Tandem type landing gear

Details Tandem type landing gear Tandem type landing gear

1982-04-02

1983-09-06

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

244102SL, B64C 2526

Patent

active

044024770

ABSTRACT:
The present invention relates to landing gears. The landing gear includes essentially two legs (1, 2) comprising respecitvely two arms (10, 28) and two rocker beams (3, 24), a bar (21) forming with the two arms (10, 28) a deformable parallelogram, a strut (37) consisting of two levers (23, 38) placed on a diagonal of the parallelogram, two locking links (50, 51) cooperating with the strut (37), these two rotatably mounted links being rotated by an actuator (70) and a spring (60). The landing gear finds its application in commuter aircraft fitted with tandem type landing gears.

REFERENCES:
patent: 2475723 (1949-07-01), Sanford
patent: 4355773 (1982-10-01), Masclef et al.

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