The invention provides aeromedical ambulance equipment. In some embodiments, the equipment includes a module base comprising a mount assembly having an unlocked configuration and a locked configuration. The mount assembly preferably can be adjusted between the unlocked and locked configurations by a tool-free operation. In addition, certain embodiments provide a module base having an advantageous system for releasably locking a stretcher onto the module base.

A cabinet comprising at least one screen allowing display of data necessary for a flight-control of an aircraft connected to at least one avionics module for management of the data. The screen at least partially forms one of the sides of the cabinet and the module or modules are installed inside the cabinet. The cabinet has a base allowing the screen or screens to be placed at a desired height. As a result, a length of cable between screen and avionics modules is reduced to a minimum.

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.

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.

Vehicles and multi-place dining tables for vehicles are provided. In one example, the vehicle includes a vehicle structure having a first sidewall, a second sidewall, and a floor disposed therebetween. The vehicle structure at least partially surrounds an interior area that has an aisleway extending therethrough. A multi-place dining table is disposed in the interior area and includes a first table section that is disposed between the first sidewall and the aisleway. The first table section includes a first tabletop. A second table section is disposed between the second sidewall and the aisleway and includes a second tabletop. The second tabletop is movable between a stowed position where the first and second tabletops are spaced apart from each other by at least the aisleway and a deployed position where the second tabletop extends across the aisleway and is coupled to the first tabletop.

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.

A frame member, a monument for a vehicle, and a vehicle are provided. The frame member includes an extrusion that has a spar with first and second opposing surfaces and first and second opposing ends. The spar includes a first retention lip extending from the first planar surface along the first end at an acute angle relative to the first planar surface. The spar includes a rub strip protrusion extending from the first planar surface between the first and second ends. The rub strip protrusion includes a third end and a second retention lip extending from a third surface facing the first retention lip. The second retention lip and the third surface form an acute angle. The extrusion also includes at least two panel protrusions extending from the second planar surface of the spar. A rub strip can include retention tabs with outward-facing notches that engage the first and second retention lips.

A room for an aircraft cabin is a hollow box shaped room and installed in the aircraft cabin. The room includes a floor wall portion that is configured to face a seat of the cabin, a side wall portion that extends from the floor wall portion in a direction away from the seat and has an opening portion for entering and leaving the room, a ladder portion extending in a direction toward the seat from a periphery of the opening portion, and a ceiling wall portion that extends to couple the floor wall portion and the side wall portion and has an engagement structure with an inner wall of the cabin.

An aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems is presented. The present disclosure includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.

An aircraft interior structure may include a primary monument, an auxiliary monument, and a passenger seating section. The primary monument may include one or more storage compartments and a primary panel configured to actuate between a primary panel stowed position and a primary panel deployed position. The auxiliary monument may be spaced a select distance from the primary monument across a floor area of an aircraft cabin, and may include an auxiliary panel configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position. The passenger seating section may include a footwell at least partially within the primary monument and proximate to the one or more storage compartments. The footwell may correspond to an aircraft seat. The aircraft seat may be configured to form a bed surface with at least a portion being within the footwell when the aircraft seat is in a lie-flat position.