Method and assembly for forming components having an internal passage defined therein

Patent metadata

Field	Value
Publication number	US-10099276-B2
Application number	US-201514972390-A
Country	US
Kind code	B2
Filing date	Dec 17, 2015
Priority date	Dec 17, 2015
Publication date	Oct 16, 2018
Grant date	Oct 16, 2018

Abstract

A method of forming a component having an internal passage defined therein includes positioning a jacketed core with respect to a mold. The jacketed core includes a hollow structure that includes an interior portion shaped to define at least one interior passage feature of the internal passage. The jacketed core also includes an inner core disposed within the hollow structure and complementarily shaped by the interior portion of the hollow structure. The method also includes introducing a component material in a molten state into a cavity of the mold to form the component, such that the inner core defines the internal passage including the at least one interior passage feature defined therein.

First claim

What is claimed is:

1. A method of forming a component having an internal passage defined therein, said method comprising:
positioning a jacketed core with respect to a mold, wherein the jacketed core includes:
a hollow structure formed from a first material that extends from an interior portion of the hollow structure to substantially an entire outer perimeter of the hollow structure, wherein the interior portion is shaped to define at least one interior passage feature of the internal passage, and wherein the first material is metallic; and
an inner core disposed within the hollow structure and complementarily shaped by the interior portion of the hollow structure;

introducing a component material in a molten state into a cavity of the mold, such that a portion of the jacketed core is submerged, and such that the component material in the molten state contacts the first material along substantially the entire outer perimeter of the submerged portion of the jacketed core to form the component, such that the inner core defines the internal passage including the at least one interior passage feature defined therein;
cooling the component material in the cavity to form the component; and
removing the inner core from the component to form the internal passage.

2. The method of claim 1 , further comprising, prior to disposing an inner core material within the hollow structure, pre-forming the interior portion of the hollow structure such that the interior portion is shaped to define a selected shape of the at least one interior passage feature.

3. The method of claim 2 , wherein said pre-forming the interior portion of the hollow structure comprises crimping the hollow structure at a plurality of locations to define a plurality of indentations, the indentations shaped to define the at least one interior passage feature when the component is formed.

4. The method of claim 2 , wherein said pre-forming the interior portion of the hollow structure comprises using a tube press.

5. The method of claim 4 , wherein said using the tube press further comprises bending the hollow structure to match a preselected nonlinear shape of the internal passage.

6. The method of claim 4 , wherein said using the tube press further comprises forming a non-circular cross-sectional perimeter of at least a portion of the hollow structure corresponding to a selected non-circular cross-sectional perimeter of at least a portion of the internal passage.

7. The method of claim 2 , wherein said pre-forming the interior portion of the hollow structure comprises forming the hollow structure using an additive manufacturing process.

8. The method of claim 7 , wherein said forming the hollow structure comprises using at least one of a direct metal laser melting (DMLM) process, a direct metal laser sintering (DMLS) process, and a selective laser sintering (SLS) process.

9. The method of claim 1 , wherein said positioning the jacketed core comprises positioning the jacketed core that includes a plurality of indentations defined on the hollow structure, the indentations shaped to define the at least one interior passage feature as a plurality of ridges.

10. The method of claim 1 , wherein said positioning the jacketed core comprises positioning the jacketed core that includes a plurality of indentations defined on the hollow structure, the indentations shaped to define the at least one interior passage feature as a plurality of dimples.

11. The method of claim 1 , wherein said positioning the jacketed core comprises positioning the jacketed core including the interior portion of the hollow structure shaped to define the at least one interior passage feature as at least one of a sharp-edged bead, a smooth-edged bead, and a rifled groove.

12. The method of claim 1 , wherein said positioning the jacketed core comprises positioning the jacketed core including the interior portion of the hollow structure shaped to define the at least one interior passage feature as at least one louvered interior passage feature.

13. The method of claim 12 , wherein said positioning the jacketed core comprises positioning the jacketed core including the interior portion that defines a plurality of obliquely disposed convolution faces, wherein each convolution face includes a plurality of louvers.

14. The method of claim 13 , wherein said positioning the jacketed core comprises positioning the jacketed core including the interior portion that defines each of the convolution faces extending from one of a plurality of peaks to one of a plurality of valleys of the louver structure, the peaks and the valleys defined on opposite sides of the hollow structure such that each of the peaks and the valleys lies proximate the outer perimeter of the hollow structure.

15. The method of claim 1 , wherein said positioning the jacketed core comprises positioning the jacketed core including the interior portion of the hollow structure shaped to define at least one complementary feature of the inner core, wherein the component material in the molten state couples against the at least one complementary feature of the inner core to shape the at least one interior passage feature.

Assignees

• Gen Electric

Inventors

• Moricca Timothy Michael
• Rutkowski Stephen Francis
• Moroso Joseph Leonard
• Willett Jr Fred Thomas

Classifications

• F05D2260/22141

  using fins or ribs · CPC title

• F05D2240/127

  Vortex generators, turbulators, or the like, for mixing · CPC title

• F05D2230/211

  by precision casting, e.g. microfusing or investment casting · CPC title

• 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

• B22D19/0072

  for making objects with integrated channels · CPC title