| 摘要 |
<p>The aircraft has one or more turboprop engines (7) with lengthwise axes (L-L) parallel to the lengthwise axis (X-X) of the aircraft, mounted on pylons (8) on a rear cell of the aircraft fuselage that acts as a noise barrier. Depending on the number of engines and the tail assembly configuration, the turboprop engines are located between vertical fins (5) and/or horizontal tailplanes (6), with contrarotating twin propellers (9, 10) located to the rear of the engines and as far as possible towards the rear of the aircraft. The aircraft can be propelled by turboprop engine(s) alone or a combination of turboprop and under-wing turbojet engines.</p> |
