25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder Description:
25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder is a high-performance cermet powder engineered for high-temperature applications, integrating a nickel-chromium-aluminum alloy with tungsten carbide cobalt. This composite powder delivers excellent erosion resistance and controlled abradability, optimized for enhancing clearance control and gas path efficiency in challenging environments such as jet engine compressors. Its robust, binder-free composition ensures uniformity and reliability, validated through rigorous testing to endure temperatures up to 650°C (1200°F) with strong oxidation resistance, making it perfect for critical industrial applications.
25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder Specifications:
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Nominal Chemistry
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25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co)
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Nom. Particle Size Distr.(µm)
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-90 +31
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Morphology
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Angular/Blocky/Spheroidal
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Max. Service Temperature (°C)
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500
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Achieved Macrohardness
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45 HRC
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Applications of 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder:
25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder is specially designed for use as an abradable coating material in the high-temperature sections of jet engine compressors. This powder is engineered to optimize clearance control by reducing wear on rotating components while maximizing gas path efficiency. It is essential for maintaining operational reliability and extending the lifespan of components in aerospace and industrial applications that operate under extreme temperatures and pressures.
Packing of 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder:
Our 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder is meticulously managed during storage and transportation to ensure it retains its original quality.
FAQ for 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder:
Q1: What are the key benefits of using 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder in jet engine compressors?
A1: This powder provides excellent erosion resistance and controlled abradability, which are crucial for optimizing clearance control, enhancing gas path efficiency, and reducing wear on rotating components in high-temperature environments.
Q2: How is 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder produced, and why is it ideal for aerospace applications?
A2: The powder is created by combining a nickel-chromium-aluminum alloy with tungsten carbide cobalt through a specialized process. This ensures robustness and uniformity, making it highly reliable for performance in aerospace and industrial settings.
Q3: Can the coatings of 25(Ni 4.3Cr 1Fe 1Si 0.9B 0.2C) - 75(WC 12Co) Powder be customized for specific erosion resistance and abradability needs?
A3: Yes, the powder can be tailored to meet specific requirements, providing flexibility to achieve the desired erosion resistance and abradability characteristics for various industrial applications.
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