Abstract: An aircraft sound diagnostic method includes a step of measurement of acoustic signals by a plurality of microphones mounted at different positions inside the aircraft, a step of recording of the measured acoustic signals, a computation step which generates a sound mapping on the basis of the measured acoustic signals, a step of comparison of the sound mapping and a reference mapping and a step of transmission of the comparison to a user device. The method makes it possible to track the trending of an abnormal noise or of an abnormal noise level and assist in determining the context thereof. An aircraft sound diagnostic device for implementing the method is also described.

Abstract: A CMOS image sensor including: an array of M×N pixels, the pixels of a same column being connected to a same output track, each pixel including a photodiode, a sense node, a transfer transistor, a reset transistor, and a read circuit; and a test circuit including an assembly of N elementary reference cells respectively connected to the N output tracks of the sensor, each cell including a resistor, a sense node, a transfer transistor, a reset transistor, and a read circuit, the N resistors being series-connected between first and second nodes of application of a reference voltage.

Abstract: A CMOS image sensor including: an array of M×N pixels, the pixels of a same column being connected to a same output track, each pixel including a photodiode, a sense node, a transfer transistor, a reset transistor, and a read circuit; and a test circuit including an assembly of N elementary reference cells respectively connected to the N output tracks of the sensor, each cell including a resistor, a sense node, a transfer transistor, a reset transistor, and a read circuit, the N resistors being series-connected between first and second nodes of application of a reference voltage.

Abstract: The invention relates to a ceiling component which is formed by a curved panel and has a support which supports a layer of sound-proofing and heat insulating material. The support is made in one piece and is constituted by a metal sheet whose edges are bent back on itself and then to form a flange projecting from one surface of said panel. The bent edges alone provide the rigidity necessary for the panel without requiring the use of ribs and girders.