File:Guide vanes after combustor.svg
Size of this PNG preview of this SVG file: 800 × 534 pixels. Other resolutions: 320 × 213 pixels | 640 × 427 pixels | 1,024 × 683 pixels | 1,280 × 854 pixels | 2,560 × 1,707 pixels | 1,063 × 709 pixels.
Original file (SVG file, nominally 1,063 × 709 pixels, file size: 83 KB)
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| Description |
English: Combustion chamber for a gas turbine. With thin film cooling for the first guide vanes of the turbine. The exhaust is cooled by acceleration by a nozzle in outside the paper-plane and by mixing with the cool air in the wake of the guide vanes. |
| Date |
2008-08-03 23:09 (UTC) |
| Source | |
| Author |
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I, the copyright holder of this work, hereby publish it under the following licenses:
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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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Original upload log
This image is a derivative work of the following images:
- Image:Combustor_with_guide_vanes.svg licensed with Cc-by-sa-3.0, GFDL
- 2008-07-20T10:37:27Z Arnero 3720x1949 (165040 Bytes) {{Information |Description={{en|1=Combustion chamber for a gas turbine. Swirl injector leading to a conical liquid fuel spray. Venturi nozzle for fast cross-flow through spray. Turbulence between fast flowing injected air fue
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File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 23:19, 3 August 2008 | | 1,063 × 709 (83 KB) | Arnero | {{Information |Description= |Source= |Date= |Author= |Permission= |other_versions= }} Category:Turbine (jet engine) |
| 23:13, 3 August 2008 |  | 1,063 × 709 (84 KB) | Arnero | {{Information |Description={{en|1=Combustion chamber for a gas turbine. With thin film cooling for the first guide vanes of the turbine. The exhaust is cooled by acceleration by a nozzle in outside the paper-plane and by mixing with the cool air in the wa |
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