Spline Torque Tube Coupling for Aircraft Wing Flex Alignment
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Solution Overview
Problem
Existing torque tube assemblies for aircraft high lift devices face issues with large rotational envelopes, bolt loosening, and structural integrity due to wing flexing, which affects torque transmission and alignment.
Innovation Solution
The use of spline couplings with integral yokes and retainer mechanisms that allow axial movement and angular adjustment, eliminating the need for bolted flanges, thereby reducing the rotational envelope and enhancing structural integrity.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Strength
If bolted flanges are used to couple torque tube to pinion gear, then structural integrity is improved, but rotational envelope becomes large requiring more space
Solution Approach 1:
The patent removes the flange component entirely from the torque tube assembly, replacing it with a spline coupling that integrates the coupling function directly into the torque tube structure. This extraction of the flange eliminates the large rotational envelope while maintaining structural integrity through the spline engagement mechanism.
Solution Approach 2:
The patent merges the flange and coupling functions into a single integrated spline coupling structure. The spline coupling combines torque transmission, alignment, and retention functions that were previously separated across multiple components (flange, bolts, coupling), thereby reducing the rotational envelope while preserving structural integrity.
2Power
If bolted flanges are used to couple torque tube to pinion gear, then torque transmission is achieved, but bolts can loosen reducing structural integrity
Solution Approach 1:
The patent replaces the bolted mechanical connection system with a spline engagement system. The spline coupling uses precise geometric interlocking between splines on the torque tube and corresponding splines in the pinion gear, eliminating bolts entirely. This substitution provides positive mechanical engagement that transmits torque reliably without the risk of loosening.
Solution Approach 2:
Instead of using bolts to pull components together (tensile force), the spline coupling uses compressive and shear forces through direct geometric interlocking. The splines engage in a way that creates mechanical interference, preventing relative motion and torque loss without relying on friction or bolt preload.
3Power
If rigid coupling is used between torque tube and drive shaft, then torque transmission is efficient, but wing flexing causes additional forces and strain
Solution Approach 1:
The patent introduces dynamic flexibility through the spline coupling mechanism, which allows for minor angular and axial movements while maintaining torque transmission. The spline engagement can accommodate small misalignments and flexing motions that occur during wing deformation, absorbing these dynamic loads without creating excessive forces on the torque tube.
Solution Approach 2:
The spline coupling changes the mechanical parameters of the connection by allowing controlled play and movement ranges. The engagement geometry permits small variations in position and orientation, transforming the rigid connection into a semi-flexible one that adapts to wing flexing while maintaining efficient torque transmission through the spline teeth.
4Adaptability or versatility
If spline coupling allows axial movement and angular adjustment, then adaptability to wing flexing is improved, but device complexity increases
Solution Approach 1:
The spline coupling performs multiple functions simultaneously: torque transmission, axial movement accommodation, angular adjustment, and retention. By integrating these functions into a single coupling mechanism rather than using separate components for each function, the patent achieves high adaptability while actually reducing overall system complexity compared to multi-component solutions.
Data Source
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AI summary
Example apparatus and methods for rigging a torque tube assembly (200) for actuating high-lift devices in an aircraft are described herein. An example torque tube assembly (200) includes a torque tube (304) and a spline coupling (404) coupled to an end (302) of the torque tube (304). The spline coupling (404) has an opening (410) to receive a spline gear (1400) on a drive shaft (228) of an aircraft high lift device actuator. The torque tube assembly also includes a retainer (1302) coupled to the spline coupling (404). The retainer (1302) blocks at least a portion of the opening (410) in the spline coupling (404) to prevent the spline coupling from being moved off of the spline gear (1400) on the drive shaft (228).