Passenger aircraft with increased passenger capacity

Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation

Patent

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Details

2441181, 244120, B64C 0106, B64C 0110, B64C 0120

Patent

active

057526737

ABSTRACT:
It is a problem in conventional aircraft having a fuselage of substantially circular cross-section, that a conventional lower deck would have an insufficient standing height for passengers if the lower deck were to be equipped as a passenger cabin space including seats, sleeping cabins, or other passenger service facilities. In the present aircraft, the lower deck floor (2, 2') is depressed or dropped at least in a certain area (14) that will form an aisle (16), so that the free height of the lower deck in the area of the depressed floor provides at least the normal standing height (HS) for a person. A module (15, 15') containing passenger service facilities is arranged in the lower deck area at least to one side of the depressed floor area. A modular construction provides a great flexibility and convenience in reconfiguring a lower deck from a cargo hold configuration to a passenger cabin configuration and vice versa.

REFERENCES:
patent: Re32176 (1986-06-01), Vernon
patent: 504615 (1893-09-01), Pope
patent: 3517899 (1970-06-01), Vernon
patent: 4066227 (1978-01-01), Buchsel
patent: 4854245 (1989-08-01), Platzer
patent: 4925132 (1990-05-01), Zider
patent: 5474260 (1995-12-01), Schwertfeger et al.
patent: 5496000 (1996-03-01), Mueller
Crashsimulationsrechnungen und Bauteilidealisierung fur einen Luftfahrzeugunterboden (Crash Simulation Calculations and Component Idealization for an Aircraft Subfloor Section) Z. Flugwiss. Weltraumforschung 11, (1987) pp. 221-229.

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