Triple-fuselage aircraft and families of aircraft of said type

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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Details

C244S013000

Reexamination Certificate

active

10504318

ABSTRACT:
A method of air transport includes improved reliability and safety of passengers and cargo transported by an aircraft having three fuselages. The method includes locating a cockpit of the aircraft at a forward portion of the first fuselage and isolating the cockpit from a remaining portion of the aircraft. The cockpit is then shielded and independently pressurized from the remainder of the aircraft by controls housed in the cockpit. The method further includes distributing passengers and cargo among the three fuselages, such as by locating dangerous or suspicious passengers or cargo in the second and third fuselages away from the cockpit. Also, dangerous or suspicious passengers or cargo may be located in the second and third fuselages and, thereby, isolated from the remaining passengers and cargo.

REFERENCES:
patent: D112834 (1939-01-01), De Seversky
patent: 2224641 (1940-12-01), Burnelli
patent: D130651 (1941-12-01), Silverstein
patent: D158736 (1950-05-01), Frank
patent: D188226 (1960-06-01), Jones
patent: 3348513 (1967-10-01), Dishart
patent: D211612 (1968-07-01), Asis
patent: 3738595 (1973-06-01), Bouchnik
patent: 3913871 (1975-10-01), Miller
patent: 3949958 (1976-04-01), Richter
patent: 4057205 (1977-11-01), Vensel
patent: 5425515 (1995-06-01), Hirose
patent: 6666406 (2003-12-01), Sankrithi et al.
patent: 6844817 (2005-01-01), Gleine
patent: 1314035 (1993-03-01), None
patent: 297 13 042 (1998-03-01), None
patent: 1 167 183 (2002-01-01), None
patent: 2 623 468 (1989-05-01), None
WO 90/13479 published Nov. 15, 1990.
WO 99/52759 published Oct. 21, 1999.

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