Gas Turbine Combustion Liners

Liner bodies, opening patterns and end connections for specific Frame configurations, reviewed against your component requirements.

Frame 6B LEC III Combustion Liner component example
Frame 6B LEC III Combustion Liner

Match the Liner to Its Drawing

Combustion liners form the inner combustion passage of a gas turbine combustion arrangement. Blaze reviews liner body geometry, openings and end connections against the specified configuration before defining a custom manufacturing project.

A liner inquiry should identify the configuration, body geometry, opening pattern and end connections. The listed DLN and LEC-labelled entries retain their own component definitions. Specify the required arrangement and mating dimensions rather than selecting by a similar photograph.

Frame 5Frame 6BFrame 6FFrame 6FAFrame 6FA.03Frame 7Frame 9EFrame 9F

Combustion Liner Examples

13 component examples
Frame 5 Combustion Liner component example
Frame 5

Frame 5 Combustion Liner

The Frame 5 combustion liner forms the flame-containing section of the MS5001 gas turbine combustor.

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Component Definition

The Frame 5 combustion liner forms the flame-containing section of the MS5001 gas turbine combustor. Its cylindrical body provides a defined combustion space, while openings along the wall admit air into the hot-gas stream. The liner connects the head-end combustion hardware with the downstream gas path.

Project Review

The production review covers the head-end plate, cooling and dilution openings, side ports, seams and outlet retention features. The required MS5001 configuration determines wall geometry, local interface dimensions and the acceptance criteria for the completed liner.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 5 Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 5 DLN Combustion Liner component example
Frame 5

Frame 5 DLN Combustion Liner

The Frame 5 DLN combustion liner is a distinct liner configuration for dry low NOx combustion hardware.

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Component Definition

The Frame 5 DLN combustion liner is a distinct liner configuration for dry low NOx combustion hardware. Its multi-opening head end works with the designated fuel-entry arrangement, while the liner body defines the combustion space and the connection toward the downstream flow path.

Project Review

For this DLN configuration, the multi-opening head end and its relationship with the cap and fuel-entry hardware are central to the manufacturing definition. Blaze reviews the body sections, opening pattern and outlet attachment features as a coordinated component.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 5 DLN Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6B Combustion Liner component example
Frame 6B

Frame 6B Combustion Liner

The Frame 6B combustion liner forms the inner combustion chamber of the MS6001B gas turbine combustion system.

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Component Definition

The Frame 6B combustion liner forms the inner combustion chamber of the MS6001B gas turbine combustion system. The perforated cylindrical wall admits air at defined locations, and the head-end and outlet features establish the liner's connection with adjacent combustion hardware.

Project Review

For custom MS6001B liner work, the engineering review covers the perforated wall, formed body sections, central opening, side-port locations and slotted end features. Wall geometry and connection dimensions are established from the specified configuration before process planning.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6B Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6B DLN Combustion Liner component example
Frame 6B

Frame 6B DLN Combustion Liner

The Frame 6B DLN combustion liner is part of a dry low NOx combustion arrangement in which the liner, cap and fuel-delivery hardware operate as a coordinated assembly.

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Component Definition

The Frame 6B DLN combustion liner is part of a dry low NOx combustion arrangement in which the liner, cap and fuel-delivery hardware operate as a coordinated assembly. Its multi-opening head end accommodates the designated nozzle layout, and its body provides the defined combustion passage.

Project Review

The DLN head-end opening layout, cooling features and outlet interface are reviewed together with the designated cap and nozzle arrangement. This defines the part to be manufactured and separates it from conventional Frame 6B liner configurations.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6B DLN Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6B LEC III Combustion Liner component example
Frame 6B

Frame 6B LEC III Combustion Liner

The Frame 6B LEC III combustion liner defines the inner combustion passage within the designated LEC III assembly.

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Component Definition

The Frame 6B LEC III combustion liner defines the inner combustion passage within the designated LEC III assembly. Its stepped cylindrical profile, local openings and end features connect the combustion zone with the surrounding head-end and downstream hardware.

Project Review

The stepped body, larger wall openings and slotted outlet region are treated as configuration-controlled features. Blaze reviews both connection ends, locating details and the surrounding assembly requirements before defining the liner manufacturing route.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6B LEC III Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6F DLN2.6 Combustion Liner component example
Frame 6F

Frame 6F DLN2.6 Combustion Liner

The Frame 6F DLN2.6 combustion liner forms the inner combustion passage within the designated dry low NOx arrangement.

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Component Definition

The Frame 6F DLN2.6 combustion liner forms the inner combustion passage within the designated dry low NOx arrangement. Its body profile and end features establish the connection between the head-end assembly and the downstream gas path.

Project Review

The engineering review addresses the inlet profile, cylindrical wall sections, local openings and outlet retention features. These details are checked against the required DLN2.6 cap and transition relationships so the liner production definition covers both end connections.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6F DLN2.6 Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6FA Combustion Liner component example
Frame 6FA

Frame 6FA Combustion Liner

The Frame 6FA combustion liner forms the inner wall of the combustion passage within the relevant F-class gas turbine arrangement.

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Component Definition

The Frame 6FA combustion liner forms the inner wall of the combustion passage within the relevant F-class gas turbine arrangement. Its cylindrical body, formed wall sections and local openings establish the combustion space and the interfaces with adjoining hardware.

Project Review

For a 6FA-series liner project, formed wall sections, corrugations, side openings and end connections are reviewed together. The exact engine and combustion revision are identified during engineering review so that family-level appearance is translated into a defined manufacturing requirement.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6FA Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 6FA.03 Combustion Liner component example
Frame 6FA.03

Frame 6FA.03 Combustion Liner

The Frame 6FA.03 combustion liner forms the inner combustion passage within the designated F-class combustion system.

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Component Definition

The Frame 6FA.03 combustion liner forms the inner combustion passage within the designated F-class combustion system. Its cylindrical body, inlet features and formed outlet region establish the component's position between the head-end assembly and downstream transition hardware.

Project Review

The inlet features, changes in wall construction, body openings and formed outlet section are reviewed against the required head-end and transition interfaces. Blaze defines the material, fabrication route and retention-feature controls for the selected 6FA.03 liner configuration.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 6FA.03 Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 7 Combustion Liner component example
Frame 7

Frame 7 Combustion Liner

The Frame 7 combustion liner forms the inner combustion passage and includes configuration-specific head-end features.

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Component Definition

The Frame 7 combustion liner forms the inner combustion passage and includes configuration-specific head-end features. The inlet arrangement, wall openings and body profile establish the relationship between the fuel-entry hardware and the downstream combustion zone.

Project Review

The head-end opening pattern, cooling features, local ports and internal passage profile are important to the production definition. Blaze reviews these details with the required cap and downstream interfaces, distinguishing the selected Frame 7 liner configuration before process planning.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 7 Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 9E Combustion Liner component example
Frame 9E

Frame 9E Combustion Liner

The Frame 9E combustion liner provides the inner combustion passage within the MS9001E gas turbine combustion system.

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Component Definition

The Frame 9E combustion liner provides the inner combustion passage within the MS9001E gas turbine combustion system. Its perforated wall, head-end arrangement and outlet features work together to establish the flame-containing space and admit air at defined locations.

Project Review

For MS9001E liner work, Blaze reviews the head-end plate, central opening, circumferential hole patterns and end connections. The specified part revision establishes the required geometry, material and surface-treatment requirements for the selected component.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 9E Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 9E DLN Combustion Liner component example
Frame 9E

Frame 9E DLN Combustion Liner

The Frame 9E DLN combustion liner belongs to a dry low NOx combustion configuration and incorporates a multi-opening head-end arrangement.

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Component Definition

The Frame 9E DLN combustion liner belongs to a dry low NOx combustion configuration and incorporates a multi-opening head-end arrangement. The liner body and its local openings define the combustion passage and the interfaces with the surrounding assembly.

Project Review

The multi-opening head end, formed wall sections and outlet retention region are reviewed against the designated DLN arrangement. Blaze defines the liner manufacturing requirements together with the mating cap, nozzle layout and downstream connection dimensions.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 9E DLN Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 9E LEC Combustion Liner component example
Frame 9E

Frame 9E LEC Combustion Liner

The Frame 9E LEC combustion liner is a liner configuration associated with the LEC combustion hardware family.

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Component Definition

The Frame 9E LEC combustion liner is a liner configuration associated with the LEC combustion hardware family. Its head-end arrangement and cylindrical body provide the inner combustion passage and the connection features required by the designated system.

Project Review

For the selected LEC configuration, the head-end passages, larger wall ports and circumferential body features define the component geometry. Blaze reviews the specified revision and retention details before establishing a custom liner manufacturing and inspection plan.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

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What information is needed for a Frame 9E LEC Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

Frame 9F DLN Combustion Liner component example
Frame 9F

Frame 9F DLN Combustion Liner

The Frame 9F DLN combustion liner provides the inner combustion passage within the designated dry low NOx system.

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Component Definition

The Frame 9F DLN combustion liner provides the inner combustion passage within the designated dry low NOx system. Its cylindrical body and formed end sections establish the geometry between the head-end hardware and downstream combustion connections.

Project Review

The inlet profile, formed body sections, outlet retention region and specified internal surface requirements are reviewed together. Blaze develops the liner manufacturing definition around the selected 9F DLN revision and its mating head-end and downstream interfaces.

Manufacturing Review

For a custom project, Blaze reviews the component drawing, configuration, material, quantity and acceptance criteria before confirming the manufacturing scope. The production route and inspection plan follow the approved technical definition.

Inquiry Requirements

Send the part drawing and revision, gas turbine configuration, material specification, required quantity and inspection requirements. Include photographs and the mating-interface details when available. If drawings are incomplete, describe the available sample and documentation so Blaze can assess the next review step.

Component Images

Select an image to view the larger version.

What information is needed for a Frame 9F DLN Combustion Liner inquiry?

Provide the part drawing and revision, configuration identifier, material, quantity and inspection requirements. Photographs and mating-interface details help Blaze define the requested scope.

Does the model name confirm that a component will fit?

A model designation identifies the product family. The part number, drawing revision, combustion arrangement and mating dimensions must be checked for the requested component.

What Should a Component Inquiry Include?

The part drawing and installed configuration define the manufacturing review. Provide the information available and identify the requirements that still need clarification.

Information for a combustion component manufacturing review
RequirementWhat to provideWhy it matters
Component definitionPart number, controlled drawing and revisionIdentifies the individual part and requested scope
ConfigurationExact Frame reference, combustion arrangement and assembly interfacesDefines the configuration and mating dimensions to review
Material and quantityMaterial specification, required quantity and processing requirementsDefines the basis of the custom manufacturing inquiry
AcceptanceInspection criteria, required documentation and sample informationDefines the checks and records to confirm during review

Questions About Combustion Liners

What should a combustion liner inquiry identify?

Provide the exact Frame and combustion-arrangement reference, part drawing and revision, body geometry, openings and end connections. Include material, quantity, inspection requirements and the mating-interface information needed to define the requested liner.

Can I select a component using only the Frame model?

The Frame model is a starting point. Identify the part number, drawing revision, combustion arrangement and mating-interface dimensions before confirming a component requirement.

What should a custom manufacturing inquiry include?

Include drawings, material specification, required quantity and inspection requirements. Add the component configuration, photographs and sample availability when relevant.

Discuss Your Component Requirements

Send the drawing and revision, exact configuration, material specification, quantity and inspection requirements. Include the available photographs, sample information and mating-interface details so Blaze can review the requested manufacturing scope.

Discuss Your Requirements

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