Projectile Muzzle Blast Simulation via Direct Impact

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Solution Overview

Problem

Existing shock simulators cannot reproduce the specific environments of muzzle blasts encountered by projectiles, as they require a mechanical resonator that modifies the structural reality of the projectile.

Innovation Solution

A device comprising a suspension system to freely mount the projectile along its longitudinal axis, a propulsion system to propel an impactor towards the rear end of the projectile, and an impactor to directly strike the projectile, simulating the shock response spectrum of a muzzle blast.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a mechanical resonator is used to reproduce shock environments, then the shock response spectrum can be reproduced, but the structural reality of the projectile is modified

Engineering Contradiction:
Improveshock response spectrum reproductionVSAvoidstructural reality fidelity
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The invention removes the mechanical resonator from the test setup entirely. Instead of using a resonator to generate shocks, the projectile itself is suspended and directly impacted by a propelled mass. This extraction of the resonator eliminates the modification of structural reality while still achieving shock response spectrum reproduction through direct impact on the suspended projectile.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

Rather than using a resonator to generate vibrations that simulate muzzle blast, the invention inverts the approach by directly impacting the suspended projectile with a propelled mass. This inversion allows the projectile's own structural response to be measured without artificial resonance, achieving both accurate shock response spectrum reproduction and structural fidelity.

Inventive Principle:
Principle #13The other way round (Inversion)

2Adaptability or versatility

If a mechanical resonator is placed on the projectile, then shock environments can be simulated, but the device complexity increases

Engineering Contradiction:
Improveshock environment simulation capabilityVSAvoidtest setup complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The mechanical resonator is completely removed from the test setup. The shock simulation is achieved through a simpler configuration consisting of a suspension device, propulsion device, and impactor. This extraction reduces device complexity while maintaining shock environment simulation capability through direct impact on the suspended projectile.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention introduces a suspension device as an intermediary between the projectile and the impactor. This suspension system allows the projectile to be freely mounted and respond naturally to impact forces without requiring a mechanical resonator, thereby simplifying the overall device complexity while preserving shock simulation versatility.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If existing shock simulators are used, then equipment resistance can be tested, but muzzle blast specific environments cannot be reproduced

Engineering Contradiction:
Improveequipment resistance testingVSAvoidmuzzle blast environment reproduction
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The invention employs a dynamic suspension system that allows the projectile to move freely along its longitudinal axis during impact. This dynamic mounting approach enables the projectile to respond naturally to muzzle blast-like shocks, achieving both equipment resistance testing and specific muzzle blast environment reproduction that static existing simulators cannot provide.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention changes the fundamental parameters of the test setup by suspending the projectile freely rather than mounting it rigidly, and by using a propelled impactor instead of a mechanical resonator. These parameter changes enable the system to reproduce muzzle blast specific environments while maintaining equipment resistance testing capability.

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

The solution provides high fidelity simulation of the dynamic munition-related environment, allowing the projectile to be stressed as a whole without intermediate artifices, effectively reproducing the shock response spectrum specific to a projectile exit from a muzzle.

Implementation Method 1

a suspension device configured for suspending the projectile along the longitudinal direction thereof so that the projectile in the suspended position thereof is freely mounted along the longitudinal axis thereof

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 2

a propulsion device configured for being arranged facing the rear end of the projectile in the suspended position thereof at a predetermined distance therefrom; and an impactor configured for being propelled by the propulsion device, at a predefined velocity toward the rear end of the projectile

Methodology Applied
Scientific EffectMechanical force: Mechanical Force

Implementation Method 3

strike the rear end of the projectile in order to reproduce a shock response spectrum which is specific to an exit of the projectile from the muzzle

Methodology Applied
Scientific EffectImpact force: Impact Force

Data Source

PatentUS12313387B2Device and method for simulating a dynamic munition-related environment for a projectile, and simulation device-projectile assembly
Publication Date: 2025.05.27 NEXTER MUNITIONS SA
  • US12313387B2 patent drawing
  • US12313387B2 patent drawing

AI summary

A device for simulating a dynamic munition-related environment for a projectile, and a simulation device-projectile assembly including: a suspension device configured for suspending the projectile along the longitudinal direction of the projectile in such a way that the projectile is mounted freely along the longitudinal axis of the projectile; a propulsion device configured for being positioned facing the rear end of the projectile at a predefined distance from the projectile; and an impactor configured for being propelled, by the propulsion device, at a predetermined velocity toward the rear end of the projectile so as to strike the projectile so as to reproduce a shock response spectrum specific to an exit from a muzzle.