Multi-material golf club head
US-2019275390-A1 · Sep 12, 2019 · US
US12508478B1 · US · B1
| Field | Value |
|---|---|
| Publication number | US-12508478-B1 |
| Application number | US-202318368774-A |
| Country | US |
| Kind code | B1 |
| Filing date | Sep 15, 2023 |
| Priority date | Sep 21, 2022 |
| Publication date | Dec 30, 2025 |
| Grant date | Dec 30, 2025 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A composite material for a component of a golf club head is disclosed herein. The composite material includes a composite layers and at least one an interlaminar layer that includes one of vertically aligned carbon nanotubes, Z-Axis aligned carbon fibers or graphene platelets. In one preferred embodiment, the golf club head component is a face component.
Opening claim text (preview).
We claim as our invention the following: 1 . A composite material for a component of a golf club head, the composite material comprising: a first composite layer; a second composite layer; and an interlaminar layer composed of vertically aligned carbon nanotubes; wherein the first composite layer and the second composite layer comprise a plurality of plies, each of the plurality of plies a unidirectional orientation, a bi-axial orientation or a tri-axial orientation; wherein a laminate comprises a structure formed from the first composite layer, the second composite layer and the interlaminar layer; wherein an additive laminate ratio = ∑ k = 1 m - 1 Area Additive k ∑ k = 1 m Area Ply k wherein m=a total number of plies, wherein an Area_Ply k is the area of each composite ply (k) in the laminate, wherein an Area Additive (k) is the area of the reinforcement present between offsetting plies (k and k+1), wherein the additive laminate ratio of the composite material ranges between 0.05 and 0.9. 2 . The composite material according to claim 1 wherein each of the first composite layer and the second composite layer has a fabric area weight ranging from 20 gsm to 500 gsm. 3 . The composite material according to claim 1 wherein each the first composite layer and the second composite layer comprises at least one of a carbon fiber, fiberglass fiber, or aramid fiber. 4 . A composite material for a component of a golf club head, the composite material comprising: a first composite layer; a second composite layer; and an interlaminar layer comprising one of vertically aligned carbon nanotubes, Z-Axis aligned carbon fibers or graphene platelets; wherein the first composite layer and the second composite layer comprise a plurality of plies, each of the plurality of plies a unidirectional orientation, a bi-axial orientation or a tri-axial orientation; wherein a laminate comprises a structure formed from the first composite layer, the second composite layer and the interlaminar layer; wherein an additive laminate ratio = ∑ k = 1 m - 1 Area Additive k ∑ k = 1 m Area Ply k wherein m=a total number of plies, wherein an Area_Ply k is the area of each composite ply (k) in the laminate, wherein an Area Additive (k) is the area of the reinforcement present between offsetting plies (k and k+1), wherein the additive laminate ratio of the composite material ranges between 0.05 and 0.9. 5 . The composite material according to claim 4 wherein each of the first composite layer and the second composite layer has a fabric area weight ranging from 20 gsm to 500 gsm. 6 . The composite material according to claim 4 wherein each the first composite layer and the second composite layer comprises at least one of a carbon fiber, fiberglass fiber, or aramid fiber. 7 . The composite material according to claim 4 wherein the interlaminar layer comprises Z-Axis aligned carbon fibers and an average thickness of the Z-Axis aligned carbon fibers between the first composite layer and the second composite layer ranges from 0.003 inch to 0.060 inch. 8 . The composite material according to claim 4 wherein the interlaminar layer comprises Z-Axis aligned carbon fibers and a fabric area weight of the interlaminar layer ranges from 10 gsm to 300 gsm.
with reinforcing fibres, e.g. carbon, polyamide fibres · CPC title
Synthetic resin · CPC title
Weight, e.g. weight per square meter · CPC title
Two or more layers · CPC title
bi-axially · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.