High Surface Area Carbon Black for Propellant Electrostatic Dissipation

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Solution Overview

Problem

Energetic compositions, such as solid propellants, are susceptible to premature ignition or explosion due to electrostatic charge buildup during manufacturing, transportation, and storage, with existing solutions like graphite and carbon fibrils affecting processability and rheology, and being costly or complex to implement.

Innovation Solution

Incorporating high surface area carbon black with a specific surface area of at least 1,200 m2/g in amounts from 0.05% to 0.25% by weight into energetic compositions to enhance electrostatic charge dissipation without compromising processing or rheological properties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If graphite is added to energetic materials to reduce electrostatic discharge susceptibility, then electrostatic charge dissipation is improved, but at least 16% weight of graphite is required which adversely affects performance of the energetic materials

Engineering Contradiction:
Improveelectrostatic charge dissipationVSAvoidamount of graphite required
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The patent changes the particle size parameter of carbon black to ultra-fine dimensions (0.003-0.02 micrometers) and increases specific surface area (50-2000 m²/g), enabling effective electrostatic charge dissipation at much lower concentrations (0.1-5.0 wt%) compared to conventional graphite additions

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent uses carbon black as a composite additive within the energetic material matrix, leveraging its high surface area to volume ratio and electrical conductivity properties to achieve electrostatic discharge protection with minimal impact on the base composition's performance

Inventive Principle:
Principle #40Composite materials

2Reliability

If graphite fibers are used in solid propellant compositions to reduce electrostatic discharge, then electrostatic charge dissipation is improved, but even small amounts markedly increase the viscosity of propellant compositions, resulting in detrimental effects on processability and propellant rheology

Engineering Contradiction:
Improveelectrostatic charge dissipationVSAvoidprocessability and propellant rheology
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent changes the form of carbon additive from fibrous to ultra-fine particulate, dramatically reducing the aspect ratio and enabling effective electrostatic charge dissipation without the viscosity-increasing effects associated with fiber reinforcement

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs ultra-fine carbon black particles that can be effectively dispersed and function at low concentrations, replacing the need for higher amounts of fibrous additives that would compromise processing

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

3Reliability

If carbon fibrils are added to energetic compositions to reduce electrostatic discharge susceptibility, then electrostatic charge dissipation is improved, but they detrimentally impact the processability and rheology of the energetic compositions

Engineering Contradiction:
Improveelectrostatic charge dissipationVSAvoidprocessability and rheology
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent transforms the carbon additive morphology from fibrillar to ultra-fine particulate with controlled size distribution (0.003-0.02 micrometers), achieving electrostatic charge dissipation functionality while maintaining favorable rheological properties for processing

Inventive Principle:
Principle #35Parameter changes

4Strength

If HTPB binder is used in solid rocket propellant compositions, then the propellant composition has good mechanical properties, but HTPB is nonpolar and has high electrical resistivity, making the propellant more susceptible to charge buildup and potential catastrophic electrostatic discharge

Engineering Contradiction:
Improvemechanical propertiesVSAvoidsusceptibility to electrostatic discharge
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent introduces ultra-fine carbon black particles as an intermediary conductive phase within the nonpolar HTPB binder matrix, creating conductive pathways that enable electrostatic charge dissipation while preserving the mechanical advantages of the HTPB system

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent creates a composite binder system where ultra-fine carbon black particles are dispersed within the HTPB matrix, combining the mechanical properties of HTPB with the electrostatic charge dissipation capabilities of conductive carbon particles

Inventive Principle:
Principle #40Composite materials

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 high surface area carbon black effectively reduces electrostatic charge buildup without affecting breakdown voltage, improving safety and reducing production costs by maintaining the energetic composition's performance and processability.

Implementation Method 1

the high surface area carbon black effectively reduces electrostatic charge buildup

Methodology Applied
Scientific EffectElectrical conduction: Conduction (electrical)

Implementation Method 2

electrostatic charge buildup during manufacturing, transportation, storage, or use

Methodology Applied
Scientific EffectElectrostatic discharge: Electrostatic Discharge

Data Source

PatentUS11434181B2Precursor formulations for a propellant composition including high surface area amorphous carbon black
Publication Date: 2022.09.06 NORTHROP GRUMMAN SYSTEMS CORP
  • US11434181B2 patent drawing
  • US11434181B2 patent drawing
  • US11434181B2 patent drawing

AI summary

A precursor formulation of an energetic composition with improved electrostatic charge dissipation, including an amorphous carbon black having a specific surface area of at least about 1,200 m2/g, in an amount from about 0.05% by weight to about 0.25% by weight. Also disclosed is a precursor formulation of a propellant composition with improved electrostatic charge dissipation. The amorphous carbon black having a specific surface area of at least about 1,200 m2/g may enhance electrostatic charge dissipation of the HTPB-based propellant composition, without affecting a breakdown voltage of the propellant composition.