The present disclosure provides aircraft high-load landing event detection, classification and maintenance guidance methods, and relates to the technical field of aircraft high-load landing event detection. The present disclosure collects complete and accurate landing data online during an aircraft…
An aircraft sensing system includes a power and communications module, a sensor module in optical communication with the power and communications module, the sensor module being disposed in an at least partially enclosed space within the aircraft, and at least one gas sensor in communication with…
A method of providing contextual display modes for a vertical takeoff and landing (VTOL) vehicle including obtaining aircraft flight information including a current position and altitude; retrieving vertiport information for a vertiport at the current position of the aircraft; displaying, to one or…
An aircraft tire monitoring system including a processor, and a data carrier having machine readable instructions that, when executed, cause the processor to, based on a plurality of sets of values indicative of tire parameters of aircraft tires, each set of values corresponding to an aircraft…
An autonomous impact detection device includes at least one impact detector; at least one wireless transmission device configured to transmit the information collected by the impact detector; at least one energy storage device configured to supply the impact detector and the wireless transmission…
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…
This device (10) for assisting in the piloting of a vehicle, in particular an aircraft, comprises a display surface (16) for displaying images and a display management assembly for images intended to be displayed on the display surface (16) in superposition with a vision of an external landscape…
A graphical in-flight message representation system comprises a sensor configured to measure a characteristic of a flight of an aircraft and a communication device configured to send and receive in-flight messages. An in-flight message is a message communicated during the flight of the aircraft…
Systems and methods for enhanced display of obstacles in a combined vision display are provided. The system comprises a display unit and an enhanced vision system configured to generate first signals representative of enhanced vision images. Data storage device contains obstacle data representative…
The system (20) has a measurement device (40) measuring torque exerted on an upstream portion (11) of a drive train (10) when mounted. Another measurement device (50) measures speed of rotation of a gas generator (6) of a turboshaft engine (5) when mounted. A processor unit (25) is connected to the…
A method for displaying an attitude of an aircraft (20) comprises the steps of: receiving a roll angle, a pitch angle and a yaw angle of the aircraft (20); generating a display image (14) indicating the roll angle, the pitch angle and the yaw angle; and displaying the display image (14) on a…
The present disclosure relates to an inertia measurement unit for an unmanned aircraft, which comprises a housing assembly, a sensing assembly and a vibration damper. The vibration damper comprises a first vibration-attenuation cushion; and the sensing assembly comprises a first circuit board, a…
The system (10) has a synthetic environment generating assembly (38) including a database (45B) with topographical information relative to a terrain. A display management assembly (42) controls display of relief lines (304) representative of the terrain on a region of a display (36), without…
The system (10) has an assembly (38) for dynamic generation of synthetic images. A management assembly (42) manages a graphical interface of a display (36), so as to control the display of the synthetic images on a region (60) of the display in certain configuration changes of an aircraft, and on…
The method involves performing a check to verify whether motion of an aircraft is consistent with a guidance setpoint relating to a flight parameter. A part of a scale e.g. speed scale (14), starting from a current value of the flight parameter is displayed in the direction of motion of the…
Methods and systems are provided for displaying visually distinguishing characteristics if an aircraft is below a minimum altitude or beyond a maximum distance when executing a procedure turn. A procedure turn icon (208), an aircraft icon (202) indicating the aircraft's present location…
A method (100) of determining a turbulent condition in an aircraft (10) with a handheld device where the handheld device has at least one of a gyroscope, seismometer, and an accelerometer (42) where the method includes receiving (102) an output from the at least one of the gyroscope, seismometer…
The present application relates to a system and method for providing real-time indications of economic impact of aircraft operations to an aircraft operator. The system and method allow the aircraft operator to reduce economic impact during flight of the aircraft. Such an analysis and cue to the…
The method involves characterizing a flight phase of an aircraft. A determination is made whether the aircraft is authorized to lose altitude (S113). A prohibited flight envelope is determined (S114). A set of prohibited vertical speeds of the aircraft for given altitudes is defined according to…
A computer apparatus and method to determine aircraft fuel mileage performance. The computer apparatus including a memory (120) and a processor (115) disposed in communication with the memory (120) and configured to issue a plurality of instructions stored in the memory (120). The instructions…
An FPM (30) and a target air attitude angle indication (32) are displayed on a PFD (10) which is an integrated instrument. The target air attitude angle indication (32) is an index showing a target angle of attack and a target air attitude angle, said target angle of attack being an angle of attack…
The invention relates to systems and methods for displaying flight information representative of a deviation from a specified four-dimensional flight path. Particularly, but not exclusively, the invention relates to a cockpit display for enabling pilots to arrive at a particular location at a…
Improved multifunction probe having circumferentially spaced pairs of sensing parts (22,24). An elongate, conically shaped probe element is rotatable about an axis. A central pressure port (20) picks up dynamic pressure. A pair of inner pneumatic ports (22,24) in slit shape is symmetrically…