Turbine blade from a Turbo-Union RB199 jet engine.
A turbine blade is the individual component which makes up the turbine section of a gas turbine or steam turbine. 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.
- 1 Introduction
- 2 Environment and failure modes
- 3 Materials
- 4 Cooling
- 5 See also
- 6 Notes
- 7 References
IntroductionDiagram of a twin spool jet engine. The high-pressure turbine is connected by a single spool to the high-pressure compressor (purple)- and the low-pressure turbine is connected to the low-pressure compressor by a second spool (green).
In a gas turbine engine, a single turbine section is made up of a disk or hub that holds many turbine blades. That turbine section is connected to a compressor section via a shaft (or "spool"), and that compressor section can either be axial or centrifugal. Air is compressed, raising the pressure and temperature, through the compressor stages of the engine. The temperature is then greatly increased by... ...read more