Prime Mover (Engine/Turbine)
View system integration details
This page explains how Combustion Chamber (for gas turbines) is classified within Machinery and Equipment Manufacturing. Technical values and manufacturer relationships are research references; confirm the current specification and supplier evidence for each order.
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)
| Parameter | Typical range | Notes & selection driver |
|---|---|---|
| Inlet Temperature | 300–600 °C | Higher improves efficiency but requires advanced materials |
| Exhaust Temperature | 800–1200 °C | Affects downstream turbine blade cooling |
| Fuel Flow Rate | 0.5–5.0 kg/s | Depends on turbine power rating |
| Air-Fuel Ratio | 40–60 | Leaner reduces NOx but may cause flame instability |
| Combustion Efficiency | 99.0–99.9 % | High efficiency minimizes unburned fuel |
| Pressure Drop | 2–5 % | Lower drop improves overall cycle efficiency |
| Material Grade | Inconel 718 | High-temperature strength and oxidation resistanceASTM B637 |
| Wall Thickness | 2–5 mm | Thinner reduces weight but may affect durability |
| Weight | 50–200 kg | Depends on turbine size and material |
| Service Life | 20000–50000 h | Influenced by thermal cycling and maintenance |
Ranges are indicative industry figures for RFQ preparation, not a supplier commitment. Confirm every value and standard with the legal manufacturer before ordering.
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) |
Indicative industry ranges for design and RFQ preparation. Confirm the exact figures and applicable standard with the manufacturer before specifying.
Quoted from the published standard.
Manufacturer profiles associated with Combustion Chamber (for gas turbines).
Manufacturer listings support early research and capability understanding. They are not certification, ranking, or transaction guarantees.
A practical evidence checklist for RFQ preparation and supplier evaluation.
CNFX does not score or rank suppliers. Buyers must verify all claims and documents with the legal manufacturer before ordering.
According to directory reference data, the operating pressure is typically 1.0–1.6 MPa. However, the exact value depends on the specific turbine model and application. Always verify with the manufacturer.
Common materials include nickel-based superalloys, cobalt-based superalloys, ceramic matrix composites (CMCs), and heat-resistant steels. A specific grade listed is Inconel 718, conforming to ASTM B637. Confirm material suitability for your operating conditions.
The service life is typically 20,000–50,000 hours, influenced by thermal cycling and maintenance practices. Actual life depends on operating conditions and maintenance schedule. Consult the manufacturer for specific recommendations.
The air-fuel ratio is typically maintained between 40–60. Leaner mixtures reduce NOx emissions but may cause flame instability. The optimal ratio balances efficiency, emissions, and stability. Verify the design ratio for your application.
Editorial classification, named public sources where available, and source-reviewed manufacturer records.
Ask for use case, specification boundaries, supplier type, and RFQ preparation information for this product.
Compare manufacturer profiles with relevant product and process capability.