Frame 6 – 1st Stage (16-Cooling Hole) Buckets
Dawopu supplies Frame 6 first stage turbine buckets with 16 cooling holes. Replacement gas turbine components with nickel-based superalloy materials and protective coating options.
| Material | Nickel-Based Superalloy, DS GTD-111 reference |
|---|---|
| Application | Industrial Gas Turbines, Power Generation, First-Stage Turbine Rotor, Hot Gas Path Maintenance |
Compatible Models
Technical Specifications
| Parameter | Specification |
|---|---|
| Product Name | 1st Stage Turbine Bucket |
| Turbine Frame | GE Frame 6 |
| Turbine Stage | 1st Stage |
| Cooling Configuration | 16 Cooling Holes |
| Base Material | Nickel-Based Superalloy |
| Reference Material | DS GTD-111 (configuration dependent) |
| Manufacturing Process | Precision Investment Casting |
| Cooling Design | Internal Air Cooling |
| Surface Protection | Protective Coating, subject to specification |
| Coating Reference | GT-33 IN / Equivalent, subject to verification |
| Installation Position | First-Stage Turbine Rotor |
| Product Type | Gas Turbine Replacement Parts |
| Inspection Requirements | Dimensional, Material and NDT Inspection, as specified |
Note: Final material grade, coating system, cooling-hole geometry, dimensional tolerances and inspection requirements must be confirmed against the applicable OEM part number or approved engineering drawing.
| Material | Nickel-Based Superalloy, DS GTD-111 reference |
|---|---|
| Application | Industrial Gas Turbines, Power Generation, First-Stage Turbine Rotor, Hot Gas Path Maintenance |
Description
Frame 6 – 1st Stage (16-Cooling Hole) Turbine Buckets
The Frame 6 First Stage Turbine Bucket is a critical hot gas path component designed to operate under demanding high-temperature and high-pressure conditions in industrial gas turbines.
Featuring a 16-hole cooling configuration, this bucket is engineered to improve internal air cooling and manage thermal loads during turbine operation. The cooling passages help reduce metal temperatures and thermal stress, contributing to component durability and operational reliability.
The bucket is manufactured using precision investment casting technology and nickel-based superalloy materials. Depending on the specific turbine configuration and engineering requirements, protective coatings can be applied to improve resistance to high-temperature oxidation and hot corrosion.
Dawopu supplies replacement gas turbine buckets and related hot gas path components based on OEM part numbers, technical specifications, drawings, and customer requirements.
Key Features
16-hole cooling configuration
Designed for high-temperature turbine operating conditions
Nickel-based superalloy construction, subject to specification
Precision casting and cooling passage manufacturing
Protective coating options according to operating requirements
Replacement solutions for compatible GE Frame 6 configurations
Supply Capability
New replacement components and manufacturing solutions can be evaluated based on customer drawings, samples, OEM references, and technical requirements.
Frequently Asked Questions
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