Clevis Assembly With Frangible Shear for Tail Rotor Torque Fail-Safe
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Solution Overview
Problem
In rotary wing aircraft, component failures in the tail rotor system can introduce additional torque, leading to unpredictable damage to mechanical system components due to the lack of effective fail-safe mechanisms.
Innovation Solution
A clevis assembly with a shearing device featuring a frangible point is integrated into the tail rotor system, which shears under high torque conditions, allowing the piston to spin with the tail rotor and preventing damage to input/feedback linkages, thereby maintaining control for a limited time and ensuring safe operation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a fail-safe mechanism is added to the tail rotor system, then reliability is improved, but device complexity increases
Solution Approach 1:
The frangible point is pre-positioned at a specific location on the shearing device with predetermined structural characteristics (reduced cross-section, material properties) that ensure it will fail first under excessive torque conditions. This preliminary design ensures that when torque exceeds safe levels, the failure occurs predictably at the frangible point rather than unpredictably elsewhere in the system.
Solution Approach 2:
The shearing device with its frangible point acts as a sacrificial component designed to fail deliberately. This disposable element protects more expensive and critical components (input linkages, feedback linkages, main rotor system) by absorbing the failure event. After the frangible point shears, the shearing device can be replaced while preserving the rest of the tail rotor system.
2Object-affected harmful factors
If the shearing device is designed to shear under high torque, then harmful factors are localized, but strength of the mechanical system is reduced
Solution Approach 1:
The shearing device with its frangible point serves as an intermediary element positioned between the torque source (tail rotor) and the vulnerable components (input linkages, feedback linkages). Under normal operating conditions, it transmits torque normally. Under excessive torque conditions, it mediates the failure by shearing at the frangible point, preventing the harmful torque from propagating to other components.
Solution Approach 2:
The design converts the potentially harmful effect of excessive torque into a beneficial protective mechanism. By deliberately creating a weak point (frangible point) that fails under excessive torque, the system transforms what would be a catastrophic unpredictable failure into a controlled, localized failure that protects the overall system. The harm of component failure is converted into the benefit of system protection.
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
The shearing device effectively localizes torque-induced failures to a predetermined area, reducing unpredictability and allowing continued operation, ensuring structural integrity and enabling safe landing procedures.
Implementation Method 1
a shearing device that includes a frangible point and is in operable communication with the bearing... the shearing device is operable to shear under a pressure greater than a threshold amount
Data Source
AI summary
According to an aspect, a clevis assembly includes a shackle having two ends, each end respectively including an aperture, a structure connecting the apertures and housing a bearing, and a shearing device that includes a frangible point and is in operable communication with the bearing, where the shearing device is housed in a hollow portion of the structure.


