Pre-nozzle Mixing Cap Assembly for Gas Turbine Combustors

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Solution Overview

Problem

Gas turbine engine combustors face challenges in reducing NOx emissions while maintaining operational efficiency, as existing designs like Dry Low NOx combustors are prone to flame holding, flashback, and auto-ignition, especially with highly reactive fuels, due to irregular fuel and air flow mixing and recirculation zones.

Innovation Solution

A pre-nozzle mixing cap assembly is introduced, featuring a fuel plenum and air tubes with fuel holes for mixing air and fuel upstream of the fuel nozzles, providing faster mixing and reduced flame holding risks, along with a cooling flow to enhance durability and reduce air requirements for cooling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-generated harmful factors

If fuel and air are premixed upstream of fuel nozzles to reduce NOx emissions, then NOx emissions are reduced, but flame holding and flashback risks increase due to irregular flow mixing and recirculation zones

Engineering Contradiction:
ImproveNOx emissionsVSAvoidflame holding risk
Core Design Contradiction:
Object-generated harmful factorsVSReliability

Solution Approach 1:

The mixing cap is segmented into multiple tubes, each containing multiple fuel holes. This segmentation creates numerous small mixing zones rather than a single large mixing zone, improving flow distribution and reducing recirculation areas where flame holding could occur. The fuel is injected through multiple discrete holes in each tube, creating distributed fuel-air mixing throughout the cap structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the mixing cap provide different functions: some tubes are positioned to optimize fuel-air mixing in specific zones, while the overall cap structure provides cooling airflow paths. The fuel holes are strategically positioned on tubes at different locations to create locally optimized mixing patterns that prevent flame holding while maintaining low NOx emissions.

Inventive Principle:
Principle #3Local quality

2Stability of the object's composition

If fuel injection is performed upstream of head-end to improve mixing, then mixing is enhanced, but flow disturbances create recirculation zones that lead to stable pockets of ignitable fuel-air mixtures

Engineering Contradiction:
Improvefuel-air mixing qualityVSAvoidflow disturbance patterns
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

Fuel is injected and mixed with air upstream of the head-end through the mixing cap structure. This preliminary mixing action occurs before the flow reaches the combustion zone, ensuring thorough fuel-air distribution. The mixing cap with its multiple tubes and fuel holes creates controlled mixing patterns that prevent later recirculation and flame holding issues.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If more air is used for cooling the combustor, then cooling effectiveness is improved, but air consumption increases

Engineering Contradiction:
Improvecombustor durabilityVSAvoidair consumption
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The mixing cap structure serves multiple functions simultaneously: it provides fuel-air mixing through the tubes and fuel holes, and it provides cooling airflow paths through its structure. The same cap that performs fuel injection also channels cooling air to the liner, eliminating the need for separate cooling components and optimizing air utilization.

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 achieves improved fuel-air mixing, lower flame holding risks, and increased combustor durability by reducing residence time and accommodating higher reactivity fuels, while meeting emission targets and minimizing combustion dynamics impacts.

Implementation Method 1

Each of the tubes may include a number of fuel holes therein such that the flow of fuel in the fuel plenum passes through the fuel holes and mixes with the flow of air

Methodology Applied
Scientific EffectMixing:

Implementation Method 2

having a cooling flow of air extending therethrough

Methodology Applied
Scientific EffectCooling: Cooling

Data Source

PatentUS9068750B2Combustor with a pre-nozzle mixing cap assembly
Publication Date: 2015.06.30 GE INFRASTRUCTURE TECH LLC
  • US9068750B2 patent drawing
  • US9068750B2 patent drawing
  • US9068750B2 patent drawing

AI summary

The present application and the resulting patent provide a pre-nozzle mixing cap assembly positioned about a cap member of a combustor for mixing a flow of air and a flow of fuel. The pre-nozzle mixing cap assembly may include a fuel plenum in communication with the flow of fuel and a number of tubes in communication with the flow of air and extending through the fuel plenum. Each of the tubes may include a number of fuel holes therein such that the flow of fuel in the fuel plenum passes through the fuel holes and mixes with the flow of air.