Cargo bin assembly for use in a helicopter cargo hold

Details Cargo bin assembly for use in a helicopter cargo hold Cargo bin assembly for use in a helicopter cargo hold

1998-11-09

2000-09-05

Poon, Peter M.

Aeronautics and astronautics

Aircraft structure

Load accommodation

220 15, 220 4, B64C 120, B65D 8800, B65D 600

Patent

active

061130311

ABSTRACT:
A helicopter, or other aircraft, cargo bin is sized and configured so as to closely match the size and configuration of a closed cargo hold in the aircraft. The cargo bin is provided with a cover that is formed from a flame-retardant fabric which can be folded forwardly to open the top of the cargo bin, whereby the open bin can be positioned on a hydraulic ramp in the cargo hold before or after the bin is filled with cargo. The bin also has a hinged back wall which can be partially folded downwardly so as to open the upper portion of the back wall while keeping the lower portion of the back wall closed. This allows luggage or the like to be placed in the bin, when the bin is in the cargo hold, through the upper open portion of the bin, while enabling the lower closed portion of the bin to prevent the inserted luggage from sliding out of the bin. The lower portion of the back wall of the bin is disposed in open ended channels attached to side walls of the bin so that the back wall can be slid out of the channels to open the entire back of the bin so as allow larger items to be inserted into the bin through the open back when the bin is positioned in the cargo hold. The inner surface of the bottom wall or floor of the bin may also be provided with rotatable rollers which allow bulky cargo to be easily slid into the bin while the bin is disposed in the cargo hold of the aircraft. The bin is light in weight so that, when empty, it can easily be inserted into the cargo hold by one person prior to being filled with cargo. The outer surface of the bottom wall or floor of the bin can also be provided with rollers so that a pre-filled bin can be slid into the cargo hold of the aircraft.

REFERENCES:
patent: 2564940 (1951-08-01), Weber
patent: 3294034 (1966-12-01), Bodenheimer et al.
patent: 4221302 (1980-09-01), Kupersmit
patent: 5090335 (1992-02-01), Russell
patent: 5533604 (1996-07-01), Brierton
patent: 5921420 (1999-07-01), Gordon et al.

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