Aircraft Shielded Supply Line Arcing Detection

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Solution Overview

Problem

In aircraft systems, the segregation distance between electrical lines and fluid lines, particularly those carrying flammable fluids, is often excessively large due to safety concerns about arcing and short circuits, which wastes installation space and increases the risk of ignition.

Innovation Solution

A supply system with an electrically conductive shield surrounding the electrical line and a detection unit that monitors differential or absolute currents, generating a warning signal if a threshold is exceeded, allowing for automatic protection against arcing and short circuits, thereby reducing the segregation distance without compromising safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional protection devices and large segregation distances are used between electrical lines and fluid lines, then safety is maintained, but installation space is wasted and the system becomes more complex

Engineering Contradiction:
ImprovesafetyVSAvoidinstallation space
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The patent replaces traditional mechanical protection devices (circuit breakers, physical barriers) with an electrical detection system that uses current monitoring to detect arcing events. The detection unit continuously monitors the electrical line for abnormal current patterns indicative of arcing, enabling early detection and response without requiring large physical separation distances or complex mechanical protection mechanisms.

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

Solution Approach 2:

The patent introduces an intermediate detection system between the electrical line and the flammable fluid line. This detection unit acts as an intermediary that monitors for arcing events and triggers protective actions, allowing the system to maintain safety with reduced segregation distances by providing an early warning mechanism that prevents ignition before it can occur.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If large segregation distances are maintained between electrical lines and fluid lines, then safety is improved, but device complexity and weight increase

Engineering Contradiction:
ImprovesafetyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical protection systems and large physical barriers with a streamlined electrical detection system. The detection unit uses electrical current monitoring to identify arcing events, eliminating the need for complex mechanical interlocks, physical shields, or elaborate safety mechanisms while maintaining or improving safety performance.

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

Solution Approach 2:

The detection system is integrated directly into the electrical line infrastructure, using the existing electrical components and wiring to perform detection functions. The system monitors its own operational status by detecting abnormal current patterns, eliminating the need for separate external monitoring systems or complex control mechanisms.

Inventive Principle:
Principle #25Self-service

3Reliability

If traditional circuit breakers are used for protection, then safety is maintained, but reaction time is too slow to prevent ignition of flammable fluids

Engineering Contradiction:
ImprovesafetyVSAvoidreaction time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The detection unit continuously monitors the electrical line for signs of arcing before the situation escalates to a dangerous level. By detecting abnormal current patterns early in the arcing process, the system can trigger protective actions (such as shutting off fuel supply or activating suppression systems) before ignition occurs, rather than waiting for traditional protection devices to react after a fault has fully developed.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The detection unit provides continuous real-time feedback on the electrical line's operational status by monitoring current patterns. When arcing is detected, the system immediately responds by triggering protective measures, creating a rapid feedback loop that eliminates the time delay inherent in traditional protection devices that only activate after a fault condition is fully established.

Inventive Principle:
Principle #23Feedback

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

This solution enables safer and more efficient use of space by quickly detecting and mitigating arcing events, reducing the risk of ignition and structural damage, and allowing for closer proximity of electrical and fluid lines, thus enhancing safety and reducing weight and maintenance complexity.

Implementation Method 1

said detection unit is adapted for detecting a differential current over the at least one core or an absolute current between two of the shield, the at least one core and a ground potential

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Implementation Method 2

an electrically conductive shield and a detection unit having at least two electrical inputs. The at least one electrical line comprises at least one core connectable to a pole of the current source, wherein the shield surrounds the at least one core under a distance and creates an intermediate space between the at least one core and the shield

Methodology Applied
Scientific EffectElectromagnetic shielding: Faraday Cage

Data Source

PatentUS9305731B2Supply system for an aircraft, use of a shielded supply line in an aircraft and an aircraft with a supply system
Publication Date: 2016.04.05 AIRBUS OPERATIONS GMBH
  • US9305731B2 patent drawing
  • US9305731B2 patent drawing
  • US9305731B2 patent drawing

AI summary

A supply system for supplying energy in an aircraft includes at least one electrical line including at least one core connectable to a pole of a current source, an electrically conductive shield, and a detection unit having at least two electrical inputs. The shield surrounds the at least one core under a distance and creates an intermediate space between the at least one core and the shield. At least one port of the detection unit is connected to the at least one core. At least another port of the detection unit is connected to at least one of the shield and the at least one core. The detection unit is adapted for detecting a differential current over the at least one core or an absolute current between the shield and a ground potential for generating a warning signal if a predetermined threshold value for the detected current value is exceeded.