Multidirectional Core Member for Aircraft Rotor Blade Stiffness
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Solution Overview
Problem
Conventional core members in composite sandwich structures lack directional strength and stiffness, limiting their effectiveness in certain loading configurations, particularly in aircraft applications where improved mechanical properties are needed.
Innovation Solution
A core member with cell members oriented at specific angles to optimize strength and stiffness in specific loading directions, utilizing a multidirectional woven fiber configuration that can be tailored for torsional strength and stiffness along the spanwise and chordwise directions, and incorporating planar members for enhanced stability and bonding.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If conventional core members with cell members normal to skin members are used, then the structure is simple to manufacture, but the directional strength and stiffness are insufficient
Solution Approach 1:
The patent applies dimensionality change by transitioning from a unidirectional core configuration (cell members normal to skins) to a multidirectional configuration with cell members oriented at various angles (e.g., 0°, 45°, 90°). This angular dimensionality provides strength and stiffness in multiple loading directions simultaneously, resolving the contradiction between directional performance and structural complexity.
Solution Approach 2:
The patent employs composite material principles by creating a core structure that combines cell members of different orientations and potentially different materials properties. This composite core configuration integrates the strengths of individual cell orientations to achieve superior overall directional strength and stiffness while managing structural complexity through systematic design.
2Reliability
If core members are optimized for directional strength and stiffness, then the mechanical strength is improved, but the manufacturing complexity increases
Solution Approach 1:
The patent applies segmentation by dividing the core into distinct regions or layers with different cell member orientations. Each segment is optimized for specific loading conditions, allowing the core to achieve high reliability in multiple directions. This segmented approach enables modular manufacturing processes, where each segment can be fabricated and then assembled, thereby managing manufacturing complexity.
Solution Approach 2:
The patent utilizes parameter changes by varying the orientation angles, material properties, and geometric parameters of cell members to optimize directional strength and stiffness. These parameter variations are systematically controlled during manufacturing, allowing for tailored mechanical performance while using standardized manufacturing techniques to maintain ease of production.
3Force
If conventional core configurations are used, then the manufacturing process is straightforward, but the load-bearing capacity in specific directions is limited
Solution Approach 1:
The patent resolves this contradiction by introducing angular dimensionality to the core structure. Cell members are oriented at multiple angles (e.g., 0°, 45°, 90°) rather than uniformly normal to the skins, enabling the core to bear loads in multiple directions. This multidirectional configuration increases load-bearing capacity while maintaining manageable structural complexity through systematic angular distribution.
Solution Approach 2:
The patent applies local quality by tailoring the cell member orientation and properties in specific regions of the core to match the local loading conditions. Areas experiencing different stress patterns have differently oriented cell members, optimizing load-bearing capacity locally. This localized optimization increases overall force capacity without requiring complex global restructuring of the entire core.
Data Source
AI summary
The present application relates a core member for a core-stiffened structural assembly. The core member includes a plurality of cell members oriented a direction to provide a tailored stiffness in a certain direction. The core member can further include one or more planar members that can aid in shear transfer between cell members. The cell members can be made from bonding a plurality of corrugated layers together. The core-stiffened structure can be a rotor blade for an aircraft. In such an embodiment, the torsional stiffness of the rotor blade can be tailored in at least one of the chordwise and spanwise directions to provide tailor a torsional stiffness at any give location in the rotor blade.


