Device for the bearing harmonization of an airborne load

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

Patent

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Details

89156, B64D 102

Patent

active

041825020

ABSTRACT:
This device incorporated in a release or ejector mechanism for adjusting the transverse direction of an airborne load comprises a device for pivoting thereon the load-supporting hook and a bell crank linkage system, whether the load is equipped with a so-called saddle member or with standard rings. This device comprises essentially a cylindrical body formed either with an eccentric portion or with a transverse screw for performing the necessary adjustment, and a lock nut for firmly maintaining the selected adjustment position.

REFERENCES:
patent: 3784132 (1974-01-01), Newell
patent: 3954233 (1976-05-01), Hasquenoph et al.

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