Gas Turbine Combustion Components

Combustion caps, fuel nozzles and selected system assemblies, reviewed against drawings and exact configuration requirements.

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Frame 6B LEC III Combustion System

Define the Component and Its Configuration

Combustion components bring together head-end hardware, combustion caps, fuel nozzles and selected system assemblies. Blaze reviews the requested component scope against drawings, configuration identifiers and mating interfaces.

A combustion system, cap and fuel nozzle describe different component scopes. Use the exact product title and Frame reference, then identify the drawing revision and the interfaces that connect the requested part to its assembly.

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

Combustion Component Examples

19 component examples

Frame 6B

Frame 6B DLN Combustion System

The Frame 6B DLN combustion system combines fuel-entry hardware, the combustion liner and downstream gas-path connections in a configuration intended for dry low NOx operation.

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Component Definition

The Frame 6B DLN combustion system combines fuel-entry hardware, the combustion liner and downstream gas-path connections in a configuration intended for dry low NOx operation. The designation describes the combustion arrangement; individual component selection depends on the installed version and its interface details.

Project Review

System-related work starts by separating the liner, cap, fuel-entry and transition-interface requirements. Blaze then reviews the requested part scope against the identified DLN configuration, establishing which components and mating dimensions need to be included in the production definition.

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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Frame 6B DLN Combustion System: component detail 1 — Component detail 1

What information is needed for a Frame 6B DLN Combustion System 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.

Discuss Your Component

Frame 6B

Frame 6B DLN Primary Fuel Nozzle

The Frame 6B DLN primary fuel nozzle is a designated fuel-delivery component within the combustor head-end arrangement.

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Component Definition

The Frame 6B DLN primary fuel nozzle is a designated fuel-delivery component within the combustor head-end arrangement. Its nozzle tip, surrounding passages and installed position form part of the primary fuel-entry geometry for the applicable DLN configuration.

Project Review

The primary-nozzle position is identified separately from the surrounding fuel-delivery components. The engineering review covers the tip, fuel-side connections, installed orientation and mounting interfaces, with passage and inspection requirements established for the specified DLN arrangement.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6B DLN Primary Fuel Nozzle: component detail 1 — Component detail 1

What information is needed for a Frame 6B DLN Primary Fuel Nozzle 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.

Discuss Your Component

Frame 6B

Frame 6B LEC III Combustion System

The Frame 6B LEC III combustion system brings the head-end fuel-delivery components, combustion liner and downstream transition hardware into a coordinated assembly.

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Component Definition

The Frame 6B LEC III combustion system brings the head-end fuel-delivery components, combustion liner and downstream transition hardware into a coordinated assembly. The system-level arrangement defines how individual combustion components connect and how the gas path develops from the fuel-entry region toward the turbine.

Project Review

A LEC III project can be defined at individual-component or assembly-interface level. Blaze reviews the requested liner, head-end and downstream connection scope so that the material, production route and dimensional requirements can be established for each selected part.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6B LEC III Combustion System: component detail 1 — Component detail 1

Frame 6B LEC III Combustion System: component detail 2 — Component detail 2

What information is needed for a Frame 6B LEC III Combustion System 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.

Discuss Your Component

Frame 6B

Frame 6B T-DLN Fuel Nozzle

The T-DLN fuel nozzle is a fuel-entry component used within a dry low NOx combustion arrangement.

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Component Definition

The T-DLN fuel nozzle is a fuel-entry component used within a dry low NOx combustion arrangement. Its shaped tip and surrounding passages form part of the local fuel-and-air introduction geometry at the combustor head end.

Project Review

For a Frame 6B T-DLN project, Blaze reviews the specified nozzle position, tip geometry, surrounding passages, fuel connections and mounting features. Manufacturing is defined for the requested configuration using its specified geometry and interface requirements.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6B T-DLN Fuel Nozzle: component detail 1 — Component detail 1

Frame 6B T-DLN Fuel Nozzle: component detail 2 — Component detail 2

What information is needed for a Frame 6B T-DLN Fuel Nozzle 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.

Discuss Your Component

Frame 6F

Frame 6F DLN2.6 Combustion Cap

The Frame 6F DLN2.6 combustion cap establishes the opening arrangement at the head end of the designated combustion liner.

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Component Definition

The Frame 6F DLN2.6 combustion cap establishes the opening arrangement at the head end of the designated combustion liner. Its multi-opening layout provides the interfaces needed for the relevant nozzle configuration, while the outer structure connects with the surrounding combustion hardware.

Project Review

For this cap configuration, the large-passage pattern, outer ring, locating features and mounting profiles govern the manufacturing definition. Blaze reviews the cap together with its designated liner and nozzle interfaces to establish the required alignment and dimensional controls.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6F DLN2.6 Combustion Cap: component detail 1 — Component detail 1

What information is needed for a Frame 6F DLN2.6 Combustion Cap 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.

Discuss Your Component

Frame 6F

Frame 6F DLN2.6 Fuel Nozzle Assembly

The Frame 6F DLN2.6 fuel nozzle assembly groups the designated fuel-entry components in a defined head-end arrangement.

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Component Definition

The Frame 6F DLN2.6 fuel nozzle assembly groups the designated fuel-entry components in a defined head-end arrangement. The nozzle array, mounting structure and connection features establish how the fuel-delivery hardware is positioned relative to the combustion cap and liner.

Project Review

The array layout, axial projection, mounting flange and fuel connections are reviewed as a complete head-end relationship. Blaze defines the requested individual-nozzle or assembly scope, including passage features, joining requirements and the interfaces to be inspected.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6F DLN2.6 Fuel Nozzle Assembly: component detail 1 — Component detail 1

What information is needed for a Frame 6F DLN2.6 Fuel Nozzle Assembly 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.

Discuss Your Component

Frame 6F

Frame 6F FlameSheet Combustion System

The Frame 6F FlameSheet combustion system is a distinct combustion arrangement within the Frame 6F gas turbine family.

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Component Definition

The Frame 6F FlameSheet combustion system is a distinct combustion arrangement within the Frame 6F gas turbine family. The complete assembly brings fuel-entry components, mixing and combustion passages, surrounding supports and downstream connections into a coordinated hardware layout.

Project Review

For hardware associated with a 6F FlameSheet arrangement, Blaze evaluates the customer-defined component scope and connection requirements. The project review establishes which parts are to be manufactured, their material requirements and the interfaces that must match the specified installation.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6F FlameSheet Combustion System: component detail 1 — Component detail 1

Frame 6F FlameSheet Combustion System: component detail 2 — Component detail 2

Frame 6F FlameSheet Combustion System: component detail 3 — Component detail 3

What information is needed for a Frame 6F FlameSheet Combustion System 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.

Discuss Your Component

Frame 6F

Frame 6F LEC III Combustion System

The Frame 6F LEC III combustion system integrates fuel-entry hardware, a defined combustion passage and the surrounding assembly features within the relevant F-class arrangement.

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Component Definition

The Frame 6F LEC III combustion system integrates fuel-entry hardware, a defined combustion passage and the surrounding assembly features within the relevant F-class arrangement. Its system configuration governs how the individual parts connect and how the hot-gas passage is established.

Project Review

For a 6F LEC III scope, the head-end interfaces, liner body, supports and downstream connection are reviewed as an assembly relationship. The manufacturing definition identifies the selected components and their mating geometry for the specified 6F configuration.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6F LEC III Combustion System: component detail 1 — Component detail 1

What information is needed for a Frame 6F LEC III Combustion System 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.

Discuss Your Component

Frame 6FA

Frame 6FA Combustion Cap

The Frame 6FA combustion cap is a head-end component that establishes the arrangement of fuel-entry openings at the combustion liner inlet.

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Component Definition

The Frame 6FA combustion cap is a head-end component that establishes the arrangement of fuel-entry openings at the combustion liner inlet. Its plate geometry, passage layout and surrounding connection features define its relationship with the designated nozzle and liner hardware.

Project Review

The cap review focuses on the head-end passage arrangement, perforated areas, outer profile and liner connection. Blaze establishes the required nozzle-opening dimensions and mounting relationships from the selected 6FA configuration before machining and inspection planning.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6FA Combustion Cap: component detail 1 — Component detail 1

What information is needed for a Frame 6FA Combustion Cap 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.

Discuss Your Component

Frame 6FA.03

Frame 6FA.03 Combustion Cap

The Frame 6FA.03 combustion cap is a head-end component that defines the opening layout at the combustion liner inlet.

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Component Definition

The Frame 6FA.03 combustion cap is a head-end component that defines the opening layout at the combustion liner inlet. Its multiple passages and surrounding structure establish the interface with the designated nozzle arrangement and adjacent liner hardware.

Project Review

The cap project review covers the multi-opening layout, outer ring, locating features and attachment interfaces. Blaze establishes the required passage positions and mating dimensions together with the specified liner and fuel-nozzle arrangement before production planning.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6FA.03 Combustion Cap: component detail 1 — Component detail 1

What information is needed for a Frame 6FA.03 Combustion Cap 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.

Discuss Your Component

Frame 6FA.03

Frame 6FA.03 Combustion System

The Frame 6FA.03 combustion system coordinates fuel introduction, the combustion passage and the downstream transition toward the turbine.

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Component Definition

The Frame 6FA.03 combustion system coordinates fuel introduction, the combustion passage and the downstream transition toward the turbine. Its arrangement defines how head-end components, liner hardware and hot-gas-path connections fit together within the specified engine configuration.

Project Review

A 6FA.03 system-related scope is divided into the specified fuel-entry hardware, cap, liner and transition-interface requirements. Blaze reviews the mating geometry and assembly identifiers so the manufacturing plan is defined for the selected components for the specified installation.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6FA.03 Combustion System: component detail 1 — Component detail 1

What information is needed for a Frame 6FA.03 Combustion System 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.

Discuss Your Component

Frame 6FA.03

Frame 6FA.03 Fuel Nozzle

The Frame 6FA.03 fuel nozzle delivers fuel to the designated combustion arrangement through a configuration-specific nozzle body and discharge section.

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Component Definition

The Frame 6FA.03 fuel nozzle delivers fuel to the designated combustion arrangement through a configuration-specific nozzle body and discharge section. Its axial geometry and mounting features establish the installed relationship with the surrounding head-end components.

Project Review

The axial body sections, mounting profiles, inlet connections and discharge geometry are treated as configuration-controlled features. Blaze reviews the requested individual nozzle or head-end scope, establishing material, machining, joining and inspection requirements from the approved technical definition.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 6FA.03 Fuel Nozzle: component detail 1 — Component detail 1

What information is needed for a Frame 6FA.03 Fuel Nozzle 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.

Discuss Your Component

Frame 7

Frame 7 DLN Combustion System

The Frame 7 DLN combustion system combines the fuel-entry region, combustion liner and downstream transition hardware within a dry low NOx arrangement.

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Component Definition

The Frame 7 DLN combustion system combines the fuel-entry region, combustion liner and downstream transition hardware within a dry low NOx arrangement. The assembly layout establishes how these parts connect and how the combustion passage leads toward the turbine inlet.

Project Review

Frame 7 DLN-related work is defined around the requested engine and combustion revision. Blaze reviews the head-end, liner and downstream interface requirements so that the selected component scope, materials and acceptance criteria can be agreed before manufacturing.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 7 DLN Combustion System: component detail 1 — Component detail 1

What information is needed for a Frame 7 DLN Combustion System 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.

Discuss Your Component

Frame 7

Frame 7 FlameSheet Combustion System

The Frame 7 FlameSheet combustion system brings the head-end hardware, combustion passage and downstream connection features into a distinct integrated arrangement.

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Component Definition

The Frame 7 FlameSheet combustion system brings the head-end hardware, combustion passage and downstream connection features into a distinct integrated arrangement. It is reviewed at the system level because the interfaces between its individual components define the complete assembly.

Project Review

For a Frame 7 FlameSheet-related project, the technical review defines the selected hardware and its relationship with the existing installation. Blaze considers mounting locations, mating surfaces and connection profiles when developing the manufacturing scope for customer-specified components.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 7 FlameSheet Combustion System: component detail 1 — Component detail 1

Frame 7 FlameSheet Combustion System: component detail 2 — Component detail 2

Frame 7 FlameSheet Combustion System: component detail 3 — Component detail 3

What information is needed for a Frame 7 FlameSheet Combustion System 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.

Discuss Your Component

Frame 7

Frame 7 LEC III Combustion System

The Frame 7 LEC III combustion system is a coordinated assembly of head-end fuel-delivery hardware, an inner combustion liner and a downstream transition arrangement.

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Component Definition

The Frame 7 LEC III combustion system is a coordinated assembly of head-end fuel-delivery hardware, an inner combustion liner and a downstream transition arrangement. The complete system defines the relationship between the fuel-entry region and the shaped passage leading toward the turbine.

Project Review

A Frame 7 LEC III scope may cover selected combustion components and their connection features. Blaze reviews the head-end mounting arrangement, liner sections, transition supports and locating interfaces, then establishes the manufacturing requirements for the parts included in the project.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 7 LEC III Combustion System: component detail 1 — Component detail 1

Frame 7 LEC III Combustion System: component detail 2 — Component detail 2

Frame 7 LEC III Combustion System: component detail 3 — Component detail 3

Frame 7 LEC III Combustion System: component detail 4 — Component detail 4

Frame 7 LEC III Combustion System: component detail 5 — Component detail 5

What information is needed for a Frame 7 LEC III Combustion System 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.

Discuss Your Component

Frame 9E

Frame 9E LEC III Combustion System

The Frame 9E LEC III combustion system brings fuel-entry hardware, the combustion liner and downstream transition connections into a defined assembly.

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Component Definition

The Frame 9E LEC III combustion system brings fuel-entry hardware, the combustion liner and downstream transition connections into a defined assembly. The system layout establishes the relationship between individual components and the gas path toward the turbine inlet.

Project Review

A 9E LEC III project starts with the required component list and assembly interfaces. Blaze reviews mounting locations, liner sections, head-end connections and transition relationships to define the material, production route and acceptance requirements for the selected hardware.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 9E LEC III Combustion System: component detail 1 — Component detail 1

What information is needed for a Frame 9E LEC III Combustion System 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.

Discuss Your Component

Frame 9F

Frame 9F Combustion System

The Frame 9F combustion system introduces fuel, establishes the combustion zone and directs the resulting hot-gas flow toward the turbine.

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Component Definition

The Frame 9F combustion system introduces fuel, establishes the combustion zone and directs the resulting hot-gas flow toward the turbine. Its arrangement includes configuration-specific head-end hardware, a combustion passage and downstream connections.

Project Review

For a 9F system-related requirement, Blaze separates the requested liner, sleeve or support hardware, fuel-entry components and transition interfaces. The exact engine and combustion variant determine the component geometry and the assembly relationships covered by the project.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 9F Combustion System: component detail 1 — Component detail 1

Frame 9F Combustion System: component detail 2 — Component detail 2

Frame 9F Combustion System: component detail 3 — Component detail 3

What information is needed for a Frame 9F Combustion System 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.

Discuss Your Component

Frame 9F

Frame 9F FlameSheet Combustion System

The Frame 9F FlameSheet combustion system is a distinct combustion arrangement within the Frame 9F gas turbine family.

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Component Definition

The Frame 9F FlameSheet combustion system is a distinct combustion arrangement within the Frame 9F gas turbine family. Its complete assembly brings fuel-entry hardware, the combustion passage, surrounding support structures and downstream connection features into an integrated layout.

Project Review

For hardware associated with a 9F FlameSheet installation, Blaze reviews the customer-defined parts and their assembly boundaries. Mounting profiles, component connections and surrounding support interfaces are established during technical review before the production scope is confirmed.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 9F FlameSheet Combustion System: component detail 1 — Component detail 1

Frame 9F FlameSheet Combustion System: component detail 2 — Component detail 2

Frame 9F FlameSheet Combustion System: component detail 3 — Component detail 3

What information is needed for a Frame 9F FlameSheet Combustion System 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.

Discuss Your Component

Frame 9F

Frame 9F Fuel Nozzle

The Frame 9F fuel nozzle delivers fuel into the designated combustion arrangement through a configuration-specific internal passage and outlet geometry.

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Component Definition

The Frame 9F fuel nozzle delivers fuel into the designated combustion arrangement through a configuration-specific internal passage and outlet geometry. Its body, inlet connections and discharge end form part of the complete fuel-delivery system.

Project Review

The fuel-nozzle review covers inlet connections, internal passage requirements, body geometry, mounting details and the discharge section. Blaze uses the specified 9F configuration and approved technical definition to establish machining, assembly and project-specific inspection requirements.

Manufacturing Review

Inquiry Requirements

Component Images

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Frame 9F Fuel Nozzle: component detail 1 — Component detail 1

What information is needed for a Frame 9F Fuel Nozzle 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.

Discuss Your 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
Requirement	What to provide	Why it matters
Component definition	Part number, controlled drawing and revision	Identifies the individual part and requested scope
Configuration	Exact Frame reference, combustion arrangement and assembly interfaces	Defines the configuration and mating dimensions to review
Material and quantity	Material specification, required quantity and processing requirements	Defines the basis of the custom manufacturing inquiry
Acceptance	Inspection criteria, required documentation and sample information	Defines the checks and records to confirm during review

Questions About Combustion Components

Which component forms are included in this collection?

The examples include combustion caps, fuel nozzles, fuel-nozzle assemblies and selected combustion systems. Each entry retains its own Frame reference and combustion-arrangement name. Define the individual part scope before requesting a quotation.

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