Multi-positional tail skids and associated methods of use

Aeronautics and astronautics – Landing gear – Tail supports

Reexamination Certificate

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Reexamination Certificate

active

06845944

ABSTRACT:
Multi-positional tail skid assemblies and methods for their use. In one embodiment, a multi-positional tail skid assembly includes a skid member and a skid deployment system operably connected to the skid member. The skid member can include a first portion attachable to an aft portion of a fuselage and a second portion movable relative to the aft portion of the fuselage. The second portion can support a skid surface configured to contact a surface of a runway. The skid deployment system can be configured to move the skid surface between first and second positions. When the skid surface is in the first position, the skid surface is closer to the aft portion of the fuselage than when the skid surface is in the second position.

REFERENCES:
patent: 1515577 (1924-11-01), Gentzcke
patent: 2355210 (1944-08-01), Eddy
patent: 3252548 (1966-05-01), Pajak et al.
patent: 3493082 (1970-02-01), Bell
patent: 4528564 (1985-07-01), Trampnau
patent: 4815678 (1989-03-01), Gaqne
patent: 5901927 (1999-05-01), Ho
patent: 5984229 (1999-11-01), Hollowell et al.

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