Impact of a cooled cooling air system on the external aerodynamics of a gas turbine combustion system
To manage the increasing turbine temperatures of future gas turbines a cooled-cooling air system has been proposed. In such a system some of the compressor efflux is diverted for additional cooling in a heat exchanger located in the by-pass duct. The cooled air must then be returned, across the main...
Saved in:
| Main Authors: | , , , , |
|---|---|
| Format: | Default Article |
| Published: |
2017
|
| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/23563 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|