Ceramic Matrix Composite Cooling Circuit Fabrication

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Solution Overview

Problem

Traditional fabrication processes for ceramic matrix composite components make it difficult to incorporate internal cooling channels, which are necessary for preventing component degradation in high-temperature environments like gas turbine engines.

Innovation Solution

A method involving wrapping multiple mandrels with fiber sheets, forming holes in the sheets using mandrel openings, and aligning these holes to create fluidly connected cavities within the composite component, followed by matrix formation and mandrel removal to create elongate cavities for cooling airflow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If traditional fabrication processes are used for ceramic matrix composite components, then the manufacturing process is simple, but it is difficult to incorporate internal cooling channels

Engineering Contradiction:
Improvemanufacturing process simplicityVSAvoidability to incorporate internal cooling channels
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The patent applies preliminary action by forming holes in the fiber sheets during the preform fabrication stage, before matrix infiltration. Mandrels with openings are used to create holes in each fiber sheet that will become the cooling channels after assembly. This preliminary formation of cooling channel structures eliminates the need for post-fabrication drilling or machining, which would be difficult in dense ceramic composites.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent segments the cooling channel formation process into discrete steps: forming holes in individual fiber sheets using mandrels, then assembling multiple sheets with aligned holes. This segmentation allows each sheet to be prepared independently with precise hole placement, and the holes are then fluidly connected through proper alignment during assembly, creating the complete internal cooling circuit.

Inventive Principle:
Principle #1Segmentation

2Temperature

If internal cooling channels are added to ceramic matrix composite components, then thermal management is improved, but the manufacturing complexity increases

Engineering Contradiction:
Improvethermal management capabilityVSAvoidmanufacturing process complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent merges the cooling channel formation process with the composite fabrication process itself. The same mandrels and fiber sheet handling used to create the composite structure are also used to form the cooling channels. The holes are created in the fiber sheets during assembly, and the matrix infiltration process simultaneously binds the fibers and preserves the hollow channels, combining two functions into one integrated process.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent uses mandrels with openings as intermediaries to transfer the cooling channel geometry from the tooling to the final component. The mandrels are temporarily introduced during fabrication, their openings define the hole positions and shapes in the fiber sheets, and the mandrels are later removed to leave the desired cooling channels. This intermediary approach simplifies the overall process compared to direct drilling or machining.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Adaptability or versatility

If holes are formed in fiber sheets during preform fabrication, then cooling channels are created, but additional process steps are required

Engineering Contradiction:
Improvecooling channel creationVSAvoidfabrication cycle time
Core Design Contradiction:
Adaptability or versatilityVSProductivity

Solution Approach 1:

The patent performs hole formation in the fiber sheets during the preform fabrication stage, which is a necessary step anyway to assemble the composite structure. By combining cooling channel formation with preform assembly, the patent avoids adding separate post-fabrication steps for channel creation. The holes are formed while the structure is still being built, making the most of the existing process sequence.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent combines multiple operations into the preform fabrication step: fiber sheet placement, hole formation using mandrels, alignment of holes between sheets, and matrix infiltration all occur in an integrated sequence. This merging eliminates the need for separate drilling, machining, or channel formation steps that would extend the fabrication cycle, maintaining productivity while adding cooling functionality.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP4098417B1Method of forming a ceramic matrix composite component having an internal cooling circuit
Publication Date: 2024.10.23 RTX CORP
  • EP4098417B1 patent drawingFigure 1
  • EP4098417B1 patent drawingFigure 2
  • EP4098417B1 patent drawingFigure 3~4

AI summary

A method of forming a ceramic matrix composite (CMC) component having an internal cooling circuit includes wrapping at least a first sheet (22; 122) around a first mandrel (20; 120), wrapping at least a second sheet (22; 122) around a second mandrel (20; 120), creating a first plurality of holes (26; 126) in the first sheet (22; 122) corresponding to a plurality of openings (24; 124) in the first mandrel (20; 120), creating a second plurality of holes (26; 126) in the second sheet (22; 122) corresponding to a plurality of openings (24; 124) in the second mandrel (20; 120), aligning the first mandrel (20; 120) and the second mandrel (20; 120) such that the first plurality of holes (26; 126) face and are aligned with the second plurality of holes (26; 126), wrapping at least a third sheet (22; 122) around both the first mandrel (20; 120) and second mandrel (20; 120) to form a preform (28; 128), the preform (28; 128) comprising each of the first sheet (22; 122), the second sheet (22; 122), and the third sheet (22; 122), and densifying the preform (28; 128). The first sheet (22; 122), second sheet (22; 122), and third sheet (22; 122) are formed from a ceramic fiber material.