Resin Infusion Sensor for Aircraft Composite Parts
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Current methods for fabricating aircraft parts using composite materials face challenges in accurately detecting when a preform is fully infused with resin, leading to potential dry zones and inconsistencies in part thickness and mechanical properties due to uncertainties in resin quantity and flow control.
Innovation Solution
Incorporating a permeable layer with lower resin permeability than the preform, positioned remotely from the preform, and using a resin presence sensor to ensure complete impregnation before resin reaches additional layers, along with a sensor capable of detecting resin presence and curing status, to control the resin injection process.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If resin is injected into the preform using conventional methods, then the preform is filled with resin, but it is difficult to detect when the preform has finished being filled, leading to uncertainties in resin quantity and potential dry zones
Solution Approach 1:
A sensor is introduced as an intermediary element between the resin and the detection system. The sensor detects the presence of resin through its permeable layer, providing accurate real-time information about resin filling status without directly contacting the resin or requiring complex measurement systems.
Solution Approach 2:
The system implements feedback control by continuously monitoring resin presence through the sensor and adjusting the injection process accordingly. When the sensor detects resin presence, the system can determine when the preform is fully filled and stop injection, ensuring accurate resin quantity control.
2Reliability
If the quantity of resin injected is increased to ensure complete filling, then dry zones are prevented, but the thickness of the part increases due to resin remaining in the mold
Solution Approach 1:
The sensor provides real-time feedback on resin presence, allowing the injection system to stop precisely when the preform is fully filled. This prevents both under-filling (dry zones) and over-filling (excessive thickness) by basing the decision on actual resin presence detection rather than theoretical calculations.
Solution Approach 2:
The patent replaces mechanical measurement methods (weighing injection vessels, measuring flow rates) with a sensor-based detection system that directly senses resin presence. This substitution provides more accurate and reliable control over resin quantity, eliminating the need to rely on indirect mechanical measurements that are prone to error.
3Reliability
If a semi-permeable membrane is used to confine resin, then resin remains in the mold, but it is difficult to detect when resin flow has stopped due to measurement inaccuracies and potential leaks
Solution Approach 1:
The sensor acts as an intermediary that directly senses resin presence through the permeable layer, providing a reliable detection method that is not affected by the semi-permeable membrane or potential leaks in the resin circuit. The sensor detects resin presence directly, eliminating the need to rely on indirect flow rate measurements.
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 method ensures precise control over resin quantity and distribution, preventing dry zones and improving the reliability of composite part fabrication by ensuring complete impregnation before resin reaches additional layers, thus enhancing the mechanical properties and consistency of the final product.
Implementation Method 1
placing in a stack comprising a preform at least one layer of a material that presents permeability to a predetermined resin that is less than the permeability of a portion of the preform that is the closest to the layer
Implementation Method 2
placing a resin presence sensor on a side of the layer that is remote from the preform
Data Source
AI summary
The method of fabricating an aircraft part comprises the steps of placing in a stack comprising a preform at least one layer of a material that presents permeability to a predetermined resin that is less than the permeability of a portion of the preform that is the closest to the layer; and placing a resin presence sensor on a side of the layer that is remote from the preform.


