Aircraft Engine Robot Mounting for Stable Borescope Inspection

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Solution Overview

Problem

During in situ inspection of aircraft engines, it is challenging to maintain the position and orientation of mobile inspection robots and borescopes due to vibrations and movements of the engine, which can disrupt the predefined inspection path and data reproducibility.

Innovation Solution

A device with a positioning and orientation adjusting unit and a rigid connector is used to secure the mobile inspection robot to the aircraft engine, ensuring that the relative position and orientation of the robot remain fixed in at least one degree of freedom, even when the engine moves, by employing a suspension or holding device with adjustable components like telescopic extension arms and stay cables.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If the mobile inspection robot is held in a fixed position relative to the aircraft engine, then the position stability is improved, but the adaptability to engine movements deteriorates

Engineering Contradiction:
Improveposition stabilityVSAvoidadaptability to engine movements
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The holding device incorporates adjustable components including telescopic extension arms that can dynamically change length, and positioning units with multiple degrees of freedom that can adapt the robot's position and orientation. This dynamic structure allows the system to maintain stable positioning while adapting to engine vibrations and movements during inspection operations

Inventive Principle:
Principle #15Dynamics

2Stability of the object's composition

If the connector provides rigid connection in all degrees of freedom, then the position and orientation fixation is improved, but the device complexity increases

Engineering Contradiction:
Improverelative position fixationVSAvoidconnector structure complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The connector provides rigid connection with fixed relative position specifically in the critical inspection directions (along the borescope insertion path), while allowing flexibility in other degrees of freedom through the adjustable positioning units. This selective rigidity approach ensures inspection accuracy without requiring complete rigid fixation in all directions

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If the positioning adjusting unit is highly adjustable, then the adaptability to different inspection paths is improved, but the device complexity increases

Engineering Contradiction:
Improveadjustability to inspection pathsVSAvoidpositioning unit complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The positioning and orientation adjusting unit is designed with multiple degrees of freedom and telescopic extension arms that can accommodate various inspection paths and angles. This universal positioning mechanism can adapt to different borescope insertion points and trajectories, making the device versatile for multiple inspection scenarios without requiring separate specialized fixtures for each path

Inventive Principle:
Principle #6Universality (Multi-functionality)

Data Source

PatentUS20240425205A1Device for securing mobile inspection means to objects to be inspected
Publication Date: 2024.12.26 LUFTHANSA TECHNIK AG
  • US20240425205A1 patent drawing
  • US20240425205A1 patent drawing
  • US20240425205A1 patent drawing

AI summary

A device secures a mobile inspection robot to an aircraft engine. The mobile inspection robot is designed to insert a borescope into the aircraft engine to be inspected. The device includes: at least one positioning or orientation adjusting unit configured to adjust the position or orientation of the mobile inspection robot in relation to the aircraft engine to be inspected and at least one connector for providing a connection, which is rigid in at least one degree of freedom, between the mobile inspection robot and the aircraft engine to be inspected, in order to fix, in at least one degree of freedom, the relative position or orientation of the mobile inspection robot in relation to the aircraft engine to be inspected.