| 摘要 |
1. A rotor, especially for a rotary-wing aircraft, having a connection of the individual rotor blade to the rotor hub (1) by way of a rotor hub arm (1.1), directed radially outwards in the shape of a fork, with the interpolation of a mounting (3) which can be loaded compressively in the longitudinal direction of the biade and which at the same time permits the pitch angle movements of the blade, and in which additionally blade root (2) coupled with a control rod (8) is supported by means of a pivot pin (10), coaxial with the blade angle axis, in radial bearing (6) of the rotor hub, characterized in that the pivot pin, as a sleeve-shaped extension (10) of a blade root fitting (7), is the mounting for a blade control shaft (11) which is coupled, in the rotor hub (1), with the control rod (8) and to which, on the other hand, there is connected, in a torsionally-fast manner, a lever (12) which extends radially outwards, in the blade root fitting (7), relative to the blade control shaft axis and which is fixable thereon so as to be adjustable in the direction of rotation of the blade control shaft. |
