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

VSEngineering Contradiction Analysis

1Reliability

If a fail-safe mechanism is added to the tail rotor system, then reliability is improved, but device complexity increases

Engineering Contradiction:
Improvetail rotor system reliabilityVSAvoidmechanical system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

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.

Inventive Principle:
Principle #10Preliminary action

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.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

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

Engineering Contradiction:
Improvetorque-induced damageVSAvoidmechanical system strength
Core Design Contradiction:
Object-affected harmful factorsVSStrength

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.

Inventive Principle:
Principle #24Intermediary (Mediator)

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.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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

Methodology Applied
Scientific EffectShear stress: Shear Stress

Data Source

PatentUS11345468B2Clevis assembly with bearing device in operable communication with a translating element, and fail-safe tail rotor system including the same
Publication Date: 2022.05.31 LOCKHEED MARTIN CORP
  • US11345468B2 patent drawing
  • US11345468B2 patent drawing
  • US11345468B2 patent drawing

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.