Gas Turbine Oxygen Sensor Adaptor Housing Thermal Management

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Solution Overview

Problem

Gas turbine engines face challenges with sensor longevity due to high temperatures and the need for expensive high-temperature alloys, as well as inefficiencies in air consumption and exhaust gas waste.

Innovation Solution

The implementation of an oxygen sensor adaptor housing that maintains the temperature of oxygen sensors below a threshold, allowing for the use of less expensive sensors and optimizing gas turbine operations through stoichiometric combustion and exhaust gas recirculation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If sensors are placed in high-temperature zones of the gas turbine engine, then measurement capability is improved, but sensor longevity deteriorates due to thermal stress and wear

Engineering Contradiction:
Improveoxygen concentration detectionVSAvoidsensor longevity
Core Design Contradiction:
Measurement precisionVSDuration of action of stationary object

Solution Approach 1:

The system divides the sensor environment from the high-temperature combustion zone by introducing a recirculation stream that creates a localized cooler environment around the sensor, protecting it while maintaining measurement capability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A recirculation stream acts as an intermediary between the hot combustion products and the oxygen sensor, transferring some of the hot gas for measurement purposes while maintaining a protective cooler environment around the sensor element

Inventive Principle:
Principle #24Intermediary (Mediator)

2Duration of action of stationary object

If expensive high-temperature alloy sensors are used, then sensor longevity is improved, but system cost increases

Engineering Contradiction:
Improvesensor longevityVSAvoidsystem cost
Core Design Contradiction:
Duration of action of stationary objectVSEase of manufacture

Solution Approach 1:

The invention enables the use of less expensive sensor materials by creating a protected environment that reduces thermal stress, making the sensor more affordable while maintaining adequate longevity through the recirculation cooling mechanism

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

Solution Approach 2:

The local temperature parameter around the sensor is changed from high-temperature combustion conditions to a cooler protected environment through the recirculation stream, allowing standard sensors to operate reliably

Inventive Principle:
Principle #35Parameter changes

3Productivity

If stoichiometric combustion is implemented, then combustion efficiency is improved, but air consumption increases

Engineering Contradiction:
Improvecombustion efficiencyVSAvoidair consumption
Core Design Contradiction:
ProductivityVSQuantity of substance

Solution Approach 1:

The system recovers and recirculates exhaust gases back into the combustion process, reducing the need for fresh air intake while maintaining efficient stoichiometric combustion through controlled recirculation

Inventive Principle:
Principle #34Discarding and recovering

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 solution extends sensor longevity, reduces costs by using less expensive sensors, and enhances gas turbine efficiency by minimizing air consumption and exhaust gas waste through effective combustion and recirculation processes.

Implementation Method 1

The oxygen sensor adaptor housing is configured to maintain a temperature of a portion of the oxygen sensor below an upper threshold

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS9587510B2System and method for a gas turbine engine sensor
Publication Date: 2017.03.07 GE INFRASTRUCTURE TECH LLC
  • US9587510B2 patent drawing
  • US9587510B2 patent drawing
  • US9587510B2 patent drawing

AI summary

A system includes a gas turbine engine that includes a combustor section having a turbine combustor that generates combustion products, a turbine section having one or more turbine stages driven by the combustion products, an exhaust section disposed downstream of the turbine section, an oxygen sensor adaptor housing disposed in at least one of the combustor section, the turbine section, or the exhaust section, or any combination thereof, and an oxygen sensor disposed in the oxygen sensor adaptor housing. The oxygen sensor adaptor housing is configured to maintain a temperature of a portion of the oxygen sensor below an upper threshold.