3D-Printed Graphene Drilling Template for Heat-Stable Hole Accuracy

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Solution Overview

Problem

Drilling templates for aircraft and spacecraft manufacturing are cumbersome and difficult to reuse across different aircraft families, leading to high ecological impact and costs due to the need for multiple templates and potential inaccuracies from template deformation during high-temperature drilling.

Innovation Solution

A smart drilling template with embedded sensors, digital components, and a human-machine interface (IHM) made from graphene-enhanced polymer materials, allowing for real-time temperature and position monitoring, and enabling rapid ad-hoc design changes via Additive Laser Manufacturing (ALM).

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If traditional drilling templates are used for aircraft manufacturing, then multiple templates are needed for different aircraft families, but this increases ecological impact and costs

Engineering Contradiction:
Improvetemplate reusabilityVSAvoidecological footprint
Core Design Contradiction:
Adaptability or versatilityVSLoss of substance

Solution Approach 1:

The drilling template is designed with a modular framework and adjustable positioning mechanisms that allow it to accommodate multiple aircraft families and configurations. The template can be repositioned and reconfigured for different drilling patterns, eliminating the need for separate dedicated templates for each aircraft type, thereby reducing waste and ecological impact.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The template incorporates adjustable and reconfigurable elements that allow it to adapt dynamically to different drilling requirements. The positioning system can be modified in real-time to accommodate various hole patterns and locations across different aircraft models, transforming a static tool into a dynamic, multi-purpose device.

Inventive Principle:
Principle #15Dynamics

2Temperature

If traditional drilling templates are used, then template deformation occurs during high-temperature drilling, but this reduces manufacturing precision

Engineering Contradiction:
Improvedrilling temperature resistanceVSAvoidhole position accuracy
Core Design Contradiction:
TemperatureVSManufacturing precision

Solution Approach 1:

The template is constructed from composite materials that combine high thermal resistance with dimensional stability. These materials maintain their structural integrity and precise geometry even under high drilling temperatures, preventing deformation and ensuring consistent manufacturing accuracy across multiple uses.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The template design incorporates thermal compensation mechanisms that adjust for temperature-induced dimensional changes. By monitoring temperature parameters and making real-time adjustments to positioning, the system maintains manufacturing precision despite the high temperatures generated during drilling operations.

Inventive Principle:
Principle #35Parameter changes

3Adaptability or versatility

If multiple drilling templates are manufactured for different aircraft families, then template availability improves, but device complexity and costs increase

Engineering Contradiction:
Improveaircraft family coverageVSAvoidtemplate system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The template system is divided into modular, interchangeable components that can be configured for different aircraft families. Rather than manufacturing entirely separate templates, the system uses standardized modules that can be assembled and reconfigured, reducing overall system complexity while maintaining versatility across multiple aircraft types.

Inventive Principle:
Principle #1Segmentation

4Duration of action of stationary object

If drilling templates are reused extensively, then costs are reduced, but template life expectancy decreases due to wear and deformation

Engineering Contradiction:
Improvetemplate service lifeVSAvoidtemplate integrity
Core Design Contradiction:
Duration of action of stationary objectVSReliability

Solution Approach 1:

The use of high-performance composite materials with superior thermal and mechanical properties enables the template to withstand repeated use without degradation. These materials resist wear, maintain dimensional stability, and preserve structural integrity even after extensive use, significantly extending the template's service life while ensuring consistent reliability.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The template design incorporates protective features and stress-distribution mechanisms that prevent wear and deformation before they occur. By designing in advance to accommodate thermal and mechanical stresses, the template maintains its integrity and precision throughout its extended service life, reducing the need for replacement and maintaining reliability.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

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

Enhances mechanical resistance, reduces ecological footprint, and extends template life expectancy by preventing deformation, while facilitating efficient reuse and reducing assembly time through smart interaction and real-time feedback.

Implementation Method 1

high temperatures are reached due to the friction between the drilling tool and the drilling template

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 2

improve its mechanical resistance via the graphene properties, in order to resist and conserve its integrity when high temperatures are reached

Methodology Applied
Scientific EffectThermal resistance: Thermal Insulation

Implementation Method 3

a set of sensors able to measure values respectively from the rigid framework and/or from or with respect to the structure to drill

Methodology Applied
Scientific EffectTemperature sensing:

Implementation Method 4

the possibility to use the ALM (Additive Laser Manufacturing) in order to manufacture quickly any simple or complex patterns of the drilling template

Methodology Applied
Scientific EffectAdditive manufacturing: 3D Printing

Data Source

PatentEP3486010B1Driling template
Publication Date: 2025.08.13 AIRBUS OPERATIONS SL
  • EP3486010B1 patent drawingFigure 1~2
  • EP3486010B1 patent drawingFigure 3a~3b
  • EP3486010B1 patent drawingFigure 3c

AI summary

This invention is based on a drilling template (20, 30a, 30b, 30c) comprising : - a rigid framework able to be manipulated by an operator or an automaton, and - a set of traversing (22, 32a, 32b, 32c, 33c) orifices designed according to the requested holes to drill, characterized in that, - the drilling template (20, 30a, 30b, 30c) is designed or restyled on an ad-hoc basis and manufactured via a 3D printing technology based on a polymer material mixed with powdered graphene.