Reinforced composite assemblies and methods of manufacturing the same

Patent metadata

Field	Value
Publication number	US-11780185-B2
Application number	US-202117193010-A
Country	US
Kind code	B2
Filing date	Mar 5, 2021
Priority date	Mar 5, 2021
Publication date	Oct 10, 2023
Grant date	Oct 10, 2023

Abstract

A reinforced composite assembly includes a first sheet made of carbon fiber and having a first perimeter, a second sheet made of a non-carbon fiber material and having a second perimeter, wherein the second sheet is disposed atop the first sheet within the first perimeter, and a metallic plate having a third perimeter, wherein the metallic plate is disposed atop the second sheet within the second perimeter. The metallic plate has a plurality of holes formed therein about a perimeter of the metallic plate and defining a plurality of respective bridge portions between each of the holes and an adjacent outer edge of the metallic plate, and/or a plurality of extensions extending outward from a main portion of the metallic plate. A first arrangement of thread stitching secures each of the bridge portions and extensions to the second sheet or to the first and second sheets.

First claim

What is claimed is:

1. A reinforced composite assembly, comprising:
a first sheet made of carbon fiber and having a first perimeter;
a second sheet made of a non-carbon fiber material and having a second perimeter, wherein the second sheet is disposed atop the first sheet within the first perimeter;
a metallic plate having a third perimeter, wherein the metallic plate is disposed atop the second sheet within the second perimeter, the metallic plate having
a plurality of extensions extending outward from a main portion of the metallic plate; and

a first arrangement of thread stitching securing each of the extensions to the second sheet or to the first and second sheets.

2. A reinforced composite assembly according to claim 1 , wherein each of the plurality of extensions is shaped as one of a T-shape, an L-shape, a U-shape having first and second ends wherein each of the first and second ends is contiguous with the main portion, a key head shape having a straight portion extending outward from the main portion and terminating in a closed loop portion, and a tab having one or more through-holes therein.

3. A reinforced composite assembly according to claim 1 , wherein the metallic plate includes a plurality of holes therein about a perimeter of the metallic plate and defining a plurality of respective bridge portions between each of the holes and an adjacent outer edge of the metallic plate, wherein each of the holes is shaped as one of a circular hole, an ellipsoidal hole, a square hole, a rounded straight slot, and a rectangular slot.

4. A reinforced composite assembly according to claim 3 , wherein the metallic plate includes at least one aperture therethrough located inward from the plurality of holes.

5. A reinforced composite assembly according to claim 1 , further comprising:
a metallic member having a first portion thereof attached to the metallic plate and a second portion thereof extending away from the metallic plate.

6. A reinforced composite assembly according to claim 1 , wherein the first sheet has a first area, the second sheet has a second area smaller than the first area, and the metallic plate has a third area smaller than the second area.

7. A reinforced composite assembly according to claim 1 , further comprising:
a second arrangement of thread stitching securing the second sheet to the first sheet.

8. A reinforced composite assembly according to claim 1 , wherein the first arrangement of thread stitching comprises a plurality of individual stitches, wherein each individual stitch extends across at least a portion of a respective one of the plurality of extensions.

9. A method of manufacturing a reinforced composite assembly, comprising:
disposing a metallic plate having a third perimeter onto a second sheet made of a non-carbon fiber material and having a second perimeter, wherein the metallic plate is disposed within the second perimeter and has a plurality of extensions extending outward from a main portion of the metallic plate thereby producing a metallic plate-second sheet sub-assembly;
placing the metallic plate-second sheet sub-assembly onto a first sheet made of carbon fiber and having a first perimeter, wherein the metallic plate-second sheet sub-assembly is disposed within the first perimeter and the second sheet separates the metallic plate from the first sheet; and
securing each of the extensions to the second sheet or to the first and second sheets using a first arrangement of thread stitching, thereby producing a reinforced preform assembly.

10. A method according to claim 9 , further comprising:
setting the reinforced preform assembly into a mold cavity;
closing a mold plug against the mold cavity to form a closed mold;
injecting a resin into the closed mold so as to saturate at least a selected portion of the reinforced preform assembly with the resin, thereby creating a saturated reinforced preform assembly;
opening the closed mold by separating the mold plug from the mold cavity so as to expose the saturated reinforced preform assembly; and
removing the saturated reinforced preform assembly from the mold cavity.

11. A method according to claim 10 , further comprising:
applying heat to the saturated reinforced preform assembly while in the closed mold until a predetermined level of cure of the resin is produced.

12. A method according to claim 10 , wherein the mold cavity includes a guide pin extending upward from a mold surface and the metallic plate includes an aperture therethrough configured for mating with the guide pin.

13. A method according to claim 10 , wherein a respective plug seal is disposed in at least one of the mold cavity and the mold plug, wherein each respective plug seal is configured to be biased against a tapped hole within a tubular member attached to the metallic plate when the mold is closed.

14. A method according to claim 10 , wherein a resin seal is disposed between the mold cavity and the reinforced preform assembly and around an aperture formed in the metallic plate when the reinforced preform assembly is positioned into the mold cavity.

15. A method according to claim 9 , wherein the first sheet has a first area, the second sheet has a second area smaller than the first area, and the metallic plate has a third area smaller than the second area.

16. A reinforced composite assembly, comprising:
a first sheet made of carbon fiber and having a first perimeter;
a first layer of non-carbon fiber material having a second perimeter, wherein the first layer is disposed atop the first sheet within the first perimeter;
a metallic plate having a third perimeter, wherein the metallic plate is disposed atop the first layer within the second perimeter, the metallic plate having a plurality of extensions extending outward from a main portion of the metallic plate;
a second layer of non-carbon fiber material having a fourth perimeter, wherein the second layer is disposed atop the metallic plate such that the metallic plate is disposed within the fourth perimeter; and
a first arrangement of thread stitching securing each of the extensions to the first layer or to the first sheet and the first layer.

17. A reinforced composite assembly according to claim 16 , wherein the first arrangement of thread stitching further secures the first sheet with the first and second layers.

18. A reinforced composite assembly according to claim 16 , wherein the first and second layers are formed from a single sheet of non-carbon fiber material folded so as to dispose the first and second layers in facing relationship with each other.

19. A reinforced composite assembly according to claim 16 , wherein the metallic plate and the second layer include respective first and second apertures therethrough, wherein the first and second apertures overlap with each other such that an entirety of the first aperture projects through the second aperture.

20. A reinforced composite assembly according to claim 16 , further comprising:
a second arrangement of thread stitching securing together at least one of the first and second layers with the first sheet.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Aitharaju Venkateshwar R
• Carlos Princess Len
• Golm Erik B
• Wathen Terrence

Classifications

• B29C70/72 Primary

  Encapsulating inserts having non-encapsulated projections, e.g. extremities or terminal portions of electrical components {(B29C70/742 takes precedence)} · CPC title

• B29C70/682

  Preformed parts characterised by their structure, e.g. form · CPC title

• B29C70/683

  Pretreatment of the preformed part, e.g. insert · CPC title

• B29C71/02

  Thermal after-treatment {(B29C71/0063 and B29C71/0072 take precedence)} · CPC title

• B32B3/266

  characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12 · CPC title