Composite Curing Mold Using Resin Recirculation Pressure

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Solution Overview

Problem

Existing methods for manufacturing turbomachine components with tight geometry tolerances using composite materials face challenges in maintaining mechanical performance and geometry precision due to resin loss during the manufacturing process, leading to increased costs.

Innovation Solution

A curing mold with an air gap and sliding pistons that utilize surplus resin to apply hydrostatic pressure to the preform, ensuring controlled temperature and pressure conditions for curing without additional resin consumption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a preform is cured in an autoclave under vacuum and pressure to achieve high mechanical performance, then the mechanical performance is improved, but the geometry tolerance cannot be maintained for tight tolerance components

Engineering Contradiction:
Improvemechanical performanceVSAvoidgeometry tolerance
Core Design Contradiction:
StrengthVSManufacturing precision

Solution Approach 1:

The autoclave process is segmented into two distinct phases: first, curing the preform under vacuum without pressure to achieve geometry precision; second, applying pressure after curing to achieve high mechanical performance. This temporal segmentation allows both geometry tolerance and mechanical performance requirements to be satisfied sequentially.

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If additional resin is used to apply hydrostatic pressure to the preform in the air gap, then the preform can be cured under controlled pressure conditions, but resin consumption increases

Engineering Contradiction:
Improvecontrolled pressure conditionsVSAvoidresin consumption
Core Design Contradiction:
Manufacturing precisionVSLoss of substance

Solution Approach 1:

The system uses the preform's own resin, which is already present in the air gap, to apply hydrostatic pressure during curing. The resin is recirculated through channels in the mold bodies, eliminating the need for additional resin consumption while maintaining controlled pressure conditions throughout the curing process.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The resin that would normally be lost or wasted is recovered and recirculated through the channels in the mold bodies. This recovered resin is used to apply hydrostatic pressure to the preform, transforming what would be a loss into a useful resource that maintains pressure control during curing.

Inventive Principle:
Principle #34Discarding and recovering

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 allows for the production of turbomachine components with high mechanical performance and tight geometry tolerances while minimizing resin waste and associated costs.

Implementation Method 1

a heating member designed to heat the preform in the air gap to a first temperature, so as to reduce the viscosity of the resin

Methodology Applied
Scientific EffectViscosity reduction through heating: Heating

Implementation Method 2

an injection member designed to inject fluid under pressure into the or each primary channel... so as to compress the resin that has entered the second chamber of said secondary channel from the preform into the air gap, so as to put the preform under hydrostatic pressure

Methodology Applied
Scientific EffectHydrostatic pressure: Pressure Increase

Implementation Method 3

the heating member heats the preform to the second temperature, so as to cure the preform

Methodology Applied
Scientific EffectPolymerization through heating: Heating

Data Source

PatentUS12491668B2Curing mold for manufacturing a turbomachine component made of composite material from a preform and method for producing a component by means of such a mold
Publication Date: 2025.12.09 SAFRAN SA
  • US12491668B2 patent drawing
  • US12491668B2 patent drawing
  • US12491668B2 patent drawing

AI summary

The invention relates to a curing mold (10) for manufacturing a turbomachine component made of composite material from a preform (200), comprising: —a first and a second body (11, 12) defining an air gap receiving the preform; —at least one primary channel (21) arranged in the first and/or the second body; —an injection member (22) of a pressurized fluid in the primary channels; —at least one secondary channel (23), in which a piston (24) slides, which delimits, on the one hand, a first chamber (26) in communication with the or a primary channel and, on the other hand, a second chamber (27) in communication with the air gap, and which is designed to compress thermosetting resin which has entered the second chamber from the preform in the air gap, so as to put the preform under hydrostatic pressure.