Linear Shaped Charge Liner Geometry for Stable Jet Cutting

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Solution Overview

Problem

Linear shaped charges face reduced cutting effectiveness due to detachment from target surfaces, leading to decreased penetration depth and increased cut width, especially on complex or wet surfaces, resulting in unpredictable and dangerous cutting outcomes.

Innovation Solution

A linear shaped charge with a V-shaped cross section, featuring a specific apex angle of 101.5 to 106.5 degrees and a stand-off distance of 0.99S to 1.21S, where S is the distance between the liner and the apex, ensuring a more stable and continuous cutting jet that maintains homogeneity and precision, even on irregular surfaces.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the charge is applied to a wet or complex surface, then attachment difficulty increases, but cutting effectiveness decreases due to separation

Engineering Contradiction:
Improveattachment to target surfaceVSAvoidcutting effectiveness
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The invention changes the geometric parameters of the liner and explosive element (apex angle of 101.5-106.5 degrees, stand-off distance ratio of 0.99S to 1.21S) to optimize jet formation and stability, making the cutting action more reliable even when attachment conditions are poor

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If the stand-off distance is increased due to surface irregularities, then jet stability decreases and break-up occurs, but the charge geometry needs to accommodate varying distances

Engineering Contradiction:
Improveaccommodation of stand-off distance variationsVSAvoidjet homogeneity
Core Design Contradiction:
Adaptability or versatilityVSStability of the object's composition

Solution Approach 1:

The invention optimizes the stand-off distance parameter (SD:S ratio of 0.99 to 1.21) in combination with the apex angle to ensure the jet forms near the target surface, reducing travel distance and maintaining jet homogeneity and stability even when stand-off distance varies due to surface irregularities

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If the apex angle is optimized for jet formation, then cutting precision improves, but manufacturing tolerance requirements increase

Engineering Contradiction:
Improvecutting precisionVSAvoidapex angle tolerance
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The invention specifies an apex angle range of 101.5 to 106.5 degrees, which is a relatively wide tolerance band that balances cutting precision requirements with manufacturing feasibility, allowing for practical production while maintaining effective jet formation

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 optimized geometry of the charge produces a longer, thinner cutting jet that remains stable and effective over greater distances, ensuring precise cutting and reliability across various target configurations, including complex and wet surfaces, with reduced risk of detachment-induced failures.

Implementation Method 1

when the explosive element is detonated

Methodology Applied
Scientific EffectDetonation: Detonation

Implementation Method 2

A linear shaped charge is an explosive device for cutting a target object

Methodology Applied
Scientific EffectShaped charge: Shaped Charge

Data Source

PatentEP2526368B1Linear shaped charge
Publication Date: 2016.09.21 JET PHYSICS
  • EP2526368B1 patent drawingFigure 1~2

AI summary

The present invention relates to a linear shaped charge (1) comprising an explosive element (2), a liner (4), a face (6) for application to a target object (8) and a space (14) between the liner and the face, the liner being arranged for projection through the space, towards the face, when the explosive element is detonated, and the explosive element and the liner having a V-shaped cross section, the liner (4) lying in a groove of the V-shaped cross section of the explosive element (2), the liner having a length L of a side furthest from the face (6) and the liner (4) having a thickness T taken perpendicular to said length L, wherein an angle a of an apex of the liner nearest the face is 101.5 to 106.5 degrees, and a stand-off distance SD between the face and a point of the liner nearest the face is 0.99S to 1.21S, S being a distance, parallel the stand-off distance SD, between the point of the liner (4) nearest the face (6) and the apex of the liner nearest the face.