Casting cores and manufacture methods

US9421606B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9421606-B2
Application numberUS-201314432790-A
CountryUS
Kind codeB2
Filing dateJul 24, 2013
Priority dateOct 12, 2012
Publication dateAug 23, 2016
Grant dateAug 23, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A casting core assembly ( 140 ) includes a metallic core ( 144, 146, 148; 360; 380; 400 ) and a ceramic core ( 142 ). A protuberant portion ( 184 ) of a metallic core is received in compartment ( 186 ) of the ceramic core.

First claim

Opening claim text (preview).

What is claimed is: 1. A casting core assembly comprising: a metallic core comprising: a thickened portion comprising a metallic laminate; and a thin portion extending from the thickened portion; a ceramic core having a compartment in which the thickened portion is received; and an adhesive joint between the thickened portion and the ceramic core. 2. The assembly of claim 1 wherein: the adhesive joint is a ceramic adhesive joint between the thickened portion and the ceramic core. 3. The assembly of claim 1 wherein: the ceramic core is an airfoil feedcore; and the metallic core is an outlet core. 4. The assembly of claim 1 wherein: the thickened portion is of increasing thickness from a proximal end toward a distal end. 5. The assembly of claim 1 wherein: the thickened portion has flat first and second faces. 6. The assembly of claim 1 wherein: a main sheet of the metallic laminate extends along both the thickened portion and the thin portion; and a plurality of additional sheets of the metallic laminate extend only along the thickened portion. 7. A pattern comprising: the assembly of claim 1 ; a wax material in which the assembly is partially embedded. 8. A mold comprising: the assembly of claim 1 ; and 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. 9. A process for forming the assembly of claim 1 , the process comprising: inserting the thickened portion of the metallic core into the compartment in the ceramic core. 10. The process of claim 9 further comprising: securing the thickened portion to the ceramic core. 11. The process of claim 10 wherein: the securing comprises introducing a ceramic adhesive between the thickened portion and the compartment. 12. The process of claim 10 wherein: the securing comprises introducing a non-ceramic adhesive between the thickened portion and the compartment. 13. The process of claim 9 further comprising: applying a coating to the metallic core. 14. The process of claim 9 further comprising: forming the thickened portion by laminating a plurality of additional sheets to a main sheet. 15. The process of claim 14 wherein: the laminating comprises welding. 16. The process of claim 14 wherein: the plurality of additional sheets are asymmetrically applied to the main sheet. 17. The process of claim 14 wherein: the plurality of additional sheets are symmetrically applied to the main sheet. 18. The process of claim 14 further comprising: machining the laminated sheets. 19. The process of claim 9 further wherein: the metallic core comprises a by-weight majority of one or more refractory metals. 20. The process of claim 9 being a portion of a pattern-forming process and further comprising: overmolding a main pattern-forming material to the core assembly in a pattern-forming die. 21. A casting core assembly comprising: a metallic core comprising: a thickened portion comprising a metallic laminate and having flat first and second faces; and a thin portion extending from the thickened portion, the first and second faces being not parallel and converging in a direction away from the direction in which the thin portion extends from the thickened portion; and a ceramic core having a pre-formed compartment in which the thickened portion is received. 22. A casting core assembly comprising: a metallic core comprising: a thickened portion comprising a metallic laminate and having first and second faces; and a thin portion extending from the thickened portion, the thin portion formed by a first sheet and the thickened portion comprising multiple stacked additional sheets on at least a first face of the first sheet; a ceramic core having a pre-formed compartment in which the thickened portion is received and complementary in shape to the thickened portion; and an adhesive joint between the thickened portion and the ceramic core. 23. The casting core assembly of claim 22 wherein: a face of the thickened portion is formed by a second face of the first sheet.

Assignees

Inventors

Classifications

  • Use of lost patterns · CPC title

  • B22C9/103Primary

    Multipart cores · CPC title

  • Installation of cores · CPC title

  • Cores; Manufacture or installation of cores {(breaker cores B22C9/084)} · CPC title

  • Lost patterns · CPC title

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Frequently asked questions

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What does patent US9421606B2 cover?
A casting core assembly ( 140 ) includes a metallic core ( 144, 146, 148; 360; 380; 400 ) and a ceramic core ( 142 ). A protuberant portion ( 184 ) of a metallic core is received in compartment ( 186 ) of the ceramic core.
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification B22C9/103. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Aug 23 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).