Dome Deflector Cavity Airflow Swirl Patterns
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Solution Overview
Problem
In gas turbine engines, particulate build-up in the dome-deflector cavity reduces the efficiency of impingement and film cooling, leading to increased maintenance frequency due to restricted airflow and reduced cooling efficiency.
Innovation Solution
The dome structure incorporates multiple groups of dome-side cooling airflow passages arranged in different swirl directions, enhancing airflow circulation and turbulence within the dome-deflector cavity to mitigate particulate accumulation and maintain cooling efficiency.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Device complexity
If a single swirl direction is used in cooling airflow passages, then the structure is simpler, but particulate build-up occurs in the cavity
Solution Approach 1:
The cooling airflow passages are segmented into multiple groups, with each group oriented to provide airflow in a different swirl direction. This segmentation allows the system to handle particulate matter more effectively by preventing accumulation through varied flow patterns, while maintaining manageable structural complexity through organized grouping.
Solution Approach 2:
Different regions of the dome structure receive cooling airflow with different swirl directions tailored to their specific needs. This local differentiation optimizes particulate removal in each cavity region while maintaining overall system efficiency, rather than applying a uniform swirl direction throughout.
2Reliability
If cooling airflow passages are added to prevent particulate build-up, then cooling efficiency is maintained, but device complexity increases
Solution Approach 1:
The cooling airflow passages are divided into multiple groups with different swirl directions, allowing the system to maintain cooling efficiency through varied flow patterns that prevent particulate accumulation, while keeping the structural complexity manageable through organized segmentation.
Solution Approach 2:
The multi-directional swirl airflow passages serve multiple functions simultaneously: they provide cooling to the dome structure, prevent particulate build-up through varied flow patterns, and maintain airflow circulation. This multi-functionality justifies the increased complexity by delivering multiple benefits from a single structural arrangement.
3Temperature
If impingement cooling is provided to the deflector, then protection from heat is improved, but particulate accumulation restricts airflow and reduces cooling efficiency over time
Solution Approach 1:
Instead of using a single swirl direction that allows particulates to accumulate in predictable patterns, the invention uses multiple swirl directions that invert the expected accumulation patterns, preventing build-up by varying the airflow paths in opposite and different directions across different passage groups.
Solution Approach 2:
The multi-directional swirl airflow passages ensure continuous and effective cooling of the deflector by maintaining uninterrupted airflow circulation. The varied swirl directions prevent particulate accumulation that would otherwise restrict airflow over time, ensuring the cooling action remains continuous and effective throughout the component's operational life.
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
This arrangement reduces dust and dirt build-up, maintains airflow, and extends the life of the deflector by ensuring consistent cooling efficiency and reduced maintenance needs.
Implementation Method 1
each group of dome-side cooling airflow passages being arranged to provide a flow of air therethrough in a respective group swirl direction
Implementation Method 2
enhancing airflow circulation and turbulence within the dome-deflector cavity
Implementation Method 3
The dome structure may include a cavity between the dome and the deflector to provide impingement cooling to the deflector
Data Source
AI summary
A dome-deflector structure for a combustor of a gas turbine includes a dome portion and a deflector portion, the dome portion and the deflector portion being connected together to form a dome-deflector cavity therebetween. The dome portion includes a plurality of dome-side cooling airflow passages therethrough arranged in a plurality of groups of dome-side cooling airflow passages, each group of dome-side cooling airflow passages being arranged to provide a flow of air therethrough in a respective group swirl direction, and adjacent groups of the dome-side cooling airflow passages providing the flow of air in a different group swirl direction with respect to one another.


