GEAR FOR A FLAPPING WING AIRCRAFT

The invention relates to a gear for a flapping wing aircraft, having a gearwheel support, on which a gear-wheel is mounted so as to be rotatably movable about a gearwheel axis, which gearwheel is connected in a rotationally fixed manner to a crankshaft, which has a central section extending coaxially to the gearwheel axis and end regions adjoining the central section on both sides, the end regions each delimiting an angle between 0 degrees and 90 degrees with the central section and engage in a guide slot of an associated joint part which is mounted pivotably movable about a pivot axis on a joint support which is connected to the gearwheel support and which is mounted pivotably movable about a respective support axis on the gearwheel support wherein the joint supports are connected to a coupling strut and wherein an actuator, which is motion-coupled to the coupling strut, is arranged on the gearwheel support. 本发明涉及一种用于扑翼式飞行器的传动机构组件，所述传动机构组件具有齿轮支架，在所述齿轮支架处绕齿轮轴线能够转动运动地支承有齿轮，所述齿轮抗转动地与曲轴连接，所述曲轴具有与齿轮轴线同轴地延伸的中间区段和在