Engine suspension on aircraft

Handling: hand and hoist-line implements – Spacing hoist bar or frame – Load gripping units

Patent

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Details

294 78A, B66C 142

Patent

active

040799816

ABSTRACT:
This invention relates to an improvement in an engine suspension for aircraft having at least one bearing with a vertical thrust bolt which introduces into the aircraft cell shearing or tangential forces acting transversely to the longitudinal axis thereof, and a hoisting device for the engine assembly, the improvement comprising bearing means between the engine and the aircraft cell which bearing means permits vertical movement, anchoring means adapted to be attached to the engine, and detachable coupling means adapted to be connected between said anchoring means and said hoisting device, whereby a rigid connection for supporting said engine is produced.

REFERENCES:
patent: 2349717 (1944-05-01), Graham
patent: 2703252 (1955-03-01), Blackwell

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