Abstract: A forward concave trapezoidal seating system and methods are presented. Trapezoidal seats comprise a front side smaller than a rear side. The trapezoidal seats are aligned in a forward arc from a straight seat to a most-angled seat. A straight side of the straight seat is configured to substantially align with a center line of an aircraft fuselage. A most-angled side of the most-angled seat is angled inboard relative to the straight side, and the most-angled seat is outboard of the straight seat. A side unit is coupled to the most-angled side and supports the trapezoidal seats.

Abstract: A forward concave trapezoidal seating system and methods are presented. Trapezoidal seats comprise a front side smaller than a rear side. The trapezoidal seats are aligned in a forward arc from a straight seat to a most-angled seat. A straight side of the straight seat is configured to substantially align with a center line of an aircraft fuselage. A most-angled side of the most-angled seat is angled inboard relative to the straight side, and the most-angled seat is outboard of the straight seat. A side unit is coupled to the most-angled side and supports the trapezoidal seats.

Abstract: A forward concave trapezoidal seating system and methods are presented. Trapezoidal seats comprise a front side smaller than a rear side. The trapezoidal seats are aligned in a forward arc from a straight seat to a most-angled seat. A straight side of the straight seat is configured to substantially align with a center line of an aircraft fuselage. A most-angled side of the most-angled seat is angled inboard relative to the straight side, and the most-angled seat is outboard of the straight seat. A side unit is coupled to the most-angled side and supports the trapezoidal seats.

Abstract: A method and apparatus comprising a plurality of seating systems and a frame for use in a passenger aircraft. A first seating system in the plurality of seating systems may have different dimensions from a second seating system in the plurality of seating systems. A frame may be configured to be connected to the plurality of seating systems.

Abstract: An accessible storage, rest, or work accommodation for an aircraft having a passenger cabin with a ceiling and a crown space above the ceiling, comprising: (a) a compartment in the crown space having at least one bunk; (b) an aperture in the passenger cabin ceiling, connecting the compartment to the passenger cabin; (c) a landing positioned below a floor of the compartment, below at least a portion of the aperture, inside the passenger cabin module; and (d) stairs or a ladder leading from the landing to a floor of the passenger cabin.

Abstract: A method and apparatus comprising a plurality of seating systems and a frame for use in a passenger aircraft. A first seating system in the plurality of seating systems may have different dimensions from a second seating system in the plurality of seating systems. A frame may be configured to be connected to the plurality of seating systems.

Abstract: A method and apparatus comprising a plurality of seating systems and a frame for use in a passenger aircraft. A first seating system in the plurality of seating systems may have different dimensions from a second seating system in the plurality of seating systems. A frame may be configured to be connected to the plurality of seating systems.

Abstract: An accessible storage, rest, or work accommodation for an aircraft having a passenger cabin with a ceiling and a crown space above the ceiling, comprising: (a) a compartment in the crown space having at least one bunk; (b) an aperture in the passenger cabin ceiling, connecting the compartment to the passenger cabin; (c) a landing positioned below a floor of the compartment, below at least a portion of the aperture, inside the passenger cabin module; and (d) stairs or a ladder leading from the landing to a floor of the passenger cabin.

Abstract: A forward concave trapezoidal seating system and methods are presented. Trapezoidal seats comprise a front side smaller than a rear side. The trapezoidal seats are aligned in a forward arc from a straight seat to a most-angled seat. A straight side of the straight seat is configured to substantially align with a center line of an aircraft fuselage. A most-angled side of the most-angled seat is angled inboard relative to the straight side, and the most-angled seat is outboard of the straight seat. A side unit is coupled to the most-angled side and supports the trapezoidal seats.

Abstract: A method and apparatus comprising a plurality of seating systems and a frame for use in a passenger aircraft. A first seating system in the plurality of seating systems may have different dimensions from a second seating system in the plurality of seating systems. A frame may be configured to be connected to the plurality of seating systems.

Abstract: A system and method for knowledge based development of interior models for configurable spaces, including passenger vehicles includes a database containing rules and parameters, a computer-aided design system, a user interface, and programmatic logic allowing aspects of the vehicle to be automatically changed upon a change initiated by a user, to maximize space and maintain compliance with the rules and parameters.

Abstract: An overhead rest area is provided in the crown of an aircraft above the ceiling for the main passenger cabin. A permanent access stairway is provided at one end of the overhead rest area, and an emergency escape apparatus is provided at another location of the rest area. The emergency escape apparatus can include a slide swingable between a closed position in which its underside forms a smooth continuation of the ceiling of the passenger cabin and a downward swung open position providing an escape route from the overhead rest area to the passenger cabin.