Coated Casting Core and Manufacture Methods

Patent metadata

Field	Value
Publication number	US-2016296996-A1
Application number	US-201415036216-A
Country	US
Kind code	A1
Filing date	Oct 28, 2014
Priority date	Nov 18, 2013
Publication date	Oct 13, 2016
Grant date	—

Abstract

A casting core assembly ( 140 ) includes a metallic core ( 144, 146, 148 ), a ceramic core ( 142 ) having a compartment ( 186 ) in which the portion of the metallic core is received, and a ceramic coating ( 260 ) at least partially covering the metallic core and the ceramic core.

First claim

1 . A process for forming a casting core assembly, the assembly comprising:
a metallic core; a ceramic core having a compartment in which a portion of the metallic core is received; and a ceramic coating at least partially covering the metallic core and the ceramic core,
the process comprising:
applying the ceramic coating by chemical vapor deposition.

2 . The process of claim 1 further comprising:
forming a ceramic adhesive joint between the portion and the ceramic core.

3 . The process of claim 1 wherein:
the ceramic core is an airfoil feedcore; and
the metallic core is an outlet core.

4 . The process of claim 1 wherein:
the metallic core is a refractory metal core.

5 . The process of claim 1 wherein:
the ceramic core is silica-based.

6 . The process of claim 1 wherein:
the coating comprises at least 50% mullite and/or alumina by weight.

7 . The process of claim 1 wherein:
the coating is a single sole layer atop both the ceramic core and the metallic core.

8 . A process for forming a pattern, the method comprising:
forming, according to claim 1 , the assembly of; and partially embedding the assembly in a wax material.

9 . A process for forming a mold, the method comprising:
forming, according to claim 1 , the assembly; and forming a shell, the metallic core having a distal portion embedded in the shell and the metallic core spanning a gap between the ceramic core and the shell.

10 . The process of claim 1 , comprising:
molding the ceramic core over the portion of the metallic core.

11 . The process of claim 10 further comprising:
applying an additional ceramic coating to the metallic core.

12 . The process of claim 10 wherein:
the applying of the coating is to the ceramic core in an unfired state.

13 . (canceled)

14 . The process of claim 10 further wherein:
the metallic core comprises a by-weight majority of one or more refractory metals.

15 . The process of claim 10 being a portion of a pattern-forming process, the pattern-forming process further comprising:
overmolding a main pattern-forming material to the core assembly in a pattern-forming die.

16 . The process of claim 15 being a portion of a shell-forming process, the shell-forming process further comprising:
shelling the pattern; and
removing the main pattern-forming material and hardening the shell.

17 . The process of claim 16 being a portion of a casting process, the casting process further comprising:
introducing molten metal to the shell;
allowing the metal to solidify; and
destructively removing the shell and the core assembly.

18 . The process of claim 17 wherein:
the ceramic core forms a feed passageway in an airfoil; and
the metallic core forms an outlet passageway from the feed passageway to a pressure side or a suction side of the airfoil.

19 . The process of claim 1 wherein:
the ceramic coating is applied to an average thickness of 0.5 mil to 1.5 mil.

20 . The process of claim 1 wherein:
the ceramic coating is applied to cover essentially all of exposed portions of both the metallic core and the ceramic core.

21 . A casting core assembly comprising:
a metallic core; a ceramic core having a compartment in which the portion of the metallic core is received; and a ceramic coating at least partially covering the metallic core and the ceramic core, the ceramic coating having an average thickness of 0.5 mil to 1.5 mil and covering essentially all of the exposed portions of both the metallic core and the ceramic core.

Assignees

• United Technologies Corp

Inventors

• Castle Lea K
• Spangler Brandon W

Classifications

• B22D25/02

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

• B22C9/24

  for hollow articles · CPC title

• B22C9/12

  Treating moulds or cores, e.g. drying, hardening · CPC title

• F05D2230/21

  by casting · CPC title

• B22C7/02

  Lost patterns · CPC title