| 摘要 |
When, according to the invention, a rotor (1) for a propeller or a windmill is equipped with two-part blades (3), which are secured to the hub (2) offset to the right of a centre line (C) through the hub, and which comprise a first blade plane (4) and a laterally offset second blade plan (5), and the blade planes are arranged in such a manner that the leading edge (7) of the first blade plane extends approximately in parallel with the centre line (C) radially outwards from the centre of the hub and forms an acute angle (A) in combination with the leading edge (8) of the second blade plane, so that the leading edge (8) is disposed behind the leading edge (7) seen in relation to the direction of rotation of the hub, and when the length of the trailing edge (10) of the second blade plane is defined by a line which extends from the centre of the hub essentially perpendicularly to the trailing edge (10) of the blade plane, and by the blade tip of the blade plane, a rotor having a high efficiency and having relatively small dimensions is achieved. |
