摘要 |
<p>Model aircraft with a support device located in the aircraft fuselage for the wing surfaces and with an adjustment drive positioned in the front of the fuselage connected by a rod system with the rudder and the ailerons. The rudder rod system consists of two rod sections each of which is linked to lever arm of a balancing lever which has a swivel bearing. The balancing lever (8a, 8b) is located on the wing surface support device (14) and the lever arms (20, 21) of the balancing lever are seized to correspond to the length of the corresponding linked rod section (6a). The balancing lever is positioned in an extension of the wing surface support device.</p> |