Landing gear for ultralight aircraft

Details Landing gear for ultralight aircraft Landing gear for ultralight aircraft

1980-06-05

1983-02-08

Barefoot, Galen L.

Aeronautics and astronautics

Landing gear

244 13, 244DIG1, B64C 2504

Patent

active

043725066

ABSTRACT:
A landing gear for ultralight aircraft includes a main landing gear assembly disposed in a position relative to the longitudinal axis of the aircraft to permit either tail wheel type landing or tricycle landing operations with the assembly including an arched axle wherein the arch provides a spring for the landing gear as well as provides clearance to enable foot launching of the aircraft. A nose wheel strut assembly is linked to and extends forward of the main wheel landing gear assembly and includes a resilient tension link member.

REFERENCES:
patent: D243594 (1977-03-01), Koch
patent: 1022903 (1912-04-01), Warrick
patent: 1056844 (1913-03-01), Simpson
patent: 2818226 (1957-12-01), Hiller et al.
Poynter, Dan, "Hang Gliding", .COPYRGT.1976, pp. 176-177.

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