Superconductor Rail Launcher Circuit Efficiency

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Solution Overview

Problem

Current electromagnetic rail launchers face low energy efficiency due to high circuit resistance, leading to significant energy losses and increased volume and mass, with existing power sources like capacitors offering low energy density and complex technologies required for higher efficiencies.

Innovation Solution

The integration of superconductor means surrounding the rails to generate magnetic induction perpendicular to the rail plane, forming a closed electrical circuit with superconductor coils or dipolar electromagnets, allowing for simultaneous current generation and supply, thereby reducing the required current intensity and enhancing energy transfer efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If high intensity currents (100 kA to 10 MA) are used to launch projectile at high speed (>3 km/s), then launching speed is improved, but energy efficiency deteriorates due to significant Joule losses from circuit resistance

Engineering Contradiction:
Improveprojectile launch speedVSAvoidenergy efficiency
Core Design Contradiction:
SpeedVSLoss of energy

Solution Approach 1:

The patent changes the electrical resistance parameter of the circuit by introducing superconducting materials with near-zero resistance. This fundamental parameter change allows maintaining high launch speeds while dramatically reducing Joule losses, as the circuit resistance is reduced from significant values to negligible levels.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs composite material structure combining superconducting materials (for zero-resistance current transmission) with conventional conducting materials (for structural support and magnetic field generation). This composite approach enables both high efficiency and functional performance in the rail launcher system.

Inventive Principle:
Principle #40Composite materials

2Power

If strong inductance coil with long wire length is used to limit current peak, then current control is improved, but total circuit resistance increases making energy efficiency worse

Engineering Contradiction:
Improvecurrent control capabilityVSAvoidcircuit resistance
Core Design Contradiction:
PowerVSLoss of energy

Solution Approach 1:

The patent changes the resistance parameter of the inductance coil by using superconducting wire instead of conventional wire. This allows maintaining the required inductance value (for current control) while reducing the resistance to near-zero, eliminating the trade-off between current control capability and energy efficiency.

Inventive Principle:
Principle #35Parameter changes

3Device complexity

If capacitor-based impulse voltage sources are used to power the launcher, then simplicity of power source is improved, but energy density is limited and volume/mass increase significantly

Engineering Contradiction:
Improvepower source simplicityVSAvoidvolume and mass
Core Design Contradiction:
Device complexityVSQuantity of substance

Solution Approach 1:

The patent changes the energy storage parameter by transitioning from capacitive energy storage (low energy density) to inductive energy storage in superconducting coils (high energy density). This allows storing the same energy in much smaller volume and mass, fundamentally changing the power source characteristics.

Inventive Principle:
Principle #35Parameter changes

4Ease of manufacture

If conventional conducting materials are used for rails and coils, then ease of manufacture is improved, but temperature rise during launching increases complicating design

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidtemperature rise
Core Design Contradiction:
Ease of manufactureVSTemperature

Solution Approach 1:

The patent changes the thermal parameter of the system by using superconducting materials that operate at low temperatures. This fundamentally alters the thermal management approach from dissipating heat to maintaining cryogenic temperatures, eliminating the temperature rise problem during high-current launching operations.

Inventive Principle:
Principle #35Parameter changes

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 significantly increases energy efficiency and compactness of rail launchers, achieving nearly 90% energy retention and reducing temperature rise, enabling higher launching frequencies and longer rail service life with lower current intensities, while simplifying the technology used.

Implementation Method 1

superconductor means able to generate a magnetic induction of a direction perpendicular to the plane formed by the rails and located therebetween during the flow of a current therein

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

generating a first Laplace force on the sabot which is then accelerated within the gun

Methodology Applied
Scientific EffectLorentz force: Lorentz Force

Implementation Method 3

supply circuit comprises the superconductor means

Methodology Applied
Scientific EffectSuperconductivity: Superconductivity

Data Source

PatentUS9032857B2Electromagnetic rail launchers and associated projectile-launching method
Publication Date: 2015.05.19 ETAT FR REPRESENTE PAR LE DELEGUE GENERAL POUR LARMEMENT
  • US9032857B2 patent drawing
  • US9032857B2 patent drawing
  • US9032857B2 patent drawing

AI summary

The present invention relates to the field of electromagnetic rail launchers, and particularly to a rail launcher and an associated projectile-launching process including at least two longitudinal rails connected to a power supply circuit of these two rails, these rails being at least partially surrounded by superconductor elements able to generate a magnetic induction of a direction perpendicular to the plane formed by the rails and located therebetween during the flow of a current therein, launcher wherein the supply circuit includes the superconductor elements.