additive manufacturing processes that could be used to produce different portions or features of a hybrid structure, such that a first additive manufacturing process could be used to form a complex seed part or first section of the hybrid component, and a different additive manufacturing component could be used to form a second section of the hybrid component. When two components are manufactures, a mandrel could be assembled into the first component to provide rigidity and resistance to deformation of the first component, even during and after formation of the second component on the interface surface of the first component using a second additive manufacturing process. Finally, struts could be formed directly on a base plate and before formation of the component so that the base plate temperature could increase to be in equilibrium with the temperature of the newly deposited material.
1 . A method of additively manufacturing a component comprising:
forming a plurality of struts on a base plate, the forming of the plurality of struts causing the base plate to heat;
continuing formation of the plurality of struts until a first temperature of the plurality of struts is substantially equal to a second temperature of the base plate; and
forming a component on the plurality of struts only when the first temperature is substantially equal to the second temperature,
wherein the plurality of struts is configured to delay thermal stress formation in the component.
2 . The method of claim 1 , wherein each strut of the plurality of struts is circumferentially spaced apart from an adjacent strut of the plurality of struts.
3 . The method of claim 2 , wherein each strut of the plurality of struts is substantially equally spaced apart around the circumference of the plurality of struts.
4 . The method of claim 1 , wherein the first temperature and the second temperature are in equilibrium between 80 degrees Celsius and 120 degrees Celsius.
5 . The method of claim 4 , wherein the first temperature and the second temperature are in equilibrium at about 100 degrees Celsius.
6 . The method of claim 1 , wherein the plurality of struts extends between 2 millimeters and 15 millimeters from the base plate.
7 . The method of claim 6 , wherein the plurality of struts extends about 10 millimeters from the base plate.
8 . The method of claim 1 , further comprising removing the plurality of struts and the cylindrical component from the base plate.
9 . The method of claim 8 , further comprising machining the plurality of struts to form a datum surface.
10 . The method of claim 9 , further comprising machining the cylindrical component to remove the plurality of struts.
11 . The method of claim 1 , wherein the cylindrical component further comprises a first cylindrical feature and a second cylindrical feature, and a second plurality of struts that extends between the first feature and the second feature, and
wherein the second plurality of struts is configured to reduce circumferential distortion between the first cylindrical feature and the second cylindrical feature.
12 . The method of claim 11 , wherein each strut of the second plurality of struts is circumferentially spaced apart from an adjacent strut of the second plurality of struts.
13 . The method of claim 11 , further comprising removing the second plurality of struts from the cylindrical component.