Ratcheting Hold-Down Assembly for Vibration-Resistant Avionics Mounting

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Solution Overview

Problem

Conventional hold-down assemblies for portable electronic units in avionics equipment mounting trays fail to maintain a robust connection due to vibrations during aircraft operation, leading to disengagement from the mating wire harness and improper operation.

Innovation Solution

A hold-down assembly comprising a hinge block, shaft, locking collar, and actuator knob with a ratchet plate and spring-biased ball bearing, which applies a locking force to the portable electronic unit, resisting vibrations and ensuring secure engagement with the mating wire harness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional hold-down assembly is used to secure the portable electronic unit, then the unit can be initially engaged with the mating wire harness, but vibration during aircraft operation causes the hold-down assembly to loosen and the unit to become disengaged

Engineering Contradiction:
Improveconnection reliabilityVSAvoidengagement stability
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The hold-down assembly incorporates a dynamic locking mechanism where the actuator knob rotates to advance the locking collar along the shaft, creating a progressive locking action. The ball bearing and detent hole system provides dynamic vibration resistance by allowing the locking collar to self-adjust while maintaining secure engagement, preventing loosening during aircraft operation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The locking collar is designed to apply preliminary counteracting force against vibration-induced loosening. The ball bearing engages with detent holes in advance to prevent the locking collar from rotating backward, creating a preliminary anti-action that counteracts the harmful vibration forces before they can cause disengagement.

Inventive Principle:
Principle #9Preliminary anti-action

2Stability of the object's composition

If the locking collar applies sufficient force to prevent vibration-induced loosening, then engagement stability improves, but the complexity of the hold-down assembly increases

Engineering Contradiction:
Improveengagement stabilityVSAvoidassembly complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The hold-down assembly is segmented into distinct functional components: the shaft for pivoting motion, the locking collar for applying locking force, the actuator knob for operation, and the ball bearing-detent hole system for vibration resistance. This segmentation allows each component to perform its specific function efficiently while maintaining overall simplicity and reliability of the assembly.

Inventive Principle:
Principle #1Segmentation

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 assembly provides a reliable and secure connection by applying a significant locking force that resists vibrations, maintaining proper operation of the portable electronic unit despite aircraft vibrations, with minimal manual torque required for locking and high resistance to loosening.

Implementation Method 1

a compression spring within the knob body. The compression spring biases the ball bearing into engagement with the ratchet plate

Methodology Applied
Scientific EffectSpring bias: Spring

Implementation Method 2

the ball bearing is forced against the spring bias of the compression spring as the ball bearing travels between adjacent detent holes

Methodology Applied
Scientific EffectRatchet mechanism: Ratchet

Implementation Method 3

The actuator knob is threadably engaged with the shaft. As the actuator knob is rotated to move along the shaft

Methodology Applied
Scientific EffectThreaded engagement: Screw

Data Source

PatentUS8870149B2Hold-down assembly
Publication Date: 2014.10.28 AMPHENOL CABLE & INTERCONNECT TECHNOLOGIES INC
  • US8870149B2 patent drawing
  • US8870149B2 patent drawing
  • US8870149B2 patent drawing

AI summary

A hold-down assembly for retaining a portable electronic unit within an avionics equipment mounting tray includes a shaft, a locking collar, and an actuator knob. The shaft is coupled to pivot with the mounting tray. The locking collar slides along the shaft to engage the portable electronic unit. The actuator knob includes a knob body, a ratchet plate having detent holes within the knob body, a ball bearing, and a compression spring within the knob body. As the actuator knob is rotated to move along the shaft, the knob body and the ball bearing rotate with respect to the ratchet plate, and the ball bearing is forced against a spring bias of the compression spring as the ball bearing travels between adjacent detent holes.