| 摘要 |
<p>A rotor wing in a fibre-reinforced composite design comprising fibre layers, in particular for a tail rotor of a rotary wing aircraft, with a rotor blade (1) that comprises a blade skin (40, 50) and a blade body (41-57) that comprises an aerodynamically effective profile, with a tension-torque-transmission element (3) connected to it, which is designed in one piece with the rotor blade (1), and with fibre layers (42-47) that extend through the tension-torque-transmission element (3) and are scarf-join in the rotor blade (1), is improved in that the fibre layers (42-47) extend right through from the tension-torque-transmission element (3) to the blade body (41-57). Furthermore, a method for producing the rotor wing is described.</p> |
