Electromagnetic Circuit Interrupter for High Voltage DC Aircraft Power Systems

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Solution Overview

Problem

High voltage DC electromagnetic switches in aircraft power distribution systems face reduced component lifetime due to arcing, which conventional techniques have not adequately addressed for safety-critical applications.

Innovation Solution

An electromagnetic circuit interrupter that sustains an arc for a predetermined time before fully opening the contacts, allowing for the dissipation of inductive energy and minimizing contact sputtering, with the first predetermined distance being less than the second to control temperature rise below the melting point.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If conventional electromagnetic switches are used to interrupt high voltage DC circuits, then the switching speed is fast (microseconds), but the contact lifetime is reduced due to arcing and contact sputtering

Engineering Contradiction:
Improveswitching speedVSAvoidcontact lifetime
Core Design Contradiction:
SpeedVSReliability

Solution Approach 1:

The contact opening process is segmented into two distinct phases: first, the contacts are separated by a first predetermined distance to sustain an arc and dissipate inductive energy; second, after a predetermined time, the contacts are separated by a second predetermined distance to extinguish the arc and break the circuit. This segmentation allows the switching function to be divided into energy dissipation and circuit interruption, resolving the contradiction between fast switching and contact protection.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The arc is sustained for a predetermined time period before the contacts are fully opened. This preliminary action allows the inductive energy to be dissipated through the arc before the contacts reach temperatures that would cause melting and sputtering, thereby extending contact lifetime while maintaining effective circuit interruption.

Inventive Principle:
Principle #10Preliminary action

2Productivity

If the contacts are opened widely and quickly to break the circuit, then the circuit interruption is fast, but the inductive energy causes the contacts to become hot enough to melt and sputter

Engineering Contradiction:
Improvecircuit interruption speedVSAvoidcontact temperature and sputtering
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

The harmful inductive energy that normally causes contact overheating and sputtering is converted into a beneficial arc that sustains for a predetermined time. This arc serves as a controlled energy dissipation path, allowing the inductive energy to be released gradually through the arc rather than directly heating the contacts, thus protecting them from thermal damage.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The contacts are held at a first predetermined distance for a predetermined time to allow the arc to dissipate inductive energy before the contacts are fully separated. This preliminary energy dissipation action prevents the contacts from reaching melting temperatures, eliminating the harmful thermal effects while maintaining circuit interruption functionality.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If additional circuitry is added to dissipate inductive energy, then the contact lifetime is enhanced, but the device complexity increases

Engineering Contradiction:
Improvecontact lifetimeVSAvoidcircuit complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The electromagnetic switch contacts serve multiple functions: they act as both the switching element and the arc electrode for energy dissipation. The same contacts that open to interrupt the circuit also sustain the arc that dissipates inductive energy, eliminating the need for separate energy dissipation circuitry and maintaining device simplicity while extending contact lifetime.

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

Solution Approach 2:

The circuit interrupter uses its own contacts to dissipate the inductive energy through a controlled arc, rather than requiring external circuitry. The contacts themselves serve the dual purpose of switching and energy dissipation, making the system self-sufficient and avoiding additional components that would increase complexity.

Inventive Principle:
Principle #25Self-service

4Reliability

If the contacts are held at a small separation distance for a long time to dissipate energy, then contact sputtering is minimized, but the total switching time increases

Engineering Contradiction:
Improvecontact durabilityVSAvoidtotal switching time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The switching process is segmented into two phases with different priorities: first, a controlled arc sustains phase where contacts remain at a small distance to dissipate energy and protect against sputtering; second, a rapid opening phase where contacts are quickly separated to complete circuit interruption. This segmentation allows optimization of each phase for its specific function, minimizing overall switching time while protecting contact durability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

After the predetermined energy dissipation time, the contacts are rapidly separated by a second predetermined distance to quickly extinguish the arc and complete the circuit interruption. This rushing through the final separation phase minimizes the time the contacts are in a vulnerable state, reducing total switching time while maintaining contact protection during the critical energy dissipation period.

Inventive Principle:
Principle #21Skipping (Rushing through)

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 approach significantly enhances the operational lifetime and reliability of the contacts by dissipating inductive energy before the contacts become hot enough to melt, reducing contact sputtering and arc restrike.

Implementation Method 1

separate first and second electrical contacts by a first predetermined distance for a predetermined time so as to sustain an arc when the contact mechanism is opened

Methodology Applied
Scientific EffectArcing: Electric Arc

Implementation Method 2

dissipate the inductive energy stored in the circuit so as to minimise the energy dissipated in the electromagnetic switches themselves

Methodology Applied
Scientific EffectInductive energy dissipation: Joule Heating

Implementation Method 3

separate the first and second electrical contacts by a second predetermined distance after the predetermined time so as to extinguish the arc

Methodology Applied
Scientific EffectArc extinction: Electric Arc

Data Source

PatentUS8564389B2Electromagnetic circuit interrupter
Publication Date: 2013.10.22 GE AVIATION SYST LTD
  • US8564389B2 patent drawing
  • US8564389B2 patent drawing
  • US8564389B2 patent drawing

AI summary

In one aspect, the present invention provides an electromagnetic circuit interrupter for use in a high voltage direct current (DC) aircraft power distribution system. The electromagnetic circuit interrupter comprises a contact mechanism operable to separate first and second electrical contacts by a first predetermined distance d1 for a predetermined time τ so as to sustain an arc when the contact mechanism is opened. The contact mechanism is further operable to separate the first and second electrical contacts by a second predetermined distance d2 after the predetermined time τ so as to extinguish the arc. The first predetermined distance d1 is less than said second predetermined distance d2. By deliberately sustaining the arc for a relatively long period of time, this aspect of the present invention is particularly useful for extending the operational lifetime of the contacts and thereby of the electromagnetic circuit interrupter itself.