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A CHROMIUM/ALUMINIUM DIFFUSION COATING SOURCE MATERIAL. THE MATERIAL IS USED FOR APPLYING TO TURBINE BLADES USED ON CIVIL AEROSPACE GAS TURBINE ENGINES. THE MATERIAL IS IN THE FORM OF SOLID CHIPS WITH A SIZE OF 8-22 MM ACROSS THE MAIN CHIP AXIS. THE CHIPS ARE SILVER GREY IN COLOUR. THE MINIMUM CHROMIUM 55%.

BONDING AND CASTING ALLOY INGOT USED IN DENTISTRY FOR MAKING CROWNS AND BRIDGES. CHROMIUM ALLOY COMPOSITION WITH TUNGSTEN, SILICON, TRACE ELEMENTS, MANGANESE, IRON, CARBON, COBALT. NICKEL, BERYLIUM AND COPPER FREE. CONTAINS PREDOMINANTLY CHROMIUM.

CHROMIUM/ALUMINIUM ALLOY - THIS IS IN A NUGGET FORM (LOOKS LIKE A SMALL ROUGH STONE 2" IN DIAMETER). THE MIX IS 56% CHROMIUM AND 44% ALUMINIUM. THESE NUGGETS ARE USED DURING A PRODUCTION PROCESS TO DEPOSIT CHROMIUM/ALUMINIUM TO AIRCRAFT ENGINE COMPONENTS. THE NUGGETS REDUCE IN SIZE OVER TIME AS THE METALS TRANSFER.