Composite Turbine Engine Component With Edge Cover Reinforcement

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Solution Overview

Problem

Turbine engine components, particularly those made of composite materials, face challenges in withstanding mechanical stresses and external forces during operation, which can lead to damage without adequate reinforcement.

Innovation Solution

A composite structure is reinforced with a cover structure, which includes a main body and an extension that fits within a channel of the composite structure, providing additional strength and protection against operational forces.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If composite materials are used for turbine engine components, then weight is reduced and manufacturing flexibility is improved, but strength and resistance to mechanical stresses are insufficient

Engineering Contradiction:
ImproveweightVSAvoidstrength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The invention uses a hybrid composite structure combining composite material sections with metal reinforcement sections. The composite sections (e.g., carbon fiber reinforced polymer) provide weight reduction and manufacturing flexibility, while the metal sections (e.g., titanium or aluminum alloy) provide the necessary strength and mechanical stress resistance. This composite-of-composites approach resolves the contradiction by integrating materials with complementary properties.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The invention applies different material properties to different sections of the same component. Critical areas subject to high mechanical stresses (such as blade roots, attachment points, or high-load zones) are reinforced with metal sections, while non-critical areas use lightweight composite materials. This local differentiation optimizes the overall structure by providing strength where needed and weight reduction where possible.

Inventive Principle:
Principle #3Local quality

2Ease of manufacture

If composite materials are used for turbine engine components, then manufacturing flexibility is improved, but reliability under operational forces is reduced

Engineering Contradiction:
Improvemanufacturing flexibilityVSAvoidreliability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The hybrid composite structure combines the manufacturing advantages of composite materials with the proven reliability of metal sections. The composite portions can be manufactured using advanced composite techniques (autoclave curing, resin transfer molding) for complex geometries, while metal sections provide reliable mechanical performance in critical areas. This integration maintains manufacturing flexibility while ensuring operational reliability.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

By applying metal reinforcement locally to critical areas, the invention ensures high reliability where mechanical stresses are most severe, while maintaining manufacturing flexibility in non-critical areas using composite materials. The metal sections are strategically placed at attachment points, blade roots, or high-load zones where reliability is paramount.

Inventive Principle:
Principle #3Local quality

3Strength

If reinforcement is added to composite turbine components, then strength is improved, but device complexity increases

Engineering Contradiction:
ImprovestrengthVSAvoidstructural complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The reinforcement is applied locally only where mechanically necessary, rather than uniformly throughout the entire component. This means metal sections are strategically positioned at critical stress points (blade roots, attachment areas, high-load zones) while the remainder of the component uses simpler composite construction. This local approach increases strength where needed without proportionally increasing overall complexity.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The component is divided into distinct sections: composite material sections for general structure and metal reinforcement sections for critical areas. This segmentation allows each section to be optimized independently and facilitates modular manufacturing and assembly, reducing the overall complexity of producing and maintaining the hybrid structure.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS20250341166A1Engine component
Publication Date: 2025.11.06 GENERAL ELECTRIC CO
  • US20250341166A1 patent drawing
  • US20250341166A1 patent drawing
  • US20250341166A1 patent drawing

AI summary

An engine component for a turbine engine. The engine component has a composite structure and a cover structure. The composite structure has a composite structure outer wall, a composite structure edge, and a channel. The channel is provided along the composite structure edge. The cover encases at least a portion of the composite structure outer wall. The cover has a main body and an extension.