An aircraft operational state monitoring system is provided that includes a module for acquiring a logic state of a plurality of components of the aircraft, the components belonging to airplane systems. The aircraft operational state monitoring system includes a module for determining the operability status of a plurality of macroscopic functions of the aircraft, each macroscopic function being defined independently of the components and airplane systems necessary for the performance of the macroscopic function, the operability status being determined based on logic states of the plurality of components between an operational status and at least one nonoperational status. The aircraft operational state monitoring system includes a display and at least one graphic display management assembly on the display, configured for displaying, on the display, summary indicators of the operability status of the macroscopic functions of the aircraft.

Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

A system is provided. The system includes a translucent display positioned such that a first face is a display face and that a second face is a projection face and at least one projector configured to project an image on the second face of the translucent display. The image is displayed on the first face. The system also includes at least one sensor configured to transmit a signal when triggered and a projector controller in communication with the at least one projector and the at least one sensor. The projector controller is programmed to receive a signal from the at least one sensor and instruct the at least one projector to project at least one image on the translucent display in response to the signal from the at least one sensor.

A photoluminescent aircraft floor path marking system includes at least a flexible track having a housing incorporating a flexible, pliable, photoluminescent portion in which the track is bendable to a radius of 1 m or less and the track has a length of at least 2 m, where the track is pliable such that it can retain a rolled or bent radius. The track may be bendable to a radius of from 0.01 m to 1.0 m or optionally from 0.01 m to 0.5 m. The flexible track may be provided in lengths of from 3 m or greater or greater than 10 m. A flexible protective layer may be provided. The flexible housing may include a holder for the photoluminescent material.

The present invention relates to a method characterized in that one or more passenger waves having a size corresponding to the number of passengers in the settling process, who may be standing at the same time in an aircraft aisle. The invention also relates to a system and equipment capable of performing a method according to the invention, in addition to corresponding computer programs.

Devices, systems and methods for electronic systems that manage an order in which an aircraft is boarded or deplaned are described. An exemplary method includes configuring an onboard computer to execute a script, wherein the script controls an order by which passengers on an airplane are prompted for deplaning, updating the script for a travel segment of the airplane using a first input comprising a passenger information for the travel segment or a second input comprising a travel configuration of the airplane during the travel segment or a third input from onboard crew of the airplane; and controlling onboard electronic equipment of the airplane by executing the script at an end of the travel segment by prompting passengers to deplane the airplane in the order.

An illumination element marks escape routes in vehicles. The illumination element includes a planar substrate, which has: a base surface configured for fastening on a first side; and at least one planar electrical lighting element on a second side. A ratio of a surface area of the base surface to a thickness of the illumination element is greater than 500 mm, and a ratio of the surface area of the base surface to a mass of the illumination element is greater than 100 mm.sup.2/g.

A system for boarding a plurality of passengers onto a passenger vehicle having a plurality of unassigned seats is disclosed. In various embodiments, the system includes a first passenger seat and a first occupancy indicator, the first occupancy indicator associated with the first passenger seat; a second passenger seat and a second occupancy indicator, the second occupancy indicator associated with the second passenger seat; and a processor connected to a communication link and to the first occupancy indicator and to the second occupancy indicator, the processor being configured to receive reservation data from a computing device having a seating reservation application engine installed thereon, the computing device configured for connection to the communication link and the seating reservation application engine configured to activate the first occupancy indicator or the second occupancy indicator.

Disclosed herein are systems and methods for planning a multimodal itinerary. The systems and methods may include receiving a transportation request. The transportation request may include a starting location, a final destination, and an estimated payload data. During a first leg of the multimodal itinerary, an updated payload data may be received. An aerial vehicle may be assigned to a subsequent leg of the multimodal itinerary based on the updated payload data.

An aircraft cabin lighting system comprises one or more cabin lighting units, each cabin lighting unit comprising an emergency exit sign arranged to be electrically illuminated; and one or more luminescent emergency exit signs. The luminescent emergency exit signs are portable, and each comprise an adhesive layer arranged to allow the luminescent emergency exit sign to be adhered to a surface. The signs are arranged to be adhered to a surface in the vicinity of the electrical emergency exit sign in use, and do not require electricity to function.