IP Library › Granted Patent US 12,365,418
Granted Patent B2
US 12,365,418 · App. 18/089,950 · Granted Jul 22, 2025

Composite structures and methods of forming composite structures

Inventors: Benjamin K. Bosworth (Morrison, CO); Matthew T. Giaraffa (Golden, CO); Samuel D. Nichols (Lakewood, CO); Togay Yuvanc (Lakewood, CO)
Assignee: ASTRO TECH CO., LTD.
B62K19/16B29C70/222B32B1/08B32B3/08B32B5/26B29L2031/3091B32B2260/023B32B2260/046
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Quick Facts
Patent No.
US 12,365,418
App. No.
18/089,950
Granted
Jul 22, 2025
Kind
B2
Abstract

Composite structures and methods of forming composite structures are provided. A composite structure as disclosed herein incorporates one or more composite structure components, such as composite panels and composite inserts. A composite panel is formed from one or more sheets of fiber reinforced thermoplastic material. Composite inserts can include one or more composite blocks or braided sleeves. A composite block can be formed as a stacked or molded structure from trimmings or waste produced during the formation of the composite structures. A braided sleeve can include a seamless, woven sleeve formed of reinforcing fibers and thermoplastic threads. In a completed composite structure, composite inserts are at least partially disposed within a volume defined by surfaces of composite panels. The various composite structures and inserts can be given a final shape and can be fused to one another in a molding and fusing step.

Claims (16)

1. A composite structure, comprising:

a first component, wherein the first component includes a panel incorporating a plurality of sheets of fiber reinforced thermoplastic material;

a second component, wherein the second component includes a panel incorporating a plurality of sheets of fiber reinforced thermoplastic material;

a first composite insert, wherein the first composite insert includes a plurality of reinforcing fibers and a thermoplastic material, and wherein at least a portion of the first composite insert is located within a first portion of an interior volume located between an interior surface of the first component and an interior surface of the second component; and

a second composite insert, wherein the second composite insert includes a plurality of reinforcing fibers and a thermoplastic material, wherein at least a portion of the second composite insert is located within a second portion of the interior volume located between the interior surface of the first component and the interior surface of the second component, wherein the first and second components are fused to one another along at least a first joint portion, wherein the first composite insert is fused to at least one of the first and second components, and wherein the second composite insert is fused to at least one of the first and second components.

2. The composite structure of claim 1 , wherein the first composite insert includes surfaces in contact with an interior surface of the first component and an interior surface of the second component.

3. The composite structure of claim 1 , wherein the first composite insert has a three dimensional shape that at least partially conforms to a shape of the first portion of the interior volume, and wherein the second composite insert has a three dimensional shape that at least partially conforms to a shape of the second portion of the interior volume.

4. The composite structure of claim 1 , further comprising a third composite insert, wherein the first composite insert is a composite block, wherein the second composite insert is a composite block, and wherein the third composite insert is a braided sleeve.

5. The composite structure of claim 4 , wherein at least a first section of the interior volume is not round, wherein a portion of an exterior surface of the braided sleeve is fused to the interior surface of the first component at the first section, and wherein another portion of an exterior surface of the braided sleeve is fused to the interior surface of the second component at the first section.

6. The composite structure of claim 4 , wherein the braided sleeve extends from the first portion of the interior volume to a second portion of the interior volume, and wherein, between the first and second portions, an entirety of the exterior surface of the braided sleeve is in contact with interior surfaces of the first or second components.

7. A method of forming the composite structure of claim 1 , comprising:

forming a first composite panel in three dimensions;

forming a second composite panel in three dimensions;

placing a first composite insert adjacent at least a portion of first interior surface of the first composite panel;

placing a second composite insert adjacent at least another portion of the first interior surface of the first composite panel; and

joining the first composite panel to the second composite panel, joining the first composite insert to the first and second composite panels, and joining the second composite insert to the first and second composite panels in a fusing step.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 6, 2024
From: REVVED INDUSTRIES, LLC
To: ASTRO TECH CO., LTD.
Reel/Frame 066391/0318 →
CHANGE OF NAME Recorded Jan 11, 2024
From: GUERRILLA INDUSTRIES LLC
To: REVVED INDUSTRIES, LLC
Reel/Frame 066275/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 24, 2023
From: BOSWORTH, BENJAMIN K.; GIARAFFA, MATTHEW T.; NICHOLS, SAMUEL D.; YUVANC, TOGAY
To: GUERRILLA INDUSTRIES LLC
Reel/Frame 063090/0187 →
Continuity (3)
Continuation 17690179 · Mar 9, 2022
Provisional Application 63158703 · Mar 9, 2021
Related Publication 20230139946A1 · May 4, 2023
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