Abstract: A device and system for transferring information from an avionics system of an aircraft to an independent computer. The device can be embedded onboard an aircraft for transferring information arising from an avionics system from the aircraft to a computer independent of the avionics system. The device includes at least one radiofrequency receiver configured to receive information which arises from the avionics system and is emitted destined for the ground or another aircraft, at least one transmitter, and a processing unit to command the transmission by the transmitter, to the computer, of at least some of the information received by the radiofrequency receiver.

Abstract: A device and system for transferring information from an avionics system of an aircraft to an independent computer. The device can be embedded onboard an aircraft for transferring information arising from an avionics system from the aircraft to a computer independent of the avionics system. The device includes at least one radiofrequency receiver configured to receive information which arises from the avionics system and is emitted destined for the ground or another aircraft, at least one transmitter, and a processing unit to command the transmission by the transmitter, to the computer, of at least some of the information received by the radiofrequency receiver.

Abstract: An aircraft comprising a landing gear, having at least one wheel rotatably driven by an electric motor, and a motor control system. The control system comprises a control panel, presenting a first control configured to deliver a torque or power value to the motor along a direction of forward travel of the aircraft and second control configured to deliver a taxiing speed value along a direction of reverse travel, a control unit connected to the control panel and to the electric motor, presenting a first arrangement configured to control, in torque or power, the motor according to the value delivered by the first control, and a second arrangement configured to control, in speed, the motor according to the taxiing speed value delivered by the second control, and a speed sensor configured to measure the taxiing speed of the aircraft, and to transmit this speed information to the control unit.

Abstract: A device to support a headset along a wall of a vehicle, that includes a hook that has a base to receive a headband of the headset, with this base being intended to be fastened transversally to the wall by its back and being integral at the opposite front with an external element for holding the headband on the base. The hook has on opening between the back and the external element with a width I at least equal to the width of the headband, permitting the passage of the headband toward the base or during removal from the base. The aforementioned device has an anti-release element blocking the opening over a width at least large enough to prevent the passage of the headband through the opening. This anti-release element can be displaced by manual action directly on the anti-release element or through the headset into a release position to allow the passage of the headband.

Abstract: A device to support a headset along a wall of a vehicle, that includes a hook that has a base to receive a headband of the headset, with this base being intended to be fastened transversally to the wall by its back and being integral at the opposite front with an external element for holding the headband on the base. The hook has on opening between the back and the external element with a width I at least equal to the width of the headband, permitting the passage of the headband toward the base or during removal from the base. The aforementioned device has an anti-release element blocking the opening over a width at least large enough to prevent the passage of the headband through the opening. This anti-release element can be displaced by manual action directly on the anti-release element or through the headset into a release position to allow the passage of the headband.