Torch Igniter Removable Glow Plug for Gas Turbine Maintenance

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Solution Overview

Problem

Torch igniters mounted internally within the high-pressure case of a gas turbine engine face accessibility issues during maintenance due to the high pressure differential, which complicates the replacement and maintenance of glow plugs.

Innovation Solution

A design where the torch igniter is partially or fully situated within the high-pressure case, with a removable glow plug configuration that allows for easy access and replacement through the high-pressure case, minimizing stress on the combustion chamber and utilizing a flange and seal system to secure the glow plug, enabling efficient maintenance without compromising the integrity of the high-pressure case.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the torch igniter is mounted externally to the high pressure case, then the torch igniter can withstand the high pressure differential, but the glow plug becomes inaccessible for maintenance

Engineering Contradiction:
Improvepressure resistanceVSAvoidglow plug accessibility
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

The torch igniter is divided into separate components: the main body is mounted within the high pressure case while the glow plug is positioned to extend through the case wall, allowing independent access to the glow plug for maintenance while keeping the pressure-containing portion inside the sealed environment

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A seal assembly acts as an intermediary component that allows the glow plug to pass through the high pressure case wall while maintaining the pressure differential. The seal enables maintenance access to the glow plug without compromising the pressure resistance of the case

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of repair

If the torch igniter is mounted within the high pressure case, then the glow plug becomes accessible for maintenance, but the combustion chamber experiences increased stress

Engineering Contradiction:
Improveglow plug accessibilityVSAvoidcombustion chamber stress
Core Design Contradiction:
Ease of repairVSStress or pressure

Solution Approach 1:

The glow plug, which requires frequent maintenance, is extracted from the internal combustion chamber environment and positioned to extend through the case wall. This allows the glow plug to be accessed from the external low-pressure side, eliminating the need to open the high pressure case for maintenance while keeping the combustion chamber sealed and stress-free

Inventive Principle:
Principle #2Taking out (Extraction)

3Ease of repair

If the glow plug is made removable for maintenance, then ease of replacement is improved, but the risk of leaks at the connection interface increases

Engineering Contradiction:
Improveglow plug replaceabilityVSAvoidleak risk
Core Design Contradiction:
Ease of repairVSObject-affected harmful factors

Solution Approach 1:

A seal assembly is pre-installed in the glow plug receptacle before the glow plug is inserted. This preliminary sealing action ensures that when the glow plug is removed and reinstalled, the seal is already in place, reducing the risk of leaks during the maintenance process while allowing easy replacement

Inventive Principle:
Principle #10Preliminary action

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 configuration allows for stress reduction on the combustion chamber, improved accessibility for maintenance, and reliable operation by ensuring the glow plug can be easily replaced or refurbished, extending the lifespan of the torch igniter components.

Implementation Method 1

Torch igniters mounted externally to a high pressure case of the gas turbine engine must be able to withstand a high pressure differential to prevent leaks

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Implementation Method 2

Torch igniters provide a flame as an ignition source for a combustor rather than the electric current provided by spark igniters

Methodology Applied
Scientific EffectResistive heating: Joule Heating

Data Source

PatentEP4015907B1Combustor of a gas turbine engine and method of replacing a surface igniter for a torch igniter thereof
Publication Date: 2023.11.22 COLLINS ENGINE NOZZLES INC
  • EP4015907B1 patent drawingFigure 1
  • EP4015907B1 patent drawingFigure 2
  • EP4015907B1 patent drawingFigure 3

AI summary

An embodiment of a combustor for a gas turbine engine includes a combustor case, a combustor liner (124) disposed within the combustor case, a fuel nozzle (127) at an upstream end of the combustor liner (124), a torch igniter (110) at least partially within the combustor case, and a removable surface igniter. The torch igniter (110) includes a combustion chamber, a cap configured to receive a fuel injector, a tip, an annular igniter wall extending from the cap to the tip and defining a radial extent of the combustion chamber, an aperture, a structural wall coaxial with and surrounding the igniter wall, and an outlet passage within the tip which fluidly connects the combustion chamber to the combustor. The torch igniter (110) is configured to receive the removable surface igniter through the aperture. An internal end of the removable surface igniter extends through the aperture into the combustion chamber of the torch igniter (110).