Composite Grid Structures Using Staggered Finite-Length Tapes

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Solution Overview

Problem

Conventional composite laminate structures face inefficiencies due to their discrete nature, requiring thick sub-laminates for symmetry and balance, leading to excessive thickness, manufacturing complexities, and limitations in achieving optimal material characteristics, especially in applications like fuselage or wing skins where thinner laminates are needed.

Innovation Solution

A composite grid structure with staggered joint configurations using elongate tapes oriented at specific angles, allowing for efficient manufacturing and improved flexural stiffness, while reducing weight and simplifying fabrication by eliminating the need for continuous tapes and discontinuous inserts.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If conventional composite laminate structures use symmetric and balanced ply layers to emulate metal characteristics, then strength characteristics are improved, but laminate thickness becomes excessive

Engineering Contradiction:
Improvestrength characteristicsVSAvoidlaminate thickness
Core Design Contradiction:
StrengthVSLength of stationary object

Solution Approach 1:

The patent divides the laminate structure into discrete tape segments with finite lengths arranged in staggered patterns. Instead of continuous symmetric plies, the structure uses segmented tapes oriented at various angles (0°, ±45°, 90°) that are discontinuous and staggered, eliminating the need for thick symmetric sub-laminates while maintaining structural integrity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs asymmetric tape arrangements where tapes are oriented at specific angles (0°, ±45°, 90°) in a non-symmetric staggered pattern. This asymmetric configuration achieves the desired strength characteristics without requiring the symmetric ply stacking that leads to excessive thickness in conventional laminates

Inventive Principle:
Principle #4Asymmetry

2Strength

If legacy quad laminates use multiple plies to achieve desired directional properties, then directional strength is improved, but manufacturing complexity increases

Engineering Contradiction:
Improvedirectional propertiesVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent segments the laminate into discrete tape portions with finite lengths arranged in staggered patterns. This segmentation allows for simplified manufacturing where pre-cut tapes can be directly placed in their final positions without complex layer-by-layer stacking and alignment procedures required by traditional multi-ply laminates

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The tapes are pre-cut to specific finite lengths and pre-oriented at the required angles (0°, ±45°, 90°) before placement. This preliminary preparation of tape segments eliminates the need for complex in-situ cutting and alignment during manufacturing, reducing overall manufacturing complexity

Inventive Principle:
Principle #10Preliminary action

3Stability of the object's composition

If conventional laminates require mid-plane symmetry, then structural stability is improved, but weight increases

Engineering Contradiction:
Improvestructural stabilityVSAvoidstructure weight
Core Design Contradiction:
Stability of the object's compositionVSWeight of moving object

Solution Approach 1:

The patent uses asymmetric staggered tape arrangements that achieve structural stability without requiring mid-plane symmetry. The staggered discontinuous tapes oriented at 0°, ±45°, and 90° create a balanced structure through their spatial distribution rather than through symmetric stacking, thereby reducing weight

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The patent transitions from the conventional two-dimensional symmetric stacking approach to a three-dimensional staggered arrangement where tapes are positioned at different depths and orientations. This dimensional change allows structural stability to be achieved through spatial distribution rather than symmetric repetition, reducing the total material required

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

4Strength

If thick sub-laminates are used to achieve minimum gauge requirements, then structural integrity is improved, but adaptability to thin-section applications decreases

Engineering Contradiction:
Improvestructural integrityVSAvoidadaptability to thin-section applications
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The patent applies local quality by using discontinuous tapes of finite lengths that can be selectively placed only where structural support is needed. This allows the structure to achieve necessary integrity in specific regions while maintaining thin overall thickness in other areas, providing adaptability to various gauge requirements

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

By segmenting the laminate into discrete tape portions rather than using continuous thick sub-laminates, the structure can be locally optimized. Tapes can be placed strategically to provide strength where needed while leaving other areas thin, enabling adaptation to both thick and thin section applications

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS11999151B2Composite structures containing finite length tapes and methods for manufacturing and using the same
Publication Date: 2024.06.04 THE BOARD OF TRUSTEES OF THE LELAND STANFORD JUNIOR UNIV
  • US11999151B2 patent drawing
  • US11999151B2 patent drawing
  • US11999151B2 patent drawing

AI summary

Described are composite grid structures that have a plurality of ply layers, each one of the plurality of ply layers comprising a plurality of first elongate tapes oriented in a first direction and a plurality of second elongate tapes oriented in a second direction, the second direction being offset from the first direction by an angle of at least 25 degrees. In the grid structures: each of the first elongate tapes has a first length extending between opposing ends of each of the plurality of first elongate tapes and a first midpoint intermediate the opposing ends, and each of the second elongate tapes has a second length extending between opposing ends of each of the plurality of second elongate tapes and a second midpoint intermediate the opposing ends. Associated composite laminate structures, grid structures, and methods of manufacturing and/or using the same are also disclosed.