IP Library Patent Application 14665594
Patent Application
App. No. 14/665,594

METHOD OF MANUFACTURING LIGHTWEIGHT COMPOSITE LATTICE STRUCTURES

Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US None
App. No.
14/665,594
Abstract

Embodiments herein described relate to a method of making composite lattice structures by threading one or more fiber tows through a removable pattern in a lattice configuration, covering the pattern and lattice members in one or more face sheets, and interfusing the assembly of pattern, lattice members and face sheets with a matrix.

Claims (47)

1 . A method of manufacturing a composite lattice, the method comprising:

providing a pattern in a removable material, the pattern having an exterior surface and one or more through-holes passing through the pattern;

threading a fiber tow through at least one of the one or more through-holes;

applying a face sheet to a portion of the exterior surface of the pattern;

interfusing the face sheet and the fiber tow with a matrix material;

curing the matrix material; and

removing the pattern from the cured matrix material, so as to form a lattice formed by the resin-impregnated fiber tows and the face sheet.

2 . The method of claim 1 wherein providing a pattern further comprises:

shaping the pattern to approximate the shape of an internal cavity of a substantially hollow structure.

3 . The method of claim 1 wherein providing a pattern further comprises:

boring a plurality of through-holes in the removable material, the through-holes being arranged in a lattice configuration.

4 . The method of claim 3 wherein boring a plurality of through-holes comprises a boring process performed by a computer-numerically-controlled machine.

5 . The method of claim 3 wherein at least a subset of the plurality of through-holes have openings that are adjacent to each other at the exterior of the pattern; and further comprising:

where first and second through-holes of the subset have adjacent openings, threading a fiber tow out from the first through-hole and into the second through-hole by way of the adjacent openings.

6 . The method of claim 1 wherein interfusing the face sheet and the fiber tow with a matrix comprises a single resin-transfer process.

7 . The method of claim 6 wherein the resin-transfer process further comprises:

sealing the pattern, the fiber tow, and the face sheet within a vacuum bag having one or more inlets and one or more outlets;

generating a vacuum within the vacuum bag; and

placing the one or more inlets into fluid contact with a reservoir containing the matrix material.

8 . The method of claim 1 further comprising:

prior to the permeating act, mixing the resin with a hardening agent.

9 . The method of claim 1 wherein threading a fiber tows further comprises:

threading the fiber tow through the face sheet from an interior surface of the face sheet to an exterior surface of the face sheet, passing the fiber tow over a section of the exterior surface of the face sheet, and passing the fiber tow back through the face sheet.

10 . The method of claim 1 wherein the face sheet comprises carbon fiber fabric.

11 . The method of claim 1 wherein applying a face sheet further comprises:

applying a plurality of unidirectional fiber sheets in two or more ply orientations.

12 . The method of claim 1 wherein the fiber tow comprises a plurality of parallel carbon fiber filaments.

13 . The method of claim 1 wherein removing the pattern comprises at least one of the following: melting, dissolving, or mechanical extraction.

14 . A composite lattice formed by the method of claim 1 .

15 . A method of manufacturing a composite lattice, the method comprising:

preparing a removable pattern, the pattern having an exterior surface that approximates an internal cavity of a structure, the removable pattern having a plurality of through-holes therethrough, the through-holes being arranged in the shape of a lattice;

threading a first length of fiber tow through a first subset of the plurality of through-holes; such that the first length passes along and abuts at least one section of the exterior surface of the pattern;

applying a fiber face sheet to the exterior surface of the pattern;

threading a second length of fiber tow through a second subset of the plurality of through-holes and also through the face sheet, such that the second length passes over and abuts at least one section of an exterior surface of the face sheet;

interfusing a resin throughout the first and second lengths of fiber tow and the face sheet;

curing the resin; and

removing the pattern.

16 . The method of claim 15 wherein the first length of fiber tow and second length of fiber tow are sections of a contiguous carbon fiber filament tow.

17 . The method of claim 15 wherein the first and second subsets of through holes comprise the same through-holes.

18 . The method of claim 15 wherein each through-hole is adjacent to one or more additional through-holes; and wherein each of the threading acts further comprises:

passing the first and second lengths of fiber tow out of the pattern by way of a first through hole and back into the pattern by way of an adjacent second through-hole.

19 . The method of claim 15 wherein interfusing a resin comprises a vacuum-assisted resin transfer molding process.

20 . The method of claim 15 wherein curing the resin further comprises:

prior to the interfusing act, mixing the resin with a hardening agent;

allowing the resin to gel at a room temperature for a first curing time; and

curing the resin at an elevated temperature for a second curing time.

21 . A composite lattice formed by the method of claim 14 .

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 4, 2017
From: KHALIFA UNIVERSITY OF SCIENCE, TECHNOLOGY & RESEARCH (KUSTAR)
To: KHALIFA UNIVERSITY OF SCIENCE AND TECHNOLOGY
Reel/Frame 044110/0891 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 21, 2016
From: CANTWELL, WESLEY JAMES; UMER, REHAN
To: KHALIFA UNIVERSITY OF SCIENCE, TECHNOLOGY & RESEARCH (50%); AEROSPACE HOLDING COMPANY LLC (50%)
Reel/Frame 038055/0679 →