Patent classifications
B64D11/003
Overhead bin access by boarding pass
A boarding pass may include a barcode with an encoded seat identifier. An overhead storage system may include a barcode reader configured to read the barcode of the boarding pass. The system may determine whether the boarding pass is eligible to access an overhead bin based on the encoded seat identifier. Where the boarding pass is eligible, a signal may be sent to one or more actuators of the overhead bin. Thus, a user may selectively access the overhead bin by the boarding pass.
Remotely locked airline overhead bins
A storage system that includes storage bins and a locking system. The locking system includes an actuation lever, pins that engage with the storage bins, and an elongated link that extends between and connects the actuation lever to the pins. The locking system is selectively movable between a locked position with the actuation lever in a first position and the pins engaged with the storage bins to prevent the storage bins from moving from the closed position, and an unlocked position with the actuation lever in a second position and the pins disengaged from the storage bins to allow the storage bins to move between the open and closed positions.
USE OF FORWARD CLOSET IN SINGLE AISLE AIRCRAFT FOR WHEELCHAIR ACCOMMODATION
A passenger cabin layout including a closet and a closet positionable in a cabin such as an aircraft passenger cabin. The closet includes a first compartment for accommodating a wheelchair, such as an occupied wheelchair, in an unfolded condition, wherein the first compartment is enterable from an aisle in the cabin, such as a branch aisle extending from a door of the aircraft. The closet further includes a second compartment for storing items. In some embodiments, the first compartment is further enterable from a second branch aisle forward of at least one passenger seat, such as a seat row facing the closet. The first compartment is configured to accommodate a personal wheelchair and in some embodiments includes a floor pallet for securing the wheelchair in place in atop the pallet.
Safe vertical take-off and landing aircraft payload distribution and adjustment
Vertical take-off and landing (VTOL) aircraft can provide opportunities to incorporate aerial transportation into transportation networks for cities and metropolitan areas. However, VTOL aircraft can be sensitive to uneven weight distributions, e.g., the payload of an aircraft is primarily loaded in the front, back, left, or right. When the aircraft is loaded unevenly, the center of mass of the aircraft may shift substantially enough to negatively impact performance of the aircraft. Thus, in turn, there is an opportunity that the VTOL may be loaded unevenly if seating, luggage placement, and/or positions of internal components are not coordinated. Among other advantages, dynamically assigning the payloads and adjusting components of the VTOL aircraft can increase VTOL safety by ensuring the VTOL aircraft is loaded evenly and meets all weight requirements; can increase transportation efficiency by increasing rider throughput; and can increase the availability of the VTOL services to all potential riders.
COMPARTMENT SYSTEM FOR A CABIN OF A VEHICLE
A compartment system for a vehicle cabin includes a framework assembly for attachment to a vehicle structure, and a container bin. The framework assembly includes a flat bottom section, a top part and a lateral stiffening element. The bottom section has a rear edge for attachment to the structure and a front edge opposite to the rear edge. The top part is spaced from and parallel to the bottom section front edge. The lateral stiffening element is connected to the top part and the bottom section to create the framework assembly having a front opening between the top part and the bottom section front edge. The container bin has a box-like shape and an open front side. The framework assembly and the container bin are configured to detachably attach the container bin in the framework assembly with the open front side arranged in the framework assembly front opening.
Vehicular seating suite configuration
A vehicular seating suite configuration may include a plurality of vertically stacked seating suites configured to be positioned within a vehicle. Each seating suite may include an elongated generally horizontal seating surface angled away from a longitudinal axis of a vehicle and a generally vertical backrest portion adjacent to a proximal end of the elongated generally horizontal seating surface. The elongated generally horizontal seating surface and the generally vertical backrest portion may be configured to accommodate a person in a sitting position and the elongated generally horizontal seating surface may be configured to accommodate a person in a lying position.
FASTENING APPARATUS FOR FASTENING A FURNISHING COMPONENT TO AN ATTACHMENT STRUCTURE OF AN AIRCRAFT CABIN
An apparatus for fastening a component to an aircraft cabin attachment structure, the attachment structure having a fastening tube with a longitudinal axis. The apparatus has an internally bored sleeve rotatably positionable on the fastening tube and an external thread. A holding body connects to the component and has two spaced-apart limbs and a bearing surface enclosed by the limbs, and on which, an internal thread configured to the sleeve external thread, is arranged. A device fixes the holding body to the threaded sleeve and the fastening tube, the external and internal threads being non-self-locking. When the holding body internal thread presses against the threaded sleeve external thread, the threaded sleeve rotates until the external and internal threads align. The fixing device connects the threaded sleeve to the holding body in a rotationally fixed manner and fixes the holding body transversely with respect to the longitudinal axis.
STOWAGE BIN LIGHTING ASSEMBLY AND METHOD FOR LIGHTING A STOWAGE BIN ASSEMBLY OF A VEHICLE
A stowage bin lighting assembly for mounting to an internal cabin of a vehicle includes a chassis having a plate extending longitudinally between ends. The chassis supports light mount pedestals, wire standoffs, and at least one valance support above the upper surface. The stowage bin lighting assembly includes a light mounted to the light mount pedestals positioned above the plate by the light mount pedestals for providing lighting from the stowage bin assembly to the internal cabin of the vehicle. The stowage bin lighting assembly includes a wire electrically connected to the light to supply power to the light and coupled to at least one of the wire standoffs to control a position of the wire relative to the plate. The stowage bin lighting assembly includes a valance coupled to the valance mount pedestals configured to be coupled to the stowage bin assembly by the valance support.
LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION
An aircraft assembly may comprise an interior aircraft monument, an aircraft structure, and a load absorbing tie rod coupled to the interior aircraft monument and the aircraft structure. The load absorbing tie rod may include an outer cylinder coupled to the aircraft structure, a piston located at least partially within the outer cylinder and coupled to the interior aircraft monument, and a compressed gas located in a volume defined by the piston and the outer cylinder.
Raised passenger seat assemblies
A passenger seat assembly includes a riser attached to an upper surface of a floor of the vehicle, a seat attached to an upper surface of the riser, and at least one shell portion attached to the upper surface of the riser. The riser includes at least one door for accessing an interior volume of the riser. At least a portion of the interior volume of the riser is a luggage storage volume.