A landing gear device for reducing crash landings includes a mounting assembly that is configured to couple to a bottom of a vertical take-off and landing aircraft, such as a remotely controlled helicopter. Each of a plurality of rods, which are resiliently flexible, is coupled to and extends transversely from the mounting assembly to define a pyramid, with the mounting assembly being positioned at an apex of the pyramid. The plurality of rods is configured to reduce a frequency of crash landings of the vertical take-off and landing aircraft.
Landing Gear Device
2021-02-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2020
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