Recursively Mapped Infill Geometry for Additive Manufacturing

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Solution Overview

Problem

Existing additive manufacturing techniques struggle to efficiently produce complex geometries for sandwich panels, limiting their ability to achieve optimal strength-to-weight ratios.

Innovation Solution

A method is developed to generate a recursively mapped infill geometry for additively manufacturable parts, involving the use of base and target unit cell meshes, extrusion of quadrilateral elements to hexahedral elements, and recursive supercell mesh generation to produce a final recursively mapped unit cell mesh.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If traditional manufacturing techniques are used, then manufacturing process is simple, but geometry complexity is limited

Engineering Contradiction:
Improvegeometry complexityVSAvoidmanufacturing process complexity
Core Design Contradiction:
ShapeVSDevice complexity

Solution Approach 1:

The manufacturing process is divided into discrete iterative steps: generating unit cell meshes, creating supercell structures, and mapping geometries. Each iteration builds upon the previous one, allowing complex geometries to be constructed from simpler components through systematic segmentation of the design space.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements nested unit cell structures where smaller unit cells are embedded within larger supercell geometries. This nesting approach allows multiple scales of complexity to be integrated, with base unit cells forming the foundation and recursively mapped supercells adding progressively complex features, enabling highly complex final geometries while maintaining manufacturability.

Inventive Principle:
Principle #7Nested doll (Nesting)

2Strength

If complex geometries are produced, then strength-to-weight ratio is improved, but manufacturing efficiency decreases

Engineering Contradiction:
Improvestrength-to-weight ratioVSAvoidmanufacturing efficiency
Core Design Contradiction:
StrengthVSProductivity

Solution Approach 1:

The patent systematically varies key parameters including unit cell size, supercell iteration depth, material distribution patterns, and geometric scaling factors. By optimizing these parameters, the design achieves high strength-to-weight ratios through controlled material placement while managing manufacturing complexity. The iterative mapping process allows parameter refinement at multiple scales to balance performance and efficiency.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach allows for the creation of additively manufactured sandwich panels with improved strength-to-weight ratios and complex geometries that would be difficult to achieve with traditional manufacturing methods.

Implementation Method 1

generating a target hexahedral unit cell mesh including a plurality of target hexahedral elements at least in part by extruding the plurality of target quadrilateral elements

Methodology Applied
Scientific EffectExtrusion: Extrusion

Data Source

PatentUS20250139322A1Recursively mapped geometry of additively manufactured part
Publication Date: 2025.05.01 THE BOEING CO
  • US20250139322A1 patent drawing
  • US20250139322A1 patent drawing
  • US20250139322A1 patent drawing

AI summary

A method of generating a recursively mapped infill geometry for an additively manufacturable part. The method includes receiving a base unit cell mesh including a plurality of base quadrilateral elements. In each of a plurality of iterations, the method further includes receiving a target unit cell mesh including target quadrilateral elements. In each iteration, the method further includes generating a target hexahedral unit cell mesh including target hexahedral elements by extruding the target quadrilateral elements. In each of the iterations, the method further includes generating a recursive supercell mesh by mapping each of the base quadrilateral elements onto a target hexahedral element. If the current iteration is not a final iteration, the method further includes setting the recursive supercell mesh as the base unit cell mesh used in a subsequent iteration. The method further includes outputting a recursively mapped unit cell mesh including a final recursive supercell mesh.