| 摘要 |
A rotor shaft (5), gearbox (6) and a drive (7) are mounted on a carrier (4) which is releasably attached to the mid region of the fuselage. The drive is formed as a turbine (7) that is attached to the carrier with the intake side upwards and the outlet side downwards. The fuselage is provided with an opening (8) for carrying out exhaust gases from the turbine. The gearbox is arranged in the region of the inlet side of the turbine.
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