Preparation method of heat insulation tile with complex shape for combustion chamber of gas turbine
A complex-shaped, gas turbine technology is applied in the field of preparing complex-shaped heat-insulating tiles for gas turbine combustion chambers, and can solve the problems of long curing time, low green strength, and complex curing process, and achieve easy demoulding and blank processing. , the effect of improving thermal shock stability and simple preparation method
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Embodiment 1
[0028] A method for preparing heat-insulating tiles with complex shapes for combustion chambers of gas turbines. The composition and weight parts of the heat-insulating tile castables are: 45 parts of corundum aggregate, 30 parts of mullite aggregate, and 10 parts of mullite fine powder , 10 parts of corundum fine powder, 5 parts of alumina fine powder, plus: 0.15 parts of solid dispersant FS20, 4.5 parts of binder silica sol solution, 3 parts of water, 0.05 parts of solid aluminum formate flocculant (or curing agent ); dry mix the solid raw materials together for 2 minutes, then add the silica sol solution and water and mix in a blender for 2 to 5 minutes, pour into the mold, maintain at room temperature for 12 hours, demould, and bake at 110°C After drying, it was kept at 1650°C for 6 hours.
Embodiment 2
[0030] A method for preparing heat-insulating tiles with complex shapes for combustion chambers of gas turbines. The composition and weight parts of the heat-insulating tile castables are: 35 parts of corundum aggregate, 35 parts of mullite aggregate, and 5 parts of mullite fine powder , 15 parts of corundum fine powder, 10 parts of alumina fine powder, plus: 0.2 parts of solid dispersant FS20, 3.5 parts of binder silica sol solution, 3.5 parts of water, 0.03 parts of solid aluminum formate flocculant (or curing agent ); dry mix the solid raw materials together for 2 minutes, then add the silica sol solution and water and mix in a blender for 2 to 5 minutes, pour into the mold, maintain at room temperature for 12 hours, demould, and bake at 110°C After drying, it was kept at 1650°C for 6 hours.
Embodiment 3
[0032] A method for preparing heat-insulating tiles with complex shapes for combustion chambers of gas turbines. The composition and weight parts of the heat-insulating tile castables are: 30 parts of corundum aggregate, 30 parts of mullite aggregate, and 10 parts of mullite fine powder , 15 parts of corundum fine powder, 15 parts of alumina fine powder, plus: 0.2 parts of solid dispersant FS20, 4 parts of binder silica sol solution, 3 parts of water, 0.02 parts of solid aluminum formate flocculant (or curing agent ); dry mix the solid raw materials together for 2 minutes, then add the silica sol solution and water and mix in a blender for 2 to 5 minutes, pour into the mold, maintain at room temperature for 12 hours, demould, and bake at 110°C After drying, it was kept at 1650°C for 6 hours.
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