Universal aircraft-carriage suspension lug system

Aeronautics and astronautics – Aircraft structure – Passenger or cargo loading or discharging

Patent

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Details

89 151, B64D 112, B64D 104

Patent

active

059610751

ABSTRACT:
A suspension lug system for use with a jettisonable weapon that provides a mechanical interface between the weapon and a multiplicity of aircraft. The system has a dual-function lug that is disposed in a well when it is in a stowed position, and that is pivotable in opposite directions on a transverse pivot pin. A first end of the lug is configured as a saddle lug that is exposed above the outer surface when the lug is rotated into a saddle-deployed position. The second end of the lug is configured as a clevis that is exposed above an outer surface of the system when the lug is rotated into a clevis-deployed position. A spring is coupled to the lug that spring loads it and returns it to a stowed position when it is not engaged with the ejector release unit to preserve the outer contour of the weapon.

REFERENCES:
patent: 2852981 (1958-09-01), Caya
patent: 2869916 (1959-01-01), Benson
patent: 3181908 (1965-05-01), Clark
patent: 4842218 (1989-06-01), Groutage et al.
patent: 4917526 (1990-04-01), Paterson
patent: 5056408 (1991-10-01), Joner et al.

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