Gas Turbine Heat Shield Particulate Mitigation Device

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Solution Overview

Problem

Particulates in the cooling air of gas turbine engine components, such as dust, ice, ash, and dirt, accumulate on heat shields, reducing their cooling efficiency and durability due to excess temperatures and thermal stresses.

Innovation Solution

A particulate mitigation device is integrated into the gas turbine engine components, featuring a tubular body or fairing with a fluid passageway that directs airflow above the boundary layer to reduce particulate ingestion, thereby maintaining cooling efficiency and extending the lifespan of heat shields.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If cooling air is directed through cooling channels to cool heat shields, then cooling efficiency is improved, but particulate accumulation on the heat shield surface increases

Engineering Contradiction:
Improveheat shield temperatureVSAvoidparticulate accumulation
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

A particulate mitigation device is introduced as an intermediary component between the cooling air source and the heat shield surface. This device modifies the cooling airflow to reduce particulate accumulation while maintaining cooling effectiveness, acting as a mediator that resolves the conflict between cooling and contamination.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The invention changes parameters of the cooling airflow, specifically directing it above the boundary layer to reduce particulate ingestion. By modifying flow parameters (velocity, direction, position relative to surface), the system achieves both cooling and particulate mitigation.

Inventive Principle:
Principle #35Parameter changes

2Strength

If cooling structures are designed to protect against high heat loads, then thermal protection is improved, but the structures become more complex

Engineering Contradiction:
Improvethermal resistanceVSAvoidcooling structure complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The cooling system is segmented into distinct functional zones: cooling channels within the heat shield structure, boundary layer regions, and particulate mitigation devices. This segmentation allows each component to be optimized independently for its specific function while contributing to overall thermal protection.

Inventive Principle:
Principle #1Segmentation

3Temperature

If cooling airflow is directed closer to the heat shield surface, then cooling efficiency is improved, but particulate ingestion increases

Engineering Contradiction:
Improvecooling effectivenessVSAvoidparticulate ingestion
Core Design Contradiction:
TemperatureVSQuantity of substance

Solution Approach 1:

The invention addresses the trade-off by utilizing the vertical dimension above the heat shield surface. By directing cooling airflow above the boundary layer rather than directly at the surface, the system accesses an additional spatial dimension that provides both cooling effectiveness and particulate mitigation.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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 effectively captures airflow above the boundary layer, reducing particulate accumulation on heat shields and enhancing cooling efficiency by directing airflow closer to the heat shield surface, thus minimizing thermal stress and maintaining the durability of engine components.

Implementation Method 1

a cooling channel therebetween in fluid communication with the cooling hole for cooling the second surface of the second component

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

the first selected distance is greater than or equal to a boundary layer of the second surface

Methodology Applied
Scientific EffectBoundary layer: Boundary Layer

Data Source

PatentUS10995635B2Apparatus and method for mitigating particulate accumulation on a component of a gas turbine engine
Publication Date: 2021.05.04 RTX CORP
  • US10995635B2 patent drawing
  • US10995635B2 patent drawing
  • US10995635B2 patent drawing

AI summary

A gas turbine engine component assembly is provided. The gas turbine engine comprises: a first component having a first surface and a second surface opposite the first surface; a second component having a first surface and a second surface, the first surface of the first component and the second surface of the second component defining cooling channel therebetween in fluid communication with the cooling hole for cooling the second surface of the second component; and a particulate mitigation device extending from the first surface of the second component a selected distance wherein the particulate mitigation device has an opening therethrough in fluid connection with the cooling channel, and wherein the selected distance is selected to reduce the amount of particulate entering the cooling channel.