Safety device for an emergency landing of an aircraft

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Patent

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Details

244110R, 244114R, B64F 100

Patent

active

051709660

ABSTRACT:
A safety device for an emergency landing of an aircraft has a runaway. A unit for retarding the speed of the aircraft is mounted in the runway and includes a plurality of rows of juxtaposed rotary bearing members, each of which is provided with a friction surface, a plurality of rotatable shafts, each of which carries each row of the rotary bearing members, and a hydraulic unit provided in each row of the rotary bearing members. A unit for braking the speed of the aircraft is fixed in the runway downstream of the retarding unit and includes a plurality of rows of juxtaposed stationary bearing members, each of which is provided with a friction surface. A unit for supporting and guiding the aircraft to move on the runway includes a base slidable on the retarding unit and the braking unit and a preventing unit for preventing the aircraft from being released from the base after the aircraft lands on the base. The safety device further includes a fire-retarding fluid provided in the runway.

REFERENCES:
patent: 2425886 (1947-08-01), Knox
patent: 3210029 (1965-10-01), Brusch et al.
patent: 3380690 (1968-04-01), Rego
patent: 3490722 (1970-01-01), Schnarr et al.

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