| 摘要 |
<p>A rotor system for an aircraft including a rotor (1) with a drive part (2) mounted rotatable about a rotation axis (8) and supporting the proximal end (9) of at least one rotor blade (3).The rotor system comprises a jet turbine (4) for providing pressurised exhaust gas to a rotary structure(7) having at least one jet nozzle outlet (6) and at least one jet stream duct (5) for transporting the pressurised exhaust gas from the turbine (4) to the jet nozzle outlet (6) to cause rotation of the rotary structure (7) by expelling the pressurised exhaust gas through the nozzle outlet (6). In addition, only the rotary structure(7) and not the rotor blade (3) comprise a jet stream duct (5) and a nozzle outlet (6).</p> |
