Aircraft landing-gear with skids

Aeronautics and astronautics – Landing gear – Skids

Patent

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Details

9310A, 244 1717, 280 28, B64C 2532, B64C 2552

Patent

active

041968786

ABSTRACT:
In rotary-wing aircraft, a landing gear having two main skids connected to the aircraft structure by two cantilevered arcuate supports. Each skid has at least one flexible element capable of flexing resiliently upon contacting the ground.

REFERENCES:
patent: 1362511 (1920-12-01), Roe
patent: 1420609 (1922-06-01), Curtiss
patent: 2023312 (1935-12-01), Seversky
patent: 2686023 (1954-08-01), Larry
patent: 2958486 (1960-11-01), Bloomfield
patent: 3220670 (1965-11-01), Fuller
patent: 3387802 (1968-06-01), Cruz
patent: 3507466 (1970-04-01), LaFleur
patent: 3586263 (1971-06-01), Payne

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