Method and device for temporarily enlarging the opening or hatch

Aeronautics and astronautics – Aircraft structure – Load accommodation

Patent

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Details

105396, 244119, B64C 122

Patent

active

046217800

ABSTRACT:
The present invention relates to a method and device for temporarily enlarging the opening or hatch area of a structural frame of an aircraft. The invention proposes a fixture of smaller dimensions than the structural girder which is able to replace the latter temporarily during certain periods, in particular during loading and unloading of cargo. The invention finds an application in the fitting out of a transport aircraft.

REFERENCES:
patent: 2392789 (1946-01-01), Watter

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