Integrated Dome-Deflector Member Combating Thermal Breakdown

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Solution Overview

Problem

Conventional metallic deflectors in gas turbine engines break down due to high heat exposure, requiring costly and time-consuming replacements.

Innovation Solution

A dome structure with a frame and integrated dome-deflector members, featuring cooling passages and a buffer material layer, which can be easily replaced and constructed from durable materials like ceramic matrix composites.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If separate metallic deflectors are used to protect the dome structure from heat, then protection from thermal breakdown is improved, but the deflector breaks down due to high heat exposure requiring costly and time-consuming replacements

Engineering Contradiction:
Improveprotection from thermal breakdownVSAvoidservice life of deflector
Core Design Contradiction:
ReliabilityVSDuration of action of stationary object

Solution Approach 1:

The deflector is integrated with the dome structure and constructed from ceramic matrix composite (CMC) materials, which provide superior thermal resistance and durability compared to conventional metallic deflectors. The CMC material allows the deflector to withstand high heat exposure without breakdown, eliminating the need for frequent replacements while maintaining protective function.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The deflector and dome structure are combined into a single integrated unit rather than separate components. This integration simplifies the overall structure, reduces the number of parts requiring maintenance, and allows the durable CMC material to protect the entire dome-deflector assembly as one unit.

Inventive Principle:
Principle #5Merging (Combining)

2Object-affected harmful factors

If separate metallic deflectors are used, then protection from heat is provided, but replacement is costly and time-consuming

Engineering Contradiction:
Improveheat protectionVSAvoidreplacement time
Core Design Contradiction:
Object-affected harmful factorsVSLoss of time

Solution Approach 1:

The use of ceramic matrix composite materials in the integrated dome-deflector structure provides superior heat resistance, allowing the component to withstand combustion chamber temperatures without degradation. This durability eliminates frequent replacements, thereby reducing maintenance time and operational downtime.

Inventive Principle:
Principle #40Composite materials

3Reliability

If separate metallic deflectors with high temperature coating are used, then added protection from thermal breakdown is provided, but the structure requires multiple separate components increasing complexity

Engineering Contradiction:
Improvethermal protectionVSAvoidnumber of separate components
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The deflector and dome structure are merged into a single integrated component, reducing the number of separate parts from two (dome + deflector) to one. This integration simplifies assembly, inspection, and maintenance procedures while the CMC material provides inherent thermal protection without requiring additional high-temperature coatings.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The integrated dome-deflector member performs multiple functions simultaneously: it provides structural support as a dome, offers thermal protection as a deflector, and resists thermal breakdown through CMC material properties. This multi-functionality eliminates the need for separate protective coatings and reduces overall system complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 extends the lifespan of the dome-deflector structure, reducing replacement frequency and maintenance costs while maintaining performance under high heat conditions.

Implementation Method 1

Cooling passages are provided through the dome wall and the deflector wall so as to provide a flow of cooling air from the pressure plenum into the cavity and, then, from the cavity to a combustion chamber side of the deflector wall

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Data Source

PatentUS11761631B2Integral dome-deflector member for a dome of a combustor
Publication Date: 2023.09.19 GENERAL ELECTRIC CO
  • US11761631B2 patent drawing
  • US11761631B2 patent drawing
  • US11761631B2 patent drawing

AI summary

A dome structure for a combustor of a gas turbine includes a frame structure extending circumferentially about a combustor centerline axis, and a plurality of integrated dome-deflector plate members mounted to the frame structure. Each of the plurality of integrated dome-deflector plate members includes a dome wall, a deflector wall, and a plurality of side walls connecting the dome wall and the deflector wall to each other. A cavity is defined by the dome wall, the deflector wall, and the plurality of side walls.