Aircraft Plug-in Connector Test System for Rapid Fault Detection

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Solution Overview

Problem

Current aircraft cabling systems with multiple plug-in connectors require extensive and time-consuming fault-finding processes, leading to high maintenance expenditures due to complex and extensive cabling.

Innovation Solution

A test system comprising a transmitting device that sends a test signal to plug-in connectors and a receiving device that outputs an acknowledgement signal, allowing for rapid and efficient testing of connectors by checking contact resistance and fault detection without disrupting existing data or energy transmission.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If extensive aircraft cabling systems with multiple plug-in connectors are used to connect electronic devices, then the electronic devices can be connected for energy supply and data communication, but the fault-finding expenditure and time increase significantly

Engineering Contradiction:
Improveconnectivity capabilityVSAvoidfault-finding time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The patent applies preliminary action by integrating test functions directly into the plug-in connectors before faults occur. Each connector includes a test signal generator and evaluator that continuously or periodically test the connection status, so when a fault occurs, the location is already identified or quickly detectable, eliminating the need for time-consuming manual fault-finding procedures after the fault occurs.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent implements feedback by having each plug-in connector continuously monitor its own connection status and provide this information to a central evaluation device. The test signal generator sends test signals through the connectors, and the evaluator receives feedback signals from each connector to determine connection status, enabling real-time monitoring and immediate fault detection without manual intervention.

Inventive Principle:
Principle #23Feedback

2Ease of manufacture

If multiple plug-in connectors are used in the aircraft cabling system to enable segment-by-segment installation, then the installation flexibility is improved, but the complexity of fault finding increases

Engineering Contradiction:
Improveinstallation flexibilityVSAvoidfault-finding complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent applies segmentation by dividing the aircraft cabling system into multiple independent plug-in connector segments, each equipped with its own test signal generator and evaluation capability. This allows each segment to be tested independently, so faults can be localized to specific connectors rather than requiring systematic testing of the entire cabling system, reducing fault-finding complexity despite the modular structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements self-service by enabling each plug-in connector to autonomously perform self-diagnosis through integrated test signal generators and evaluators. Each connector tests its own connection status and provides self-generated test data to the evaluation device, eliminating the need for external manual testing equipment or procedures and simplifying the overall fault-finding process.

Inventive Principle:
Principle #25Self-service

3Measurement precision

If traditional fault-finding methods are used where plug-in connections are detached and manually checked, then individual plugs can be measured, but the maintenance time and expenditure increase

Engineering Contradiction:
Improvefault detection accuracyVSAvoidmaintenance efficiency
Core Design Contradiction:
Measurement precisionVSProductivity

Solution Approach 1:

The patent replaces the mechanical manual fault-finding system with an automated electrical testing system. Instead of physically detaching and manually measuring connectors, the system uses electrical test signals transmitted through the connectors to automatically detect faults. This substitution maintains measurement precision through electrical testing while dramatically improving maintenance efficiency by eliminating manual disassembly and measurement procedures.

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

Solution Approach 2:

The patent introduces an intermediary automated evaluation device that mediates between the plug-in connectors and the fault-finding process. This intermediary device receives test signals from connectors, evaluates the connection status, and provides fault information, replacing the need for human operators to manually test each connector while maintaining accurate fault detection capabilities.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 rapid and efficient testing of complex cabling systems, significantly reducing maintenance time as the system can test multiple connectors simultaneously and identify faults without additional power supply lines or separate power sources.

Implementation Method 1

a transmitting device which is designed for sending out at least one predetermined test signal for the plug-in connectors to be tested

Methodology Applied
Scientific EffectElectrical signal transmission: Conduction (electrical)

Implementation Method 2

at least one receiving device for each plug-in connector to be tested which is electrically coupled with the respective plug-in connector and which is designed for receiving the transmitted test signal

Methodology Applied
Scientific EffectSignal detection:

Data Source

PatentUS9310415B2Test system for plug-in connectors, aircraft or spacecraft and method
Publication Date: 2016.04.12 AIRBUS OPERATIONS GMBH
  • US9310415B2 patent drawing
  • US9310415B2 patent drawing
  • US9310415B2 patent drawing

AI summary

A test system for plug-in connectors, especially for plug-in connectors in an airplane. A transmitting device which is designed for sending out a test signal to the plug-in connectors to be tested, and comprising at least one receiving device for each plug-in connector to be tested which is electrically coupled with the respective plug-in connector and which is designed for receiving the transmitted test signal and outputting an acknowledgement signal in response to receiving the transmitted test signal. Furthermore, the present invention creates an aircraft or a spacecraft and a method.