ENGINE HPT blade construction and and its cooling holes

AI Thread Summary
The discussion focuses on a request for assistance regarding High-Pressure Turbine (HPT) blades and their cooling holes, specifically in the context of the CFM56-5C engine. The original poster seeks information on the source of cooling air for HPT blades, particularly whether it comes from High-Pressure Compressor (HPC) air. There is some confusion about whether the poster is looking for research facilities for experiments or academic papers on the topic. Participants in the discussion seek clarification on the specific needs of the poster. The thread highlights the importance of understanding cooling systems in turbine design.
Lloyd Alejandro
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Hi there, i am currently working in an airline industry but unfortunately do not have enough facilities to carry out my research on the HPT Blades and its cooling holes of an Engine.

Would anybody help me on this matter?

Thanks
 
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It's a little unclear what you are asking. Do you want to find turbine research facilities to perform your own experiments in or are you looking for papers on the subject?
 
billy_joule said:
It's a little unclear what you are asking. Do you want to find turbine research facilities to perform your own experiments in or are you looking for papers on the subject?
Sorry, i have noted that there are cooling system in a particular HPT Blade design basically for CFM56-5C. Just wanted to know if someone could provide simulation in which where the cooling air came from (e.g internal cooling of HPT came from the HPC air and etc.

Tnx
 
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