An aircraft emergency lighting system is disclosed. This emergency lighting system may include interior emergency lighting, interior ambient light sensors, exterior emergency lighting, and exterior ambient light sensors. The interior emergency lighting, the exterior emergency lighting, or both, may be controlled based upon an input of the interior ambient light condition (e.g., using an output from at least one of the interior ambient light sensors) and based upon an input from at least one of the exterior ambient light sensors.

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 passenger unit for use on-board a passenger vehicle (e.g., an in-flight entertainment device) includes a display, a memory storing a passenger unit identifier, a network interface, and a connector configured to physically couple to a connector on a mounting unit, where the mounting unit is installed on, or proximate to, a particular seat of a plurality of seats on-board the passenger vehicle. The passenger unit also includes a controller configured to obtain a seat location code of the particular seat from the mounting unit, and to cause the seat location code and the passenger unit identifier to be transmitted, via the network interface, to a server on-board the passenger vehicle. The server is configured to map the passenger unit to the particular seat using the seat location code and the passenger unit identifier.

A method of altering propulsor output when powering an electronic aircraft includes calculating a power demand of each propulsor of the plurality of propulsors for at least a future phase of flight, wherein each propulsor is powered by an electrical energy source of a plurality of electrical energy sources. The method includes measuring an electrical parameter of each energy source, calculating a power-production capability of each energy source as a function of the electrical parameter. The method includes identifying at least a compromised energy source of the plurality of energy sources, notifying, by a notification unit, a user of the at least a compromised energy source, and adjusting, as a function of the user notification, the power output from the plurality of energy sources to the plurality of propulsors for a current phase of flight as a function of the power-production capability and the power demand.

A passenger cabin monitoring system includes infrared cameras disposed in respective passenger rest compartments, a flight attendant information system including at least one display and at least one speaker, and a computing device in communication with the infrared cameras and the flight attendant information system. The computing device is configured to detect a temperature of a portion of passenger rest compartment based on one or more thermal images generated by a respective infrared camera of the passenger rest compartment. The computing device is further configured to compare the temperature of the portion of the passenger rest compartment with a predetermined critical temperature and provide an audible alert and/or a visual alert via the flight attendant information system to indicate a critical status of the passenger rest compartment when the temperature of the portion of the passenger rest compartment is above the predetermined critical temperature.

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 seatbelt detection system detects seatbelt use in each seat of a passenger aircraft to produce safety-compliance data. A computer system, which is communicatively coupled to the seatbelt detection system, generates a time-based record of the safety-compliance data. The computer system can use the time-based record to adapt cabin operations policy, including cabin temperature, cabin lighting, illumination of seatbelt signs, scheduling of meal or drink service, timing of inflight announcements, or the availability of in-flight entertainment.

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.

A boarding guidance system includes a beacon (202A) associated with a passenger seat (400A). The beacon is configured to communicate (506) with a passenger guiding device (102) and determine a distance between the passenger guiding device and the passenger seat. When the passenger guiding device is a predetermined distance from the passenger seat, the beacon provides an indication. The beacon further alter at least one characteristic of the indication based on the distance between the passenger guiding device and the passenger seat.

An aircraft emergency lighting system is disclosed. This emergency lighting system may include interior emergency lighting, interior ambient light sensors, exterior emergency lighting, and exterior ambient light sensors. The interior emergency lighting, the exterior emergency lighting, or both, may be controlled based upon an input of the interior ambient light condition (e.g., using an output from at least one of the interior ambient light sensors) and based upon an input from at least one of the exterior ambient light sensors.