File:GaTurbineBlade.svg
Size of this PNG preview of this SVG file: 545 × 298 pixels. Other resolutions: 320 × 175 pixels | 640 × 350 pixels | 1,024 × 560 pixels | 1,280 × 700 pixels | 2,560 × 1,400 pixels.
Original file (SVG file, nominally 545 × 298 pixels, file size: 203 KB)
Summary
| Description | English: A schematic of a high-pressure turbine blade as used in aircraft jet engines. An internal cooling system enables a temperature gradient across the walls of the blade. Cooling holes allow the cooling air to exit and cover the outer blade surface with a cooling film. |
| Date | |
| Source | Own work by uploader; produced with Adobe illustrator |
| Author | Tomeasy |
Licensing
I, the copyright holder of this work, hereby publish it under the following licenses:
This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license.
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- attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made. You may do so in any reasonable manner, but not in any way that suggests the licensor endorses you or your use.
- share alike – If you remix, transform, or build upon the material, you must distribute your contributions under the same or compatible license as the original.
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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. |
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 10:15, 17 February 2009 | | 545 × 298 (203 KB) | Tomeasy | {{Information |Description={{en|1=A high-pressure turbine blade with internal cooling as used in aircraft jet engines.}} |Source=Own work by uploader; produced with Adobe illustrator |Author=Tomeasy |Date=2009-02-17 |Permission= |other_ve |
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