| 摘要 |
403,253. Wind motors. STRANDGREN, C. B., 14, Rue Gallieni, Versailles, France. March 9, 1933, Nos. 7166 and 7167. Convention dates, March 11, 1932 and Jan. 25, 1933. [Class 110 (iii).] A feathering paddle wheel or wind motor has its blades connected to the hub by flexible members such members extending in pairs in opposite directions and in substantial alignment from the same points on the hub so as to balance out the centrifugal and aerodynamic forces acting on the hub. In one form, Figs. 1 and 2, two feathering paddle wheels are carried by a transverse shaft 3 supported above the body of a flying machine by struts 2. Each wheel comprises a hub 4 built up from sheet steel plates and having secured at its periphery a number of attaching members 8, Fig. 3. To each member 8 are attached two sets of diverging flexible connecting members 9, 9a, 9b, Fig. 2, each member such as ab, Fig. 1 of one set being substantially in line with a member such as cd of the other set. These members may be cables or wires of circular, oval, or willow leaf section. At their outer ends members 9, 9a, 9b of each set are attached to forked brackets 10, 10a, 10b to which a wing 11 is pivoted on an axis 12. Brackets 10, 10b are secured to collars 13 by which they are connected to elements of a polygonal or circular belt 14 which is built of metal tubes and serves to maintain the wings in position when the wheel is idle and to prevent lateral wing movements. The wings are feathered about pivots 12 by cables 14, 15 attached to the ends of a lever 20, Fig. 3, which is oscillated during rotation of the wheel by means of a roller 24 engaged in a cam slot 23 formed in a radial arm 22 of lever 20. Roller 24 is carried by an eccentric member 25 rotating with the hub. Fig. 6 shows an arrangement in which a double hub A, B is used. A wheel having only four wings may have each wing braced to the corners of a small central rectangular frame. In the case of a five-wing wheel this frame may be pentangular or circular. In the case of wings of large span it is necessary in order to avoid using three or more hubs to provide means for bracing the wings against bending moments due to centripetal acceleration or to aerodynamic loading tension bracing only being used. Bracing members connecting each wing to its adjacent wings only may be used. A multi-hub wheel may be braced against lateral wing movement by wires connected to fittings on the propeller shaft spaced inwardly from the outermost hubs, |
