Ambient Curing of Epoxy Prepregs via Ammonia Flow

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Solution Overview

Problem

Current aerospace-grade composite material curing processes require high temperatures and pressures, making them expensive, limited in size, and complex, with tooling needing to withstand these conditions and match the coefficient of thermal expansion of prepregs.

Innovation Solution

Curing epoxy-containing prepreg composite materials at ambient temperature and pressure using an enclosed environment with a controlled delivery of ammonia-containing compounds, maintaining the prepreg at room temperature and atmospheric pressure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If high temperature and pressure are used for curing, then the curing reaction rate is improved, but the equipment cost and complexity increase

Engineering Contradiction:
Improvecuring reaction rateVSAvoidequipment complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent changes the chemical parameters of the resin system by using low-viscosity epoxy resins and specific amine hardeners that enable effective curing at ambient temperature and pressure, eliminating the need for high-temperature and high-pressure equipment while maintaining acceptable curing reaction rates

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces the mechanical/thermal curing system (ovens and autoclaves requiring high temperature and pressure) with a chemical curing system using ammonia-containing compounds that achieve curing at ambient conditions, substituting mechanical energy with chemical reaction energy

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If high temperature and pressure equipment is used, then the curing effectiveness is improved, but the production cost increases

Engineering Contradiction:
Improvecuring effectivenessVSAvoidproduction cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent modifies the chemical composition parameters by selecting specific low-viscosity epoxy resins and amine hardeners with appropriate reactivity ratios, enabling effective curing at ambient temperature and pressure, thereby eliminating expensive specialized equipment while maintaining curing effectiveness

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs consumable chemical agents (ammonia-containing compounds) that can be applied directly to the prepreg and allowed to evaporate or react, replacing expensive reusable equipment (autoclaves and ovens) with cheaper chemical systems

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

3Productivity

If high temperature curing is used, then the reaction rate is improved, but the tooling requirements become more stringent

Engineering Contradiction:
Improvereaction rateVSAvoidtooling availability
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

The patent changes the temperature parameter from high-temperature curing (250-355°F) to ambient temperature curing, which eliminates the requirement for tooling to withstand high temperatures and match thermal expansion coefficients, greatly expanding tooling material options and availability

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

Instead of adapting tooling to withstand high temperatures and match thermal properties, the patent inverts the approach by using chemical curing at ambient temperature, allowing any material to serve as tooling since extreme thermal conditions are eliminated

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

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

Enables efficient and cost-effective curing of composite materials without the need for high temperatures and pressures, allowing for larger parts and reduced tooling complexity, while maintaining the quality of the cured composite.

Implementation Method 1

delivering a flow of an ammonia-containing compound to the enclosed environment to a predetermined concentration via the inlet; maintaining the flow of the ammonia-containing compound to the enclosed environment at the predetermined concentration for a predetermined duration, and curing the epoxy-containing prepreg assembly

Methodology Applied
Scientific EffectChemical reaction (epoxy curing): Chemical Bonding

Implementation Method 2

the ammonia-containing compound may be derived from, without limitation, any compound capable of generating volatile ammonia such as ammonia carbonate, or pure ammonia, such as that supplied under pressure from a compressed gas cylinder

Methodology Applied
Scientific EffectVolatile ammonia generation: Evaporation

Data Source

PatentUS9738764B2Methods, systems and apparatuses for curing epoxy-containing prepreg composite assembly
Publication Date: 2017.08.22 THE BOEING CO
  • US9738764B2 patent drawing
  • US9738764B2 patent drawing
  • US9738764B2 patent drawing

AI summary

Methods and systems and components made according to the methods and systems, are disclosed relating to improved curing methods for epoxy resin-containing composite prepreg materials, wherein the composite prepreg materials are exposed to a flow of ammonia-containing compounds to fully cure the composite prepreg materials at substantially ambient temperatures and pressures.