Segmented Artillery Charge Shell for Long-Length Stability

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Solution Overview

Problem

Existing artillery charges face stability issues due to the collision of modular shells at contact points, leading to a loss of propelling charge capacity and limited range, especially in longer shells.

Innovation Solution

A shell design incorporating a housing with a stabilizing element, such as a stabilizing disk, that separates the cavity into subcavities, allowing for improved mechanical stability and efficient use of propelling charge, especially in shells over 1100 mm long.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of moving object

If modular shells are used to increase propelling charge quantity, then the range of the projectile is increased, but the cover and floor collide at the contact points leading to a loss of maximum available propelling charge capacity

Engineering Contradiction:
Improveshell lengthVSAvoidpropelling charge capacity
Core Design Contradiction:
Length of moving objectVSQuantity of substance

Solution Approach 1:

The shell is divided into multiple modular sections that can be connected end-to-end. Each section has its own floor and cover, eliminating the need for intermediate contact points between sections. This segmentation allows the shell to achieve the required length for increased range while maintaining full propelling charge capacity in each section without collision losses.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention transitions from a single-section shell design to a multi-section modular arrangement, adding the dimension of serial connection along the longitudinal axis. This dimensional change allows the shell to achieve greater length without the traditional cross-sectional collision problems that limit propelling charge capacity in single-section designs.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Length of moving object

If the shell length is increased to increase range, then the propelling charge quantity is increased, but the stability of the shell deteriorates

Engineering Contradiction:
Improveshell lengthVSAvoidshell stability
Core Design Contradiction:
Length of moving objectVSStability of the object's composition

Solution Approach 1:

The shell is divided into multiple modular sections with individual floors and covers. This segmentation creates multiple rigid compartments that maintain structural stability even as the overall shell length increases. Each section acts as an independent stability unit, preventing the shell from becoming unstable due to excessive length.

Inventive Principle:
Principle #1Segmentation

3Length of moving object

If the shell length is increased beyond 1100 mm, then the range is increased, but the stability becomes insufficient without additional stabilizing elements

Engineering Contradiction:
Improveshell lengthVSAvoidshell stability
Core Design Contradiction:
Length of moving objectVSStability of the object's composition

Solution Approach 1:

The shell is divided into multiple modular sections with individual floors and covers. This segmentation creates multiple rigid compartments that maintain structural stability even as the overall shell length increases. Each section acts as an independent stability unit, preventing the shell from becoming unstable due to excessive length.

Inventive Principle:
Principle #1Segmentation

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

Enhances the stability and range of artillery projectiles by allowing for increased propelling charge capacity without exceeding gun diameter limits, while maintaining mechanical integrity and ease of handling.

Implementation Method 1

The propelling charge serves to cause acceleration of the artillery projectile by means of an exothermic reaction

Methodology Applied
Scientific EffectExothermic reaction: Exothermic Reaction

Implementation Method 2

an igniter tube (70) extending in the longitudinal direction (L), wherein a flame front ignites the propelling charge (90) in the cavity (12)

Methodology Applied
Scientific EffectFlame front: Combustion

Data Source

PatentUS20250362118A1Shell and artillery charge
Publication Date: 2025.11.27 NITROCHEM ASCHAU
  • US20250362118A1 patent drawing
  • US20250362118A1 patent drawing
  • US20250362118A1 patent drawing

AI summary

A shell includes a housing a stabilizing disk and an ignition tube, wherein the shell and/or the housing are combustible, wherein the shell extends in a longitudinal direction, wherein the housing includes a floor, a cover and a cleading, wherein a cavity is formed inside the shell, wherein the cavity is configured to receive propelling charge, wherein the cavity is separated by the stabilizing element into a primary subcavity and a secondary subcavity.