Prime Mover (Engine/Turbine)
View system integration details
Based on aggregated insights from multiple verified factory profiles within the CNFX directory, the standard Combustion Chamber (for gas turbines) used in the Machinery and Equipment Manufacturing sector typically supports operational capacities ranging from standard industrial configurations to heavy-duty production requirements.
A canonical Combustion Chamber (for gas turbines) is characterized by the integration of Liner and Fuel Nozzle. In industrial production environments, manufacturers listed on CNFX commonly emphasize Nickel-based superalloys construction to support stable, high-cycle operation across diverse manufacturing scenarios.
A high-temperature component in gas turbines where fuel is mixed with compressed air and ignited to produce hot gases that drive the turbine.
Technical details and manufacturing context for Combustion Chamber (for gas turbines)
Commonly used trade names and technical identifiers for Combustion Chamber (for gas turbines).
This component is essential for the following industrial systems and equipment:
| pressure: | 10 to 30 bar (typical compressor discharge pressure range) |
| flow rate: | 50 to 500 kg/s (air mass flow rate, depending on turbine size) |
| temperature: | 800°C to 1600°C (typical operating range, with peak flame temperatures up to 2000°C) |
| fuel air ratio: | 0.01 to 0.03 (stoichiometric ratio for natural gas combustion) |
Verified manufacturers with capability to produce this product in China
✓ 98% Supplier Capability Match Found
Authentic performance reports from verified B2B procurement managers.
"Reliable performance in harsh Machinery and Equipment Manufacturing environments. No issues with the Combustion Chamber (for gas turbines) so far."
"Testing the Combustion Chamber (for gas turbines) now; the technical reliability results are within 1% of the laboratory datasheet."
"Impressive build quality. Especially the technical reliability is very stable during long-term operation."
“Feedback is collected from verified sourcing managers during RFQ (Request for Quote) and factory evaluation processes on CNFX. These reports represent historical performance data and technical audit summaries from our B2B manufacturing network.”
Nickel-based and cobalt-based superalloys are standard for temperatures up to 1,200°C, while ceramic matrix composites (CMCs) offer superior performance above 1,300°C with better heat resistance and lower weight.
Inspection intervals depend on operating hours and fuel type, but typically liners and nozzles require checking every 8,000-24,000 hours. CMCs may extend service life compared to metallic alloys.
Key factors include fuel-air mixing uniformity (via swirlers/nozzles), liner cooling design, material thermal capabilities, and minimizing pressure drops while maintaining stable ignition across operating ranges.
CNFX is an open directory, not a transaction platform. Each factory profile provides direct contact information and production details to help you initiate direct inquiries with Chinese suppliers.
Request technical pricing, lead times, or customized specifications for Combustion Chamber (for gas turbines) directly from verified manufacturing units.
Connect with verified factories specializing in this product category