A method and system for protecting an aircraft against an incoherent command instruction. The system has a generation unit generating a command instruction transmitted to an evaluation unit that evaluates whether or not the command instruction is incoherent and generates and transmits a validation order if the command instruction is coherent or an arbitration request if not, the arbitration request being transmitted by an arbitration unit, where applicable, to an operator who sends a confirmation response or a cancellation response. The arbitration unit generates and transmits a validation order to an execution unit in the event of receiving a confirmation response and a cancellation order in the event of receiving a cancellation response, the system allowing the execution unit to execute only the command instructions evaluated and confirmed as not being incoherent.

An emergency lighting system (ELS) for an aircraft has a capacitor, at least one of an onboard power system and a ground power unit configured to charge the capacitor, and a light emitting diode (LED) selectively powered by the capacitor.

A system is described that includes a controllable component of an engine configured to regulate fuel flow to the engine, a digital control unit configured to control the engine by at least communicating with the controllable component of the engine, and a protection component configured to disable communication between the digital control unit and the controllable component of the engine. The system further includes an analog control unit configured to control the engine by at least communicating with the controllable component of the engine in response to the protection component disabling communication between the digital control unit and the controllable component of the engine.

In an example, method for locking/unlocking a structure is described. The method includes attaching a first end of a pawl to a support assembly, wherein the pawl comprises a shape memory alloy (SMA) element configured to transition between a first configuration and a second configuration, and wherein the pawl is attached to the support assembly such that a second end of the pawl is movable between a locked position that prevents a rotatable shaft from rotating and an unlocked position that allows the rotatable shaft to rotate, activating the SMA element, thereby causing the SMA element to take on the first configuration and move the second end of the pawl to the locked position, and deactivating the SMA element, thereby causing the SMA element to take on the second configuration and move the second end of the pawl from the locked position to the unlocked position.

Embodiments described herein provide for flight crew areas onboard aircraft that are only accessible via a door to the exterior of the aircraft. The flight crew areas may be included within the same section of the fuselage of the aircraft as the aircraft cabin, or may be included within a different section of the fuselage. One embodiment comprises an aircraft that includes an aircraft cabin and a flight crew area. The aircraft cabin is configured for passenger seating. The flight crew area includes a door opening to an exterior of the aircraft that is sized for a person, and a cockpit that is only accessible by a flight crew via the door.

A method is provided that includes generating a visual environment for interactive development of a machine learning (ML) model. The method includes accessing observations of data each of which includes values of independent variables and a dependent variable. The method includes performing an interactive feature construction and selection in which select independent variables are selected as or transformed into a set of features for use in building a ML model to predict the dependent variable. The method includes building the ML model using a ML algorithm, the set of features, and a training set produced from the set of features and observations of the data. And the method includes outputting the ML model for deployment to predict the dependent variable for additional observations of the data.

The present disclosure relates to optimisation of a cold nozzle, or bypass exit area, for a gas turbine engine, in particular for a geared turbofan gas turbine engine. Example embodiments include a method of optimising a geared turbofan gas turbine engine for an aircraft, the method comprising: determining expected service parameters for the aircraft, the expected service parameters including an expected range of travel for the aircraft; selecting components for the geared turbofan gas turbine engine to define a first smaller cold nozzle area if the range of travel is within a first smaller range and to define a second larger cold nozzle area if the range of travel is within a second larger range.

An unmanned aerial vehicle (UAV) including a detection device configured to detect that a disassembly operation has been performed on the UAV and a controller configured to determine whether the disassembly operation is an unauthorized disassembly operation, and prohibit the UAV from moving in response to the disassembly operation being the unauthorized disassembly operation, where the detection device is communicatively connected to the controller.

Systems and methods for illuminating an airplane cabin using a light strip comprising a plurality of spectrally-tuned illuminators within a housing are provided. The illuminators include a first visible light illuminator and an infrared illuminator. The light strip is disposed to provide indirect infrared illumination of the cabin via diffuse reflection from a surface of the cabin (wash lighting) from a shrouded location. The illuminators include light emitting diodes (LEDs), and include white and some combination of red, yellow, green, and blue. A controller varies intensities of each illuminator, to emphasize or de-emphasize various colors or infrared illumination throughout an interior of the airplane cabin.

A vehicle network system is configured to detect unauthorized intrusions by a passenger-owned device, and to identify the passenger-owned device based at least in part on stored information representative of network communications. The vehicle network system can be further configured to determine a position of the intruding passenger-owned device within a passenger area of the vehicle and to obtain a name and/or camera image of a passenger associated with the device. The position of the intruding device can be identified based at least in part on communications between the intruding device and one or more network-access devices distributed throughout the passenger area.