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Gas Turbine Heat Transfer and Cooling Technology by Je-Chin Han , Sandip Dutta , Srinath Ekkad Book Details
| Book Name | Gas Turbine Heat Transfer and Cooling Technology |
| Author | Je-Chin Han , Sandip Dutta , Srinath Ekkad |
| Category | Mechanical Engineering Books, Education Books |
| Book Language | English |
| Publisher | Taylor and Francis Publishers |
| Pages | 865 |
| Country | India |
| Book Size | 30 MB |
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About Gas Turbine Heat Transfer and Cooling Technology by Je-Chin Han , Sandip Dutta , Srinath Ekkad Book
Gas Turbine Heat Transfer and Cooling Technology is a specialized topic within the field of gas turbines and engineering thermodynamics. This area focuses on the study and application of heat transfer principles and cooling techniques in gas turbine engines. Gas turbines are widely used in aviation, power generation, and industrial applications, and managing heat transfer is crucial for their efficiency, performance, and durability.
Key aspects and topics related to gas turbine heat transfer and cooling technology include:
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Gas Turbine Basics: Gas turbines are engines that convert the energy of fuel combustion into mechanical work through the expansion of hot gases. Understanding the basic operation and components of gas turbines is essential before delving into heat transfer and cooling considerations.
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Combustion and Hot Gases: Gas turbines involve high-temperature combustion processes that produce hot gases. Effective heat transfer management is critical to prevent overheating and ensure the longevity of engine components.
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Turbine Blades and Vanes: Turbine blades and vanes are exposed to extremely hot gases. Effective cooling methods are employed to prevent damage and prolong their operational life. This might include film cooling, internal cooling channels, and thermal barrier coatings.
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Film Cooling: Film cooling is a technique where a thin layer of cooler air is injected over the surface of turbine blades to create a protective cooling film, reducing the heat transfer from the hot gases to the blade.
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Internal Cooling: Many gas turbine components, such as blades and vanes, are designed with internal cooling passages through which cooler air is circulated to extract heat from the material and maintain lower surface temperatures.
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Heat Transfer Analysis: Engineers analyze heat transfer patterns within gas turbine components to ensure uniform cooling and prevent hot spots that could lead to material degradation.
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Cooling Technologies: Different cooling technologies, such as impingement cooling, convective cooling, and transpiration cooling, may be used to manage heat transfer in various gas turbine components.
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Computational Fluid Dynamics (CFD): CFD simulations play a crucial role in designing and optimizing cooling systems. CFD software allows engineers to model and analyze heat transfer and fluid flow within complex geometries.
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Cooling Challenges: Achieving efficient cooling while minimizing the impact on overall engine efficiency is a challenge in gas turbine design. Balancing the needs for cooling and performance is a key consideration.
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Thermal Barrier Coatings: These coatings are applied to turbine components to provide insulation and protect them from high-temperature gases, enhancing their lifespan.
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Research and Development: Ongoing research focuses on improving cooling techniques, materials, and designs to enhance the performance and efficiency of gas turbine engines.
Given the complexity and importance of managing heat transfer and cooling in gas turbine technology, this area requires interdisciplinary knowledge in fluid dynamics, thermodynamics, material science, and engineering design. If you're interested in this field, you may find textbooks, research papers, and courses that cover gas turbine heat transfer and cooling technology to be valuable resources.
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