A vehicle includes an interior cabin including a floor and a ceiling. A deployable seat assembly is moveably coupled to the ceiling. The deployable seat assembly is moveable between a stowed position in which at least a portion of the deployable seat assembly is stowed within a stowage space within the ceiling, and a deployed position in which the deployable seat assembly extends between the ceiling and the floor.

A support structure for a flight attendant seat, the support structure having supporting elements arranged at an upper and a lower end of the support structure. The supporting elements connect the support structure to an aircraft structure via fastening points, the support structure having receiving elements for receiving the flight attendant seat. The support structure has at least two substantially vertical elements and at least one substantially horizontal element. The vertical elements have at least one upper and one lower end, the supporting elements being attached to respective ends of the vertical elements and forming lattice struts. The support elements are designed to be connected to the aircraft structure at at least two attachment positions, at least two upper and two lower fastening points being selectable in their respective attachment position to the aircraft structure, at least one cabin element being adaptively attached to the support structure.

A vehicle includes an interior cabin including a floor and a ceiling. A deployable seat assembly is moveably coupled to the ceiling. The deployable seat assembly is moveable between a stowed position in which at least a portion of the deployable seat assembly is stowed within a stowage space within the ceiling, and a deployed position in which the deployable seat assembly extends between the ceiling and the floor.

A support structure for a flight attendant seat, the support structure having supporting elements arranged at an upper and a lower end of the support structure. The supporting elements connect the support structure to an aircraft structure via fastening points, the support structure having receiving elements for receiving the flight attendant seat. The support structure has at least two substantially vertical elements and at least one substantially horizontal element. The vertical elements have at least one upper and one lower end, the supporting elements being attached to respective ends of the vertical elements and forming lattice struts. The support elements are designed to be connected to the aircraft structure at at least two attachment positions, at least two upper and two lower fastening points being selectable in their respective attachment position to the aircraft structure, at least one cabin element being adaptively attached to the support structure.

A turbulence reduction seat device includes an orb that is positioned within an aircraft and which has an entrance to facilitate a passenger to enter the orb. A chair is positioned within the orb to facilitate the passenger to sit on the chair when the passenger enters the orb. A door is slidably attached to the orb for opening and closing the entrance. A pair of shock absorbers is each movably attached to the orb. Each of the pair of shock absorbers is mounted to a respective one of a floor and a ceiling of the aircraft to reduce movement of the orb when the aircraft encounters turbulence. A plurality of display screens is each integrated into the outer wall of the orb and each of the display screens displays indicia to facilitate the passenger to view the indicia.

A turbulence reduction seat device includes an orb that is positioned within an aircraft and which has an entrance to facilitate a passenger to enter the orb. A chair is positioned within the orb to facilitate the passenger to sit on the chair when the passenger enters the orb. A door is slidably attached to the orb for opening and closing the entrance. A pair of shock absorbers is each movably attached to the orb. Each of the pair of shock absorbers is mounted to a respective one of a floor and a ceiling of the aircraft to reduce movement of the orb when the aircraft encounters turbulence. A plurality of display screens is each integrated into the outer wall of the orb and each of the display screens displays indicia to facilitate the passenger to view the indicia.

A seat beam for a rotary-wing aircraft adapted for receiving seat posts of a seat bench device, including a first seat beam end; a second seat beam end; and a seat beam body connecting both. A link with a link working line is arranged at the first seat beam end and includes: a link-beam fixation that is attached to the seat beam body and rotatable around a first link rotational axis that is perpendicular to the seat beam extension axis, and a first seat beam fixation that is connected to the link-beam fixation and adapted for being attached to the airframe attachment point such that the first seat beam fixation is rotatable around a second link rotational axis that is parallel to the first link rotational axis.

A transportation system includes a body, a plurality of propulsion units, and a control unit. The body defines an interior space. The plurality of propulsion units are mounted on the body. Each of the plurality of propulsion units includes a thrust-generating mechanism and a power source. The thrust-generating mechanism is configured to produce a propulsion force. The control unit is operatively coupled to each of the plurality of propulsion units. The transportation system further includes a housing unit or a pilot attachment disposed within the interior space. The housing unit or the pilot attachment is suspended by at least one connecting element or a suspension mechanism which is configured to dampen and/or stabilize and/or actively adjust movement relative to the body.

A motor vehicle includes a structural element and a seat having at least two separate and independent seat portions, each of the seat portions being configured to support a part of a user's body and being independently coupled to the structural element in a movable manner relative to the structural element with three degrees of freedom including two translations in a plane along respective orthogonal axes and a rotation around a further axis orthogonal to said plane.

Systems and methods for a vehicle containing a structural column are disclosed. The vehicle includes: a structural column positioned between a first and second interior surface of the vehicle. The vehicle may further include a seating assembly attached to a first surface of the structural column, wherein the seating assembly comprises a seating surface and a seat back. In addition, the structural column may be configured to redistribute a force load to at least one other structural component in the vehicle. Other aspects are described and claimed.