Method of in-situ repair of an ultra-large single-piece casting

Patent metadata

Field	Value
Publication number	US-12097583-B2
Application number	US-202217729603-A
Country	US
Kind code	B2
Filing date	Apr 26, 2022
Priority date	Apr 26, 2022
Publication date	Sep 24, 2024
Grant date	Sep 24, 2024

Abstract

A method of repairing an ultra-large single-piece cast component of a vehicle body. The method includes the steps of locating a damaged portion of the cast component, determining an extent of the damaged portion of the ultra-large cast component, defining a cut-line sectioning off the damaged portion from an undamaged portion of the ultra-large cast component, cutting along the cut-line to excise the damaged portion from the undamaged portion of the ultra-large cast component, and joining a replacement piece to the undamaged portion of the ultra-large cast component. The replacement piece is fabricated based on the original manufacturer's geometry and dimensional data of the excised damaged portion. The undamaged portion of the ultra-large cast component remains on the vehicle body during the repair.

First claim

What is claimed is:

1. A method of repairing a cast component, comprising:
locating a damaged portion of the cast component;
determining an extent of the damaged portion of the cast component;
defining a cut-line sectioning off the damaged portion from an undamaged portion of the cast component;
cutting along the cut-line to excise the damaged portion from the undamaged portion of the cast component; and
joining a replacement piece to the undamaged portion of the cast component;
wherein joining the replacement piece to the undamaged portion of the cast component includes:
providing a plurality of bolt brackets on the replacement piece, wherein each of the plurality of bolt brackets defines a bolt through-hole;
drilling a plurality of bolt through-holes on the undamaged portion of the cast component, wherein the drilled bolt through-holes correspond to the bolt through-holes of the plurality of bolt brackets when the replacement piece is joined to the undamaged portion of the cast component; and
bolting the replacement piece onto the undamaged portion of the cast component.

2. The method of claim 1 , wherein determining the extent of the damaged portion of the cast component, comprising:
determining whether the damaged portion includes a load bearing structure; and
defining the cut-line to avoid cutting into the load bearing structure when the damaged portion does not include the load bearing structure.

3. The method of claim 2 , further comprises defining the cut-line to include a damaged load bearing structure portion when the damaged portion includes the load bearing structure.

4. The method of claim 3 , wherein joining the replacement piece includes one of welding the replacement piece to the undamaged portion of the cast component and bolting the replacement piece to the undamaged portion of the cast component.

5. The method of claim 1 , further comprising designing the replacement piece by using geometry and dimension data from a design specification of the cast component.

6. The method of claim 1 , wherein fabricating the replacement piece includes sand casting the replacement piece.

7. The method of claim 1 , wherein fabricating the replacement piece includes additive manufacturing the replacement piece based on original manufacturer design data.

8. The method of claim 7 , wherein additive manufacturing includes at least one of a friction stir additive manufacturing, a powder bed fusion (PBF), a direct energy deposition (DED), and a droplet on demand (DOD) using cast aluminum alloy feed stock and powders.

9. The method of claim 1 , wherein the cast component is a floor casting of a vehicle.

10. The method of claim 9 , wherein the cast component is a battery tray of a vehicle.

11. A method of in-situ repairing of an ultra-large casting of a vehicle body component, comprising:
locating a damaged portion of the ultra-large casting;
inspecting the damaged portion to determine whether a load bearing structure is damaged;
defining a cut-line to avoid the load bearing structure when the load bearing structure is not damaged and defining the cut-line to include a damaged load bearing structure portion when the load bearing structure is damaged;
cutting through the ultra-large casting at the cut-line to remove the damaged portion from an undamaged portion of the ultra-large casting; and
joining a replacement piece to the undamaged portion of the ultra-large casting to replace the damaged portion;
wherein joining the replacement piece to the undamaged portion of the ultra-large casting to replace the damaged portion includes:
providing a plurality of bolt brackets on the replacement piece, wherein each of the plurality of bolt brackets defines a bolt through-hole;
drilling a plurality of bolt through-holes on the undamaged portion of the cast component, wherein the drilled bolt through-holes correspond to the bolt through-holes of the plurality of bolt brackets when the replacement piece is joined to the undamaged portion of the ultra-large casting; and
bolting the replacement piece onto the undamaged portion of the cast component.

12. The method of claim 11 , wherein the ultra-large casting includes a width of at least 0.8 meter (m), a length of at least 1 m, and a height of at least 0.25 m.

13. The method of claim 11 , wherein joining the replacement piece to the undamaged portion of the ultra-large casting includes welding the replacement piece to the undamaged portion of the ultra-large casting when load bearing structure is damaged.

14. A method of in-situ repairing of an ultra-large die casting cast in a 2-piece die, comprising:
defining a cut-line sectioning off a damaged portion from an undamaged portion of the ultra-large casting;
excising the damaged portion by cutting along the cut-line;
fabricating a replacement piece; and
joining the replacement piece to the ultra-large casting in place of the excised damaged portion; and
wherein the ultra-large die casting includes a projected area of at least 0.3 m 2 on a projection plane parallel to a parting plane of the 2-piece die.

15. The method of claim 14 , further comprising:
determining a damaged load bearing structure;
defining the cut-line to include the damaged load bearing structure; and
one of welding the replacement piece to the ultra-large casting and bolting the replacement piece to the ultra-large casting.

16. The method of claim 14 , wherein joining the replacement piece to the ultra-large casting in place of the excised damaged portion includes:
providing a plurality of bolt brackets on the replacement piece, wherein each of the plurality of bolt brackets defines a bolt through-hole;
drilling a plurality of bolt through-holes on the undamaged portion of the cast component, wherein the drilled bolt through-holes correspond to the bolt through-holes of the plurality of bolt brackets when the replacement piece is joined to the undamaged portion of the cast component; and
bolting the replacement piece onto the undamaged portion of the cast component.

17. The method of claim 14 , wherein fabricating the replacement piece includes sand casting the replacement piece.

18. The method of claim 14 , wherein fabricating the replacement piece includes additive manufacturing the replacement piece based on original manufacturer design data.

19. The method of claim 14 , wherein the ultra-large die casting is a floor casting of a vehicle body.

20. The method of claim 19 , wherein the undamaged portion of the ultra-large casting is not removed from the vehicle body during joining the replacement piece to the ultra-large casting in place of the excised damaged portion.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Wilson Daniel J
• Wang Liang
• Wang Qigui
• Hess Devin R
• Wood Michelle A
• Shabbir Ali
• Daul Ronald C
• Gerard Dale A
• Melekian Gregory

Classifications

• B33Y10/00

  Processes of additive manufacturing · CPC title

• B33Y40/10

  Pre-treatment · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B22F7/062

  involving the connection or repairing of preformed parts · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title