Load lifting system

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

Patent

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Details

212 71, B64D 108

Patent

active

039469719

ABSTRACT:
A load lifting system includes a platform suspended beneath a helicopter and provided with an engine for supplying thrust in a vertical direction. The platform engine is controlled to lift the load suspended below the platform while the aircraft supplies the lift for supporting the platform and engine.

REFERENCES:
patent: 3017138 (1962-01-01), Flint
patent: 3112900 (1963-12-01), Yost
patent: 3856236 (1974-12-01), Doolittle

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