Gas Turbine Combustor Base Plate Purging Air Flow Passage

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Solution Overview

Problem

Combustors in gas turbines face challenges in extending service life due to high-temperature environments and vortex formation, leading to thermal damage and reduced operational efficiency.

Innovation Solution

A combustor design featuring a nozzle with a rod-like portion, a tubular burner case, and a base plate with a purging air flow passage that injects air into the burner case, reducing vortex formation and combustible gas concentration near the downstream end, thereby suppressing combustion and thermal damage.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If fuel is burnt in the combustor, then energy is produced, but thermal damage occurs to components reducing service life

Engineering Contradiction:
Improveenergy productionVSAvoidservice life
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The combustor is divided into distinct functional zones: a combustion zone for energy production and a purging air space for thermal protection. The base plate segments these zones, creating a physical barrier that separates high-temperature combustion gases from sensitive downstream components, thereby maintaining service life while preserving power generation capability

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Purging air acts as an intermediary substance between the combustion zone and downstream components. This cool air flows through the purging air space and exits via outflow openings, forming a protective gas layer that mediates thermal interaction and prevents direct thermal damage to components while allowing combustion to proceed

Inventive Principle:
Principle #24Intermediary (Mediator)

2Productivity

If vortexes form in combustible gas at the downstream end, then combustion efficiency decreases, but thermal damage increases

Engineering Contradiction:
Improvecombustion efficiencyVSAvoidthermal damage
Core Design Contradiction:
ProductivityVSObject-affected harmful factors

Solution Approach 1:

Purging air is introduced in advance into the purging air space before combustible gas reaches the downstream end of the burner case. This preliminary action creates a protective atmosphere that prevents vortex formation and subsequent thermal damage to downstream components, while maintaining combustion efficiency through proper airflow management

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The purging air space creates an inert-like protective environment downstream of the combustion zone. By filling this space with cool purging air that exits through outflow openings, the system establishes a protective gas atmosphere that suppresses harmful thermal effects and prevents unintended combustion of drifting combustible gases

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

3Reliability

If the purging air space is enlarged, then thermal protection improves, but device complexity increases

Engineering Contradiction:
Improvethermal protectionVSAvoidstructural complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The base plate serves multiple functions simultaneously: it structurally supports the combustor assembly, defines the purging air space geometry, and provides mounting surfaces for outflow openings. This multi-functionality achieves effective thermal protection through a unified component rather than requiring separate protective structures, thereby limiting complexity increase

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

Solution Approach 2:

The purging air space utilizes the radial dimension by spreading the base plate in the radial direction from the burner case axis. This dimensional approach creates an effective thermal protection zone without significantly increasing axial or circumferential complexity, allowing the system to achieve reliability improvement through spatial optimization

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 design increases the service life of combustor components by minimizing vortex formation and thermal damage, ensuring efficient operation and prolonged durability.

Implementation Method 1

the combustible content of the combustible gas is diluted with the purging air

Methodology Applied
Scientific EffectMixing:

Implementation Method 2

a nozzle having a rod-like portion centered on a burner axis and configured to inject fuel

Methodology Applied
Scientific EffectFluid injection: Jet

Implementation Method 3

a burner case configured to form a tubular shape, to surround an outer circumference of the nozzle, and to inject air and the fuel from the nozzle

Methodology Applied
Scientific EffectFluid injection: Jet

Data Source

PatentUS10190775B2Combustor and gas turbine having the same
Publication Date: 2019.01.29 MITSUBISHI POWER LTD
  • US10190775B2 patent drawing
  • US10190775B2 patent drawing
  • US10190775B2 patent drawing

AI summary

A combustor is equipped with a burner case, and a base plate spreading from a downstream end of the burner case in a radial direction. The base plate defines a purging air space at an upstream side of the base plate. The combustor includes a purging air flow passage configured to inject purging air in the purging air space to a downstream side relative to the base plate. An outflow opening of the purging air flow passage is defined within at least one of a radial range from an inner circumferential surface of the burner case and an axial range from the downstream end of the burner case.