| 摘要 |
The engine has a multi-stage fan (9) with adjustable blades, a compressor unit (1,2), a combustion chamber (3), and a turbine (4). A second combustion chamber (5) with auto-ignition is positioned downstream of the turbine, and a second turbine (6) is positioned downstream of the second chamber. A diffusor is positioned upstream of the second chamber. One compressor (2) and both turbines are positioned on a common rotor shaft (7). All flow engines (9,1,2,4,6) of the jet engine are located on at least two rotor shafts, which are in active connection with each other via a transmission (8).
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