English: Diagram of a typical gas turbine jet engine (in English). Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor fan blades.
Français : Schéma en anglais montrant un turboréacteur d'avion typique (simple flux, simple corps). L'air est comprimé par les pales en entrant dans le réacteur, puis est mélangé avec le carburant qui brule dans la chambre à combustion. Les gaz d'échappement donnent une forte poussée en avant et fait tourner les turbines qui actionnent les pales de compression.
This is a retouched picture, which means that it has been digitally altered from its original version. Modifications: added energy graph. The original can be viewed here: Jet engine.svg: .
I, the copyright holder of this work, hereby publish it under the following licenses:
to share – to copy, distribute and transmit the work
to remix – to adapt the work
Under the following conditions:
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.
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.http://www.gnu.org/copyleft/fdl.htmlGFDLGNU Free Documentation Licensetruetrue
2007-12-19T05:56:12Z Jeff Dahl 1000x400 (521524 Bytes) reduce stroke width
2007-12-17T03:06:42Z Jeff Dahl 1000x400 (483965 Bytes)
2007-12-17T03:00:21Z Jeff Dahl 1000x400 (483965 Bytes) one more rectangle
2007-12-16T18:31:02Z Jeff Dahl 1000x400 (483071 Bytes) fx caps
2007-12-16T07:25:15Z Jeff Dahl 1000x400 (482623 Bytes) convert one last text to path
2007-12-16T07:23:29Z Jeff Dahl 1000x400 (471134 Bytes) convert text to paths
2007-12-16T07:15:01Z Jeff Dahl 1000x400 (403779 Bytes) {{Inkscape}} {{Information |Description=Diagram of a jet engine |Source=self-made, vector version of [[:en:Image:FAA-8083-3A Fig 14-1.PNG]] which comes from an [http://www.faa.gov/library/manuals/aircraft/airplane_handbook/ F
{{Information |Description={{en|Diagram of a typical gas turbine jet engine (in English). Air is compressed by the fan blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward t