Why Choose Us?
Wide Sales Market
Our products are sold to the UK, Germany, France, Italy, Poland, the United States, Canada, the Netherlands, Sweden, Austria, New Zealand, Singapore and India, serving more than 100 customers in the automotive industry.
Guaranteed Quality
China Welong was founded in 2001 and is certified by ISO 9001:2015 and the API-7-1 quality system. We are dedicated to the development and supply of customized metal parts used in various industries.
Rich Product Variety
Our main businesses include forging, sand casting, investment casting, centrifugal casting and machining. The materials we handle include cast iron, steel, stainless steel, aluminum, copper, zinc and various alloys.
Leading Service
We have many years of industry experience and a complete production management, quality supervision, sales service operation system. Whether you want to buy forging or stainless steel, just send your requirements by email and we can customize the product for you.
What is Turbine Blades
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.
Blade Shape
Turbine Blades are usually streamlined or aerodynamically designed with optimized curved shapes. Such a design can reduce fluid resistance and improve fluid flow efficiency.
Cooling Channels
Turbine Blades usually have internal cooling channels for cooling the blade surface through fluid. These cooling channels can help reduce the operating temperature of the blades and prevent the blades from overheating and causing failure.
Material Selection
Turbine Blades are usually made of high-temperature alloys or ceramic materials to meet the requirements of high temperature, high speed and high pressure environments. These materials have good heat resistance, corrosion resistance and high strength, and can withstand complex working conditions.

Cooling Method
It works by passing cooling air through passages internal to the blade. Heat is transferred by conduction through the blade, and then by convection into the air flowing inside of the blade. A large internal surface area is desirable for this method, so the cooling paths tend to be serpentine and full of small fins. The internal passages in the blade may be circular or elliptical in shape. Cooling is achieved by passing the air through these passages from hub towards the blade tip. This cooling air comes from an air compressor. In case of gas turbine the fluid outside is relatively hot which passes through the cooling passage and mixes with the main stream at the blade tip.
Film cooling (also called thin film cooling), a widely used type, allows for higher cooling effectiveness than either convection and impingement cooling.This technique consists of pumping the cooling air out of the blade through multiple small holes or slots in the structure. A thin layer (the film) of cooling air is then created on the external surface of the blade, reducing the heat transfer from main flow, whose temperature (1300–1800 kelvins) can exceed the melting point of the blade material (1300–1400 kelvins).
The blade surface is made of porous material which means having a large number of small orifices on the surface. Cooling air is forced through these porous holes which forms a film or cooler boundary layer. Besides this uniform cooling is caused by effusion of the coolant over the entire blade surface.
In the narrow trailing edge film cooling is used to enhance heat transfer from the blade. There is an array of pin fins on the blade surface. Heat transfer takes place from this array and through the side walls. As the coolant flows across the fins with high velocity, the flow separates and wakes are formed. Many factors contribute towards heat transfer rate among which the type of pin fin and the spacing between fins are the most significant.
This is similar to film cooling in that it creates a thin film of cooling air on the blade, but it is different in that air is "leaked" through a porous shell rather than injected through holes. This type of cooling is effective at high temperatures as it uniformly covers the entire blade with cool air.Transpiration-cooled blades generally consist of a rigid strut with a porous shell. Air flows through internal channels of the strut and then passes through the porous shell to cool the blade.
Factors to Consider in Turbine Blade Material Selection
Strength
The material must have sufficient strength to withstand the high loads and stresses experienced during operation. This includes both tensile and compressive strength.
Stiffness
The material should have high stiffness to minimize blade deflection and ensure structural integrity. Stiffness is typically measured in terms of Young's modulus.
Fatigue Resistance
The material must have excellent fatigue resistance to withstand the cyclic loads experienced over the turbine's lifetime, which can exceed 20 years.
Damage Tolerance
The material should be able to withstand damage, such as impact from debris or lightning strikes, without catastrophic failure.
Specific Stiffness
The ratio of stiffness to density, known as specific stiffness, is an important factor as it affects the overall weight of the blade.
Specific Strength
Similarly, the ratio of strength to density, or specific strength, is crucial for minimizing the blade's weight.
Specific Fatigue Limit
The ratio of the fatigue limit to density, or specific fatigue limit, is another important consideration for ensuring the blade's long-term durability.
The Foundation of Turbine Blade Shape
Chord Length
The distance between the leading edge and the trailing edge of the blade at a given point. Longer chord lengths can increase the surface area and generate more lift, but they also increase the structural loads on the blade.
Camber
The curvature of the upper surface of the blade. Higher camber values can increase lift, but they also increase the risk of stall at higher wind speeds.
Thickness
The distance between the upper and lower surfaces of the blade at a given point. Thicker blades can provide more structural integrity, but they also increase drag and reduce the overall efficiency of the turbine.
Twist
The angle of the blade relative to the axis of rotation. Twisting the blade can help to optimize the angle of attack along the length of the blade, improving the overall performance of the turbine.
Process of Turbine Blade
CAD/CAM Design
The process starts with computer-aided design (CAD) and computer-aided manufacturing (CAM) software. Engineers create a 3D model of the turbine blade, incorporating precise geometries, aerodynamics, and material considerations. The CAD model serves as a blueprint for subsequent machining operations.
Material Selection
High-performance materials are crucial for turbine blades, given the harsh operating conditions they endure. Nickel-based superalloys, such as Inconel and Rene, are commonly used due to their exceptional strength, corrosion resistance, and high-temperature capabilities. Material selection is crucial to ensure the blade's integrity and performance.
Rough Machining
The rough machining process begins with the removal of excess material from the blade's initial shape. This is typically achieved using advanced CNC machining techniques such as milling or turning. Rough machining establishes the basic shape and removes any excess material, allowing for subsequent finishing operations.
Airfoil Profiling
Airfoil profiling involves precision machining of the blade's aerodynamic profile. This process requires high-precision CNC machining, including 5-axis or even 9-axis simultaneous machining to achieve intricate blade geometries and tight tolerances. The goal is to create the desired airfoil shape, including the camber, twist, and chord length, to optimize aerodynamic performance.
Cooling Holes Drilling
Turbine blades often feature intricate internal cooling systems to maintain temperature stability. These cooling holes are drilled or machined into the blade to allow for the passage of cooling air. Specialized drilling techniques, such as laser drilling or EDM (Electrical Discharge Machining), are utilized to achieve precise hole placement and diameters.
Finishing Operations
Once the rough machining and airfoil profiling are complete, the turbine blades undergo various finishing operations. This includes precision grinding, polishing, and surface treatments to achieve the required surface finish and remove any machining marks. Finishing operations are critical to reduce aerodynamic losses and improve the blade's overall efficiency.
Quality Control
Throughout the machining process, rigorous quality control measures are implemented to ensure the turbine blades meet the highest standards. Advanced inspection techniques, such as coordinate measuring machines (CMM), non-destructive testing (NDT), and visual inspections, are employed to verify dimensional accuracy, surface quality, and structural integrity.
Frequently Asked Questions
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