How Do Surface Finish Characteristics Affect Turbofan HPT Blades?

  • Thread starter WaltLankor
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In summary, the researcher is looking for general background information on high pressure turbine blades, including metrology and fluid dynamics data. He is also looking for references from real people with experience in the field.
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WaltLankor
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Hi all
I recently found this thread helpful in my research
https://www.physicsforums.com/showthread.php?t=242166
and I figured you guys were a good option to help me find some more specific detail.
I am currently looking at background research for an investigation of the surface finish characteristics of the high pressure turbine blades of turbofan motors.
I am looking for general background information on; single crystal growth techniques, post casting machining procedures, Nickel superalloys, creep limiting data, plus anything else that would inform me in meaningful way about the field generally.
I also need good data referring to the surface finish of the blades, from both a surface metrology point of view and a fluid dynamics perspective.
I have searched and found some useful material but I have always found real people with experience in the field a far better bet than Google.
I would be very grateful for any information or references you might be able to offer, and any more generalised comments you might make.

Thanks
 
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in advance for your help.In addition to the resources mentioned in the previous thread, here are some additional resources that may be helpful for your research:1. Nickel Superalloys: - Nickel-Based Superalloys: Fundamentals and Applications by E. A. Loria (Springer, 2004)- Nickel-Based Superalloys: Properties, Characteristics, and Applications by S. P. Saovapakdi and J. C. Lippold (Elsevier, 1991)2. Single Crystal Growth Techniques: - Single Crystal Growth Technology by K. E. Spear (Springer, 2008)- Single Crystal Growth: Theory and Techniques by P. G. De Brabandere (CRC Press, 2004)3. Post Casting Machining Procedures:- The Foundry Handbook by S. M. Kaufman (CRC Press, 2003)- Machining of Materials and Their Properties by M. W. Shaw (Elsevier, 2009)4. Creep Limiting Data:- Creep and Creep-Rupture of Metals and Alloys by D. R. Askeland and H. F. Lundin (Elsevier, 2005)- Creep Mechanics by Y. I. Barlat (Springer, 2002)5. Surface Finish of Turbine Blades:- Finite Element Analysis of Turbine Blade Shaping Using Surface Roughness Parameters by R. T. Abualsamh and M. M. El-Hefnawi (Elsevier, 2004)- A Study on the Effect of Surface Roughness on Turbine Blade Performance by S. M. Kunz, et al. (Springer, 2006)
 

FAQ: How Do Surface Finish Characteristics Affect Turbofan HPT Blades?

What is a turbofan HPT blade?

A turbofan HPT (high-pressure turbine) blade is a component of a turbofan engine that is responsible for extracting energy from the hot, high-pressure exhaust gases produced by the engine's combustion process. This energy is used to power the engine's compressor and generate thrust for the aircraft.

Why is research on turbofan HPT blades important?

Research on turbofan HPT blades is important because these components play a critical role in the performance and efficiency of a turbofan engine. Improvements in HPT blade design can lead to increased engine efficiency, reduced emissions, and lower fuel consumption, making air travel more sustainable and cost-effective.

What materials are used in turbofan HPT blade research?

The materials used in turbofan HPT blade research vary, but they typically include high-strength alloys such as nickel-based superalloys. These materials are chosen for their ability to withstand high temperatures and stress levels, as well as their resistance to corrosion and fatigue.

How is the design of turbofan HPT blades tested?

The design of turbofan HPT blades is tested using a combination of computer simulations and physical testing. Computer simulations use advanced modeling techniques to predict the performance and behavior of the blades under different operating conditions. Physical testing involves subjecting actual blades to extreme conditions in a controlled environment to validate the results of the simulations.

What are some current areas of research in turbofan HPT blade technology?

Current areas of research in turbofan HPT blade technology include improving blade cooling techniques, exploring new materials and manufacturing processes, and developing more efficient and aerodynamic blade designs. There is also ongoing research on the impact of sustainability and environmental concerns on HPT blade design and development.

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