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Turbine Blade /Manufacturer For Aerospace,Casting high temperature alloys (inconel 718/713C)

Casting high temperature alloys (inconel 718/713C) Our factory can independently produce cast high -temperature alloy alloy and precision casting products,plus 5axis CNC machining. Casting high -temperature alloy alloy alloys are a type of high -temperature alloy that is formed by casting methods. It has a higher degree of alloying composition range and higher service temperature range.
Precision castings are key components used in the thermal end of aviation engines and gas turbines, including large complicated thin -walled structural parts, turbine rotation and guidance blades, overall leaves, guides, transposers, etc.
Our factory is one of the few production companies in China that master the core technology of high -temperature alloy near -net melting models. Products are mainly used in the field of aviation and burning machines.

June 5, 2023

A turbine blade is a radial aerofoil mounted in the rim of a turbine disc and which produces a tangential force which rotates a turbine rotor.Each turbine disc has many blades. As such they are used in gas turbine engines and steam turbines. The blades are responsible for extracting energy from the high temperature, high pressure gas produced by the combustor. The turbine blades are often the limiting component of gas turbines.To survive in this difficult environment, turbine blades often use exotic materials like superalloys and many different methods of cooling that can be categorized as internal and external cooling,and thermal barrier coatings. Blade fatigue is a major source of failure in steam turbines and gas turbines. Fatigue is caused by the stress induced by vibration and resonance within the operating range of machinery. To protect blades from these high dynamic stresses, friction dampers are used.

Blades of wind turbines and water turbines are designed to operate in different conditions, which typically involve lower rotational speeds and temperatures.

In a gas turbine engine, a single turbine stage is made up of a rotating disk that holds many turbine blades and a stationary ring of nozzle guide vanes in front of the blades. The turbine is connected to a compressor using a shaft (the complete rotating assembly sometimes called a "spool"). Air is compressed, raising the pressure and temperature, as it passes through the compressor. The temperature is then increased by combustion of fuel inside the combustor which is located between the compressor and the turbine. The high-temperature, high-pressure gas then passes through the turbine. The turbine stages extract energy from this flow, lowering the pressure and temperature of the gas and transfer the kinetic energy to the compressor. The way the turbine works is similar to how the compressor works, only in reverse, in so far as energy exchange between the gas and the machine is concerned, for example. There is a direct relationship between how much the gas temperature changes (increase in compressor, decrease in turbine) and the shaft power input (compressor) or output (turbine).

For a turbofan engine the number of turbine stages required to drive the fan increases with the bypass-ratio unless the turbine speed can be increased by adding a gearbox between the turbine and fan in which case fewer stages are required.The number of turbine stages can have a great effect on how the turbine blades are designed for each stage. Many gas turbine engines are twin-spool designs, meaning that there is a high-pressure spool and a low-pressure spool. Other gas turbines use three spools, adding an intermediate-pressure spool between the high- and low-pressure spool. The high-pressure turbine is exposed to the hottest, highest-pressure air, and the low-pressure turbine is subjected to cooler, lower-pressure air. The difference in conditions leads to the design of high-pressure and low-pressure turbine blades that are significantly different in material and cooling choices even though the aerodynamic and thermodynamic principles are the same.Under these severe operating conditions inside the gas and steam turbines, the blades face high temperature, high stresses, and potentially high vibrations. Steam turbine blades are critical components in power plants which convert the linear motion of high-temperature and high-pressure steam flowing down a pressure gradient into a rotary motion of the turbine shaft.

Artisan Industry is a supplier of aerospace components; Products include impeller, turbine, combustion chamber, fastener, etc.

If you have any questions or needs, please contact us. Here is our contact information:

Price Inquiry:sales.lily@superalloyparts.com

Technical Support:eng.daisy@superalloyparts.com

Superalloy parts, refers to the name of the article after the structural change is finally fabrication by changing the high-temperature alloys with a suitable manufacturing process.

The properties of high temperature resistance and corrosion resistance of superalloy mainly depend on its chemical composition and structure. Taking the GH4169 nickel-based deformed superalloy as an example, it can be seen that the niobium content in the GH4169 alloy is high, and the degree of niobium segregation in the alloy is directly related to the metallurgical process. The high temperature of about 1 000 ℃ is similar to the US grade Inconel718. The alloy is composed of γ matrix phase, δ phase, carbide and strengthening phase γ’ and γ” phases. The chemical elements and matrix structure of GH4169 alloy show its strong mechanical properties. The yield strength and tensile strength are several times better than those of 45 steel, and the plasticity is better than that of 45 steel. The stable lattice structure and a large number of strengthening factors constitute its excellent mechanical properties.

Superalloy refers to a kind of metal material based on iron, nickel and cobalt, which can work for a long time under the action of high temperature above 600℃ and certain stress; and has high high temperature strength, good oxidation resistance and corrosion resistance, Good fatigue properties, fracture toughness and other comprehensive properties. The superalloy is a single austenite structure, which has good structure stability and service reliability at various temperatures.

Based on the above performance characteristics, and the high degree of alloying of superalloys, also known as “super alloys”, is an important material widely used in aviation, aerospace, petroleum, chemical, and ships. According to the matrix elements, superalloys are divided into iron-based, nickel-based, cobalt-based and other superalloys. The operating temperature of iron-based superalloys can generally only reach 750~780 °C. For heat-resistant parts used at higher temperatures, nickel-based and refractory metal-based alloys are used. Nickel-based superalloys occupy a special and important position in the entire field of superalloys, and are widely used to manufacture the hottest parts of aviation jet engines and various industrial gas turbines.

Custom Superalloy Parts Applications – What is Custom Superalloy Parts Used for
Because the fabrication allows a very high precision without altering the structure of the material with a good rate of manufacture, fabrication is becoming increasingly common as its machine range, control systems and cutting tools are just growing.