Flexible Core Layer for Sandwich Composite Tolerance Compensation
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
The manufacturing of sandwich composite components faces challenges in maintaining precise tolerance dimensions and ensuring a strong adhesive bond between the core and cover layers, particularly under extreme stress, which can lead to rigidity and strength loss and component failure.
Innovation Solution
A core layer composed of flexible core elements that can be variable in longitudinal extent, allowing for elastic deformation to compensate for length deviations and adapt to complex shapes, combined with resin channels for controlled resin flow, enabling flexible and rigid core elements to be joined without cavities and ensuring uniform properties.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Manufacturing precision
If core material with tight tolerance is used to maintain manufacturing precision, then manufacturing precision is improved, but device complexity and ease of manufacture deteriorate
Solution Approach 1:
The patent changes the physical state of the core material from rigid to flexible, allowing it to be deformable. This enables the core to adapt to tolerance variations through elastic deformation rather than requiring precise dimensional control during manufacturing, thereby improving manufacturing precision while simplifying the manufacturing process
Solution Approach 2:
The core material is designed with dynamic flexibility, allowing it to change shape and adapt during the bonding process. The flexible core can be deformed to match mold tolerances and then maintains the desired shape after bonding, resolving the contradiction between precision requirements and manufacturing ease
2Adaptability or versatility
If flexible core elements are used to compensate for length deviations, then adaptability is improved, but manufacturing precision deteriorates
Solution Approach 1:
The flexible core elements are pre-designed with specific flexibility characteristics and geometric configurations that enable them to compensate for anticipated length deviations. This preliminary design allows the core to automatically adapt to dimensional variations during assembly without compromising the final precision of the bonded component
3Strength
If resin infusion process is used to bond core and cover layers, then strength is improved, but manufacturing precision deteriorates
Solution Approach 1:
The patent changes the physical state of the core material from rigid to flexible, allowing it to be deformable. This enables the core to adapt to tolerance variations through elastic deformation rather than requiring precise dimensional control during manufacturing, thereby improving manufacturing precision while simplifying the manufacturing process
Solution Approach 2:
The core material is designed with dynamic flexibility, allowing it to change shape and adapt during the bonding process. The flexible core can be deformed to match mold tolerances and then maintains the desired shape after bonding, resolving the contradiction between precision requirements and manufacturing ease
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 solution allows for precise tolerance compensation and improved bonding within the core and cover layers, enhancing the structural integrity and adaptability of sandwich composite components, facilitating the production of complex shapes and maintaining mechanical properties.
Implementation Method 1
allowing for elastic deformation to compensate for length deviations and adapt to complex shapes
Implementation Method 2
combined with resin channels for controlled resin flow
Data Source
Figure 1~3
Figure 4~6
Figure 7
AI summary
Core element (1) for a core layer (3) of a sandwich composite component (10), is claimed, where the core element shaped surface is arranged with a first main surface (11), a second main surface (12) and side surfaces (13). At least one undercut recess open toward first and/or second major surfaces. Independent claims are also included for: (1) a core layer for a sandwich composite component, where several core elements are arranged in planar manner; and (2) a sandwich composite component comprising a core layer and a cover layer provided with at least one of the major surfaces.