Additively Manufactured Metallic Coupling for Torque and Flexibility
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Solution Overview
Problem
Current drive shaft couplings for aircraft face a dilemma in needing to be both stiff and strong under torque while also being flexible under axial and bending deformations, with existing high-precision and expensive solutions sought to be replaced by more cost-effective alternatives.
Innovation Solution
A metallic coupling design featuring two cylindrical flanges with spirally arranged connectors in opposing directions, forming an annular gap, which provides stiffness under torque and flexibility through additive manufacturing, allowing for axial and bending flexibility.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If traditional diaphragm couplings with high-precision fabrication and welding are used, then torque stiffness and strength are improved, but manufacturing cost and complexity increase
Solution Approach 1:
The patent changes the manufacturing parameters from traditional high-precision fabrication and welding to additive manufacturing processes. This allows the coupling to achieve the required torque stiffness and strength while significantly reducing manufacturing cost and complexity. The additive manufacturing process enables direct fabrication of complex geometries without expensive tooling or assembly operations.
Solution Approach 2:
The patent employs additive manufacturing to create couplings that are more cost-effective than traditional precision-fabricated couplings. The process eliminates expensive welding operations and high-precision machining, replacing them with a more economical direct fabrication approach that maintains structural integrity while reducing overall manufacturing cost.
2Force
If traditional rigid couplings are used, then torque transmission is improved, but axial and bending flexibility deteriorates
Solution Approach 1:
The coupling is segmented into multiple struts arranged in a polyhedral geometry, creating discrete load paths that can independently deform. This segmentation allows the coupling to transmit torque through the structured arrangement of struts while accommodating axial and bending deformations through the relative movement and elastic deformation of individual strut elements.
Solution Approach 2:
The coupling transitions from a rigid static structure to a dynamic structure that can adapt its stiffness characteristics. The polyhedral geometry with multiple struts allows the coupling to maintain torque transmission capability while dynamically adjusting to axial and bending loads, providing the required flexibility without sacrificing torque transmission performance.
3Manufacturing precision
If high-precision fabrication methods are used, then coupling performance is improved, but manufacturing time and complexity increase
Solution Approach 1:
The patent replaces traditional mechanical fabrication processes (machining, welding, assembly) with additive manufacturing technology. This substitution eliminates multiple sequential operations including precision machining, welding procedures, and quality inspection steps, dramatically reducing manufacturing time while maintaining or improving coupling performance through the ability to directly fabricate complex geometries with high precision.
Solution Approach 2:
The additive manufacturing process merges multiple manufacturing operations into a single fabrication step. The coupling geometry, including all structural details and features, is created in one continuous process without the need for separate machining, welding, or assembly operations, thereby reducing both manufacturing time and process complexity while maintaining high precision.
Data Source
Figure 1A~1B
Figure 2A~2B
Figure 3
AI summary
A metallic coupling for a drive shaft includes a first cylindrical flange (14) extending axially along a center axis and a second cylindrical flange (16) extending axially along the center axis and spaced axially from the first cylindrical flange. The metallic coupling also includes a first plurality and a second plurality of connectors (18, 20). Each connector of the first plurality of connectors extends from the first cylindrical flange to the second cylindrical flange and are spaced circumferentially apart from each other about the center axis. Each connector of the second plurality of connectors also extends from the first cylindrical flange to the second cylindrical flange and are spaced circumferentially apart from each other about the center axis. The second plurality of connectors are radially inward from the first plurality of connectors relative to the center axis. An annular gap (22) is radially between the first plurality of connectors and the second plurality of connectors.