Gear for a flapping wing aircraft
AssigneeFesto AG & Co.
InventorRainer Mugrauer
Life of this patent
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AssigneeFesto AG & Co.
InventorRainer Mugrauer
Estimating the term…
Gear for a flapping wing aircraft, having a gearwheel support, on which a gearwheel 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.
A gear for a flapping wing aircraft, comprising a gearwheel support, on which a gearwheel is rotatably mounted about a gearwheel axis, further comprising a crankshaft, which is non-rotatably connected to the gearwheel and which has a central section extending coaxially with the gearwheel axis and which has end regions, wherein the central section passes through the gearwheel and wherein the end regions delimit an angle between 0 degrees and 90 degrees with the central section, wherein each of the end regions is inserted into a guide slot of an associated joint part which is mounted on a joint support connected to the gearwheel support so as to be pivotable about a pivot axis, and wherein each of the joint supports is mounted on the gearwheel support so as to be pivotable about a respective support axis, wherein the joint supports are connected to a coupling strut, wherein an actuator for providing an actuating movement is arranged on the gearwheel support and is coupled to the coupling strut.
Dependencies are inferred from the claim text.