Wireless Telemeter Tool for Landing Gear Maneuvering Adjustment

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Solution Overview

Problem

Adjusting the maneuvering mechanism of a retractable main landing gear of an aircraft to ensure sufficient space between the doors and the gear for safe closure is challenging, requiring manual measurement and adjustment within the landing gear bay, which is unsafe and inefficient.

Innovation Solution

A tool with a telemeter and wireless communication unit allows remote adjustment of the maneuvering mechanism by locking onto a wheel, enabling measurement and display of the distance without an operator needing to be inside the bay, using a telemeter connected to a control device for precise adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If an operator positions themselves in the landing gear bay to manually measure the distance, then measurement can be performed, but operator safety is compromised and the process is inefficient

Engineering Contradiction:
Improvedistance measurementVSAvoidoperator safety
Core Design Contradiction:
Measurement precisionVSObject-affected harmful factors

Solution Approach 1:

The patent introduces a telemeter as an intermediary device to perform distance measurements between the landing gear and the bay door without requiring an operator to physically position themselves in the landing gear bay. The telemeter is mounted on the landing gear and measures the distance to the bay door, transmitting the data wirelessly to eliminate safety risks while maintaining measurement precision

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces the manual mechanical measurement process with an optical/electronic telemeter system. Instead of an operator using physical tools to measure distance, the telemeter uses light or electromagnetic waves to measure and transmit distance data wirelessly, eliminating the need for manual intervention in the landing gear bay

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Manufacturing precision

If manual measurement and adjustment is performed within the landing gear bay, then adjustment can be made, but the process is time-consuming and inefficient

Engineering Contradiction:
Improveadjustment precisionVSAvoidadjustment efficiency
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The patent implements a feedback system where the telemeter continuously measures the distance between the landing gear and the bay door, and this data is transmitted wirelessly to operators or control systems. This real-time feedback enables precise adjustment of the maneuvering mechanism without requiring repeated manual measurements, significantly improving adjustment efficiency while maintaining precision

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The telemeter system enables the landing gear system to self-measure and provide distance data without requiring external manual intervention. The automatic measurement and wireless transmission of data reduces the time and labor required for adjustment operations while maintaining precise control over the retraction clearance

Inventive Principle:
Principle #25Self-service

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 safe and efficient adjustment of the main landing gear mechanism from a remote location, reducing the risk of operator injury and improving the process by providing accurate measurements for proper retraction and door closure without manual intervention.

Implementation Method 1

a telemeter, a locking system (12) for locking the telemeter (11) on the external face of a wheel (6)

Methodology Applied
Scientific EffectLight: Light

Data Source

PatentUS11541993B2Tool for assisting with the adjustment of a maneuvering mechanism of a main landing gear
Publication Date: 2023.01.03 AIRBUS OPERATIONS (SAS)
  • US11541993B2 patent drawing
  • US11541993B2 patent drawing
  • US11541993B2 patent drawing

AI summary

An adjustment tool for adjusting a maneuvering mechanism of a main landing gear of an aircraft, the landing gear having a plurality of wheels. The tool includes a telemeter, a locking system for locking the telemeter on the external face of a wheel, a wireless communication unit that is connected to the telemeter and makes it possible, when the tool is being used, to connect the telemeter with a control device provided with a display screen.