![]() ![]() The rotor was then disengaged before the takeoff run.As de la Cierva's autogyros achieved success and acceptance, others began to follow and with them came further innovation. ![]() The most acceptable solution was finally achieved with the, which was produced in some quantities a direct drive from the engine to the rotor was fitted, through which the rotor could be accelerated up to speed. Another approach was to tilt the tail stabiliser to deflect engine slipstream up through the rotor. Several methods were attempted in addition to the coiled rope system, which could take the rotor speed to 50% of that required, at which point movement along the ground to reach flying speed was necessary, while tilting the rotor to establish autorotation. It was based upon an fuselage, initial rotation of the rotor was achieved by the rapid uncoiling of a rope passed around stops on the undersides of the blades.A major problem with the autogyro was driving the rotor before takeoff. This machine had a four blade rotor with flapping hinges but relied upon conventional airplane controls for pitch, roll and yaw.
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |