Monitoring Module Circuit for Aircraft Cable Interruption Detection

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Solution Overview

Problem

Existing electrical installations in aircraft, which rely on monitoring modules to detect cable interruptions, face challenges in reducing energy consumption and complexity while maintaining reliability, especially in environments sensitive to vibrations.

Innovation Solution

The proposed electrical installation incorporates a monitoring module that uses transistors and resistors to detect cable interruptions by generating distinct potentials on a measurement cable, allowing for efficient detection of power supply cable interruptions without requiring complex sensors, and is designed to be vibration-resistant and energy-efficient.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If inductive sensors are used to detect cable interruptions, then cable interruption detection capability is improved, but device complexity and sensitivity to vibrations increase

Engineering Contradiction:
Improvecable interruption detection capabilityVSAvoidmonitoring module complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces inductive sensors with a purely electrical monitoring approach using transistors and resistors. The monitoring module detects cable interruptions by measuring electrical potential differences generated when cables are interrupted, eliminating the need for mechanical or inductive sensing components. This substitution reduces device complexity and vibration sensitivity while maintaining detection capability.

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

Solution Approach 2:

The patent uses simple, inexpensive electrical components (transistors and resistors) instead of complex inductive sensors. These basic components are readily available, cost-effective, and sufficient for the detection function, reducing overall system complexity and cost while achieving the required reliability.

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

2Reliability

If inductive sensors are used to detect cable interruptions, then cable interruption detection capability is improved, but energy consumption increases

Engineering Contradiction:
Improvecable interruption detection capabilityVSAvoidmonitoring module energy consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The patent replaces energy-intensive inductive sensors with a passive electrical circuit using transistors and resistors. The monitoring module operates by detecting voltage potentials generated naturally in the circuit when cables are interrupted, requiring minimal energy for operation while maintaining reliable detection capability.

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

3Device complexity

If simple monitoring modules are used, then device complexity and energy consumption are reduced, but reliability in vibration-sensitive environments deteriorates

Engineering Contradiction:
Improvemonitoring module complexityVSAvoidvibration resistance
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent uses purely electrical components (transistors and resistors) that are inherently resistant to vibrations, eliminating mechanical moving parts that would be sensitive to vibration. The electrical circuit detects cable interruptions through potential difference measurements, which remain stable and reliable in vibration-prone aircraft environments.

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

Data Source

PatentUS11762039B2Electrical installation comprising a monitoring module
Publication Date: 2023.09.19 CROUZET AUTOMATISMES SA
  • US11762039B2 patent drawing
  • US11762039B2 patent drawing
  • US11762039B2 patent drawing

AI summary

Electrical installation comprising a monitoring module positioned between a sensor connected to a measurement cable and first and second power supply cables for the sensor. The monitoring module comprises a first transistor comprising a first and a second power electrode and a control electrode, the first and the second power electrodes of the first transistor being electrically connected to the second power supply cable and to the measurement cable, respectively, so that, when the first transistor is in the closed state thereof, a first fault value is generated on the measurement cable. The control electrode of the first transistor is connected to the first power supply cable so that the loss of first potential on the first power supply cable, caused by the interruption thereof, automatically triggers the switching of the first transistor to the closed state thereof.