The compressor blade is a critical rotating component mounted along the outer edge of the compressor disk in a gas turbine engine. Its primary function is to impart kinetic energy to the incoming air, increasing its pressure as it passes through successive stages of the compressor section. This high-pressure, high-temperature air is then directed into the combustion chamber, where it mixes with fuel to support efficient and powerful engine operation.

Compressor blades are typically manufactured from high-strength materials such as titanium alloys, nickel-based superalloys, or stainless steel. Depending on customer requirements, we can also produce blades using custom-specified materials to meet specific operational needs such as heat resistance, weight reduction, or durability in extreme environments.

The aerodynamic shape of the blade is precisely engineered to maximize pressure rise while minimizing losses due to turbulence or vibration. Each stage of the compressor may feature a different blade profile, tailored for optimal performance at that specific point in the air compression process. Blades can be solid, hollow, or incorporate cooling channels depending on the engine’s design and operating conditions.

Our company manufactures a wide range of compressor blades for gas turbines used in power generation, aviation, and marine propulsion systems. We can produce blades according to customer specifications, technical drawings, or physical samples. Whether for new production, maintenance, or reverse engineering of legacy components, we deliver high-quality blades that meet demanding industry standards.