Gas Turbine Combustion Chamber Refractory Lining
High-alumina alumina-mullite ceramic heat-shield bricks designed to protect gas turbine combustion chamber metal bodies from severe heat, abrasion, chemical exposure and repeated thermal cycling.
Thermal Protection for the Metallic Chamber Body
Gas turbine combustion chambers operate under intense thermal loading. Temperatures in the range of approximately 1200–1300°C can seriously damage the metallic chamber body if the hot face is not protected by a suitable refractory lining.
Shaped ceramic bricks are installed as an inner heat-shield layer. Their function is to reduce direct heat transfer to the metal, maintain lining integrity under repeated start-and-stop cycles and resist abrasion caused by high-velocity combustion gases.
Key Demands on Combustion Chamber Refractories
The refractory lining must maintain its protective function despite simultaneous thermal, mechanical and chemical stresses.
High-Alumina Alumina-Mullite Ceramic Bricks
The shaped ceramic bricks are used as replaceable heat-shield elements along the inner surface of the combustion chamber.
Alumina-Mullite Brick
A high-alumina refractory brick intended for ceramic heat-shield service in gas turbine combustion chambers. The product is supplied in shaped segments matching the geometry of the chamber lining.
Product Classification and Function
| Item | Classification | Primary Function | Main Service Requirements |
|---|---|---|---|
| Reference Grade | MEHR.ALUM.90A | Identifies the referenced alumina-mullite refractory quality. | Final compatibility must be confirmed against the turbine model and technical drawings. |
| Material Type | High-Alumina Alumina-Mullite Brick | Forms the replaceable ceramic lining inside the combustion chamber. | Thermal shock, abrasion and chemical stability. |
| Application | Ceramic Heat-Shield Segment | Protects the metallic chamber body from direct exposure to high-temperature gases. | Accurate shape, secure installation and stable performance under cyclic operation. |
Typical Areas of Use
Combustion Chamber Inner Lining
Ceramic brick segments forming the protective inner layer between the hot gases and the chamber shell.
High-Heat Transition Zones
Shaped lining elements for locations exposed to concentrated heat flux and repeated thermal cycling.
Replacement Heat-Shield Segments
Custom-manufactured bricks for maintenance and replacement of worn combustion chamber lining sections.
Information Needed for Technical Selection
The refractory shape and material quality must be selected according to the turbine design and actual operating conditions.
Request a Gas Turbine Combustion Chamber Refractory Quotation
Send us the turbine model, approved drawings, brick dimensions, operating conditions, required quantity and destination country for technical and commercial review.