Aircraft interior configuration
AssigneeBombardier Inc.
InventorsBruce Malek, Louis Joseph Gagnon-Seguin, Bruno Miron, Philippe Andre Eugene Erhel, Tim Michael Fagan
Life of this patent
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Abstract
An aircraft interior configuration includes a first passageway extending along a longitudinal axis of a fuselage of the aircraft and a second passageway extending along the longitudinal axis. A transitional region is disposed between the first passageway and the second passageway. The transitional region extends perpendicularly to the longitudinal axis, between starboard and port sides of the aircraft. The transitional region is configurable from at least a first configuration to at least a second configuration.
Claims7
An interior configuration for an aircraft, comprising:
- a first passageway;
- a second passageway;
- and
- a transitional area disposed between the first passageway and the second passageway;
- wherein the transitional area is configurable from at least a first configuration to at least a second configuration,
- wherein the transitional area comprises:
- a first group of three seats disposed at a fore side of the transitional area, and
- a second group of three seats disposed at an aft side of the transitional area,
- wherein the first group of seats and the second group of seats face one another,
- wherein two of the three seats in the first group of seats are disposed next to one another adjacent a first side of the aircraft and are separated by the first passageway from a third of the three seats, and
- wherein two of the three seats in the second group of seats are disposed next to one another adjacent to a second side of the aircraft and are separated by the second passageway from a third of the three seats.
Dependencies are inferred from the claim text.