Manufacturing a monolithic component with discrete portions formed of different metals

Patent metadata

Field	Value
Publication number	US-10422228-B2
Application number	US-201615096544-A
Country	US
Kind code	B2
Filing date	Apr 12, 2016
Priority date	Apr 12, 2016
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

Methods are provided for manufacturing a component. In one method, first metal material is cast into a first body. At least a portion of the first body is machined. Second metal material is cast onto at least the machined portion of the first body to form a monolithic second body. A first portion of the second body is formed by the first metal material, A second portion of the second body is formed by the second metal material. The second metal material is different from the first metal material.

First claim

What is claimed is:

1. A method for manufacturing a component, comprising:
casting first metal material into a first body;
machining at least a portion of the first body to remove select material from the first body; and
casting second metal material onto at least the machined portion of the first body to form a monolithic second body, a first portion of the second body formed by the first metal material, and a second portion of the second body formed by the second metal material, wherein the second metal material is different from the first metal material;
wherein, during the casting of the second metal material, a solidified portion of the first metal material melts and bonds to and/or alloys with an adjacent portion of the second metal material.

2. The method of claim 1 , wherein the casting of the first metal material comprises:
directing the first metal material, in molten form, into a casting mold; and
solidifying the first metal material to form the first body.

3. The method of claim 2 , wherein the first metal material is solidified to provide the first body with a substantially single crystal microstructure.

4. The method of claim 2 , further comprising:
removing the first body from the casting mold;
arranging the first body with a second casting mold;
wherein the second metal material is cast onto at least the machined portion of the first body within the second casting mold.

5. The method of claim 1 , wherein the casting of the second metal material comprises:
directing the second metal material, in molten form, into a casting mold, the molten second metal material contacting the machined portion of the first body; and
solidifying the second metal material to form the second body.

6. The method of claim 5 , wherein the first metal material and the second metal material are solidified to provide the second body with a substantially single crystal microstructure.

7. The method of claim 1 , further comprising:
machining at least a portion of the second body; and
casting third metal material onto at least the machined portion of the second body to form a monolithic third body, a first portion of the third body formed by the first metal material, a second portion of the third body formed by the second metal material, and a third portion of the third body formed by the third metal material, wherein the third metal material is different from at least the first metal material and/or the second metal material.

8. The method of claim 7 , wherein the third metal material is different from the first metal material and the second metal material.

9. The method of claim 7 , wherein the casting of the third metal material comprises:
directing the third metal material, in molten form, into a casting mold, the molten third metal material contacting the machined portion of the second body and the second metal material; and
solidifying the third metal material to form the third body.

10. The method of claim 9 , wherein the first metal material, the second metal material and the third metal material are solidified to provide the third body with a substantially single crystal microstructure.

11. The method of claim 1 , wherein the select material comprises at least one of overcast material, material with one or more defects and/or porous material.

12. The method of claim 1 , wherein the component is a rotor blade and comprises an airfoil extending radially out from a platform, and an interface between the first metal material and the second metal material is at the platform.

13. The method of claim 1 , wherein the component is a rotor blade and comprises an airfoil, and an interface between the first metal material and the second metal material is at a position along a radial span of the airfoil.

14. The method of claim 1 , wherein the component is a rotor blade and comprises an airfoil and a root, and an interface between the first metal material and the second metal material is within the root.

15. The method of claim 1 , wherein the machining comprises chemical milling, media blasting, mechanical machining, laser machining, grinding, sanding or buffing.

16. A method for manufacturing a component for a gas turbine engine, comprising:
directing molten first metal material into a first casting mold;
solidifying the first metal material to form a first body;
removing the first body from the first casting mold;
performing an operation on at least a portion of the first body;
arranging the first body with a second casting mold;
directing molten second metal material into the second casting mold, the molten second metal material contacting the portion of the first body, wherein the second metal material is different from the first metal material; and
solidifying the second metal material to form a second body, a first portion of the second body formed by the solidified first metal material, a second portion of the second body formed by the solidified second metal material, and the second metal material chemically bonded to the first metal material in an interface region between the first portion and the second portion.

17. The method of claim 16 , further comprising:
removing the second body from the second casting mold;
performing an operation on at least a portion of the second body;
arranging the second body with a third casting mold;
directing molten third metal material into the third casting mold, the molten third metal material contacting the portion of the second body and the second metal material, wherein the third metal material is different from the second metal material; and
solidifying the third metal material to form a third body, a first portion of the third body formed by the solidified first metal material, a second portion of the third body formed by the solidified second metal material, and a third portion of the third body formed by the solidified third metal material.

18. The method of claim 16 , wherein the operation comprises a machining operation.

19. The method of claim 16 , wherein the first metal material and the second metal material are solidified to provide the second body with a substantially single crystal microstructure.

20. A method for manufacturing a component of a gas turbine engine, comprising:
arranging a first body with a casting mold, the first body comprising first metal material, and the first body formed outside of the casting mold, wherein the first body is solid before and when arranged with the casting mold;
directing molten second metal material into the casting mold, the molten second metal material contacting at least a portion of the first body, wherein the second metal material is different from the first metal material; and
solidifying the second metal material to form a monolithic second body, a first portion of the second body formed by the solidified first metal material, a second portion of the second body formed by the solidified second metal material, and the second metal material alloyed with the first metal material in an interface region between the first portion and the second portion;
wherein the first metal material in the first portion of the second body has a substantially single crystal microstructure, and the second metal material in the second portion of the second body has a substantially single crystal microstructure.

21. The method of claim 20 , further comprising machining at least the portion of the first body.

Assignees

• United Technologies Corp

Inventors

• Castle Lea Kennard
• Bochiechio Mario P

Classifications

• B22D19/16

  for making compound objects cast of two or more different metals, e.g. for making rolls for rolling mills (casting compound ingots B22D7/02) · CPC title

• B22D19/04

  for joining parts · CPC title

• B22D19/0081

  pretreatment of the insert, e.g. for enhancing the bonding between insert and surrounding cast metal · CPC title

• B22D19/10

  Repairing defective or damaged objects by metal casting procedures (by other procedures B23P6/04; ingot mould B22D7/06; B22D19/06 takes precedence) · CPC title

• B22D25/02 Primary

  by its peculiarity of shape; of works of art {(cylinders, pistons B22D15/02)} · CPC title