Torque Link Quick-Release Locking for Single-Person Towing

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Solution Overview

Problem

Current aircraft landing gear torque link assemblies require at least two persons to disconnect and reconnect, making it cumbersome and inefficient for single-person operation, especially during towing operations.

Innovation Solution

A torque link assembly with a quick release locking mechanism using locking pin assemblies with a biasing element and a guide pin system that allows a single individual to easily engage and disengage the upper and lower torque links, utilizing a handle and channel mechanism for single-handed operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If conventional apex pin connections are used to connect upper and lower torque links, then the torque links can be securely connected, but at least two persons are required to disconnect and reconnect them

Engineering Contradiction:
ImproveEase of disconnection and reconnectionVSAvoidComplexity of locking mechanism
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The locking pin assembly incorporates a movable locking pin that can transition between engaged and disengaged states, allowing the connection to be dynamically adjusted. The pin is biased by a spring element and can be moved by a single operator using a handle, enabling easy disconnection and reconnection while maintaining secure engagement during operation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The locking pin assembly acts as an intermediary mechanism between the upper and lower torque links. It provides a simplified interface that allows a single operator to control the connection state through handle actuation, which moves the locking pin to engage or disengage the torque links, eliminating the need for multiple persons.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If apex pins are biased to engaged position with a spring, then secure connection is maintained, but two hands are required to separate the pins and a third hand to separate the torque links

Engineering Contradiction:
ImproveReliability of engaged positionVSAvoidNumber of hands required for operation
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The locking pin, handle, and spring element are merged into a single integrated locking pin assembly. The handle is connected to the locking pin, and the spring biases the pin toward engagement. This merging allows a single operator to control the entire locking mechanism with one hand by actuating the handle, which moves the pin to disengage the torque links.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The spring element automatically biases the locking pin toward the engaged position, maintaining reliable connection without requiring continuous manual intervention. The handle mechanism allows the operator to easily override this bias when disconnection is needed, and the system self-returns to the engaged state when the handle is released.

Inventive Principle:
Principle #25Self-service

3Strength

If conventional torque link assemblies are used, then the landing gear can support aircraft weight, but towing operations require multiple personnel and are cumbersome

Engineering Contradiction:
ImproveStrength to support aircraft weightVSAvoidSpeed of disconnection and reconnection
Core Design Contradiction:
StrengthVSProductivity

Solution Approach 1:

The locking pin assembly provides a dynamic connection system that can quickly transition between locked and unlocked states. The handle mechanism allows rapid actuation to disengage the torque links for towing operations, and the spring automatically re-engages them when the handle is released, enabling fast setup and teardown without compromising structural strength.

Inventive Principle:
Principle #15Dynamics

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

Enables a single person to efficiently disconnect and reconnect the torque links, simplifying towing operations and reducing the need for multiple personnel, while maintaining secure engagement and disengagement.

Implementation Method 1

A biasing element biases the locking pin member towards engagement with the second link portion

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

the other of the housing and the locking pin member further includes a guide pin that engages the channel such that the locking pin member is movable between the engaged position and the disengaged position when the guide pin is in the longitudinal portion of the channel

Methodology Applied
Scientific EffectMechanical constraint: Mechanical Force

Data Source

PatentUS11377206B2Torque link apex quick release locking mechanism
Publication Date: 2022.07.05 SAFRAN LANDING SYST CANADA INC
  • US11377206B2 patent drawing
  • US11377206B2 patent drawing
  • US11377206B2 patent drawing

AI summary

A torque link assembly for a landing gear includes a lower torque link and an upper torque link that releasably engage first and second quick release pin assemblies. The pin assemblies each include a housing attached to one of the torque links, and a locking pin member extending through the housing. The locking pin member includes a rod portion and a pin portion, and is slidable between an engaged position and a disengaged position for hingedly connecting/disconnecting the torque links. One of the housing and the locking pin member includes a channel having a longitudinal portion and a circumferential portion, and the other has a guide pin that engages the channel. The guide pin is in the longitudinal portion of the channel when moving between the engaged and disengaged positions, and is retained in the disengaged position when the guide pin is in the circumferential portion of the channel.