Abstract: A device for an aircraft having at least one first communication with an air traffic control center. The device establishes a second communication with a remote assistance center and performs a first mixing of audio signals from the first communication or communications and of audio signals from the second communication and transmits the result to the pilot. The device also performs a second mixing of audio signals from the first communication or communications and of audio signals from the pilot and transmits the result to the remote assistance center by using the second communication. The device performs a relaying of commands received via the second communication to devices of the aircraft. An operator in the remote assistance center listens to the exchanges between the pilot and the air traffic control center and can exchange with the pilot and relieve him or her of certain tasks.

Abstract: A device for an aircraft having at least one first communication with an air traffic control center. The device establishes a second communication with a remote assistance center and performs a first mixing of audio signals from the first communication or communications and of audio signals from the second communication and transmits the result to the pilot. The device also performs a second mixing of audio signals from the first communication or communications and of audio signals from the pilot and transmits the result to the remote assistance center by using the second communication. The device performs a relaying of commands received via the second communication to devices of the aircraft. An operator in the remote assistance center listens to the exchanges between the pilot and the air traffic control center and can exchange with the pilot and relieve him or her of certain tasks.

Abstract: A communication system installed in an aircraft, the system comprising a transmitter configured to transmit audio data signals to a ground recording station provided with memories for the recording of the data, at least one audio assembly per pilot of the aircraft for transmitting and receiving audio data signals, a CVR recorder and an audio management unit connected to each audio assembly, to the CVR recorder and to the transmitter, the unit being configured to transfer the audio signals received or transmitted by an audio assembly to the transmitter and to the CVR recorder. Each audio assembly comprises an in-use detection system connected to the transmitter and configured to transmit to the transmitter a signal representative of the in-use state of the audio assembly. The transmitter transmits the audio data signals received from the management unit to the ground recording station on reception of the signal.

Abstract: A communication system installed in an aircraft, the system comprising a transmitter configured to transmit audio data signals to a ground recording station provided with memories for the recording of the data, at least one audio assembly per pilot of the aircraft for transmitting and receiving audio data signals, a CVR recorder and an audio management unit connected to each audio assembly, to the CVR recorder and to the transmitter, the unit being configured to transfer the audio signals received or transmitted by an audio assembly to the transmitter and to the CVR recorder. Each audio assembly comprises an in-use detection system connected to the transmitter and configured to transmit to the transmitter a signal representative of the in-use state of the audio assembly. The transmitter transmits the audio data signals received from the management unit to the ground recording station on reception of the signal.

Abstract: The method of communication between an airplane and the ground, the aircraft communicates by radiowaves with the ground via at least one satellite and in a frequency band extending from 5030 MHz to 5091 MHz, bounds included, using a WiMax type transmission standard. The invention also provides an on-board communications terminal for an aircraft, suitable for communicating by radiowaves with the outside of the terminal in a frequency band extending from 5030 MHz to 5091 MHz, bounds included, in application of a WiMax type transmission standard.

Abstract: Radiocommunication system for aircraft. The radiocommunication system (S1) comprises a single box and, integrated into this single box, at least one single main interface module (7), which is formed in such a way as to carry out the processing of the interfaces of all the radiocommunication means (3 to 6) of said radiocommunication system (S1).

Abstract: The method of communication between an airplane and the ground, the aircraft communicates by radiowaves with the ground via at least one satellite and in a frequency band extending from 5030 MHz to 5091 MHz, bounds included, using a WiMax type transmission standard. The invention also provides an on-board communications terminal for an aircraft, suitable for communicating by radiowaves with the outside of the terminal in a frequency band extending from 5030 MHz to 5091 MHz, bounds included, in application of a WiMax type transmission standard.

Abstract: Radiocommunication system for aircraft. The radiocommunication system (S1) comprises a single box and, integrated into this single box, at least one single main interface module (7), which is formed in such a way as to carry out the processing of the interfaces of all the radiocommunication means (3 to 6) of said radiocommunication system (S1).

Abstract: This invention relates to a distress beacon comprising at least one transmitter stage (22) connected to an antenna, and one receiver stage (21) locked onto a distress frequency connected to the said antenna (25), and a detection module connected to the output of this receiver stage (21) capable of activating a signal in order to indicate an alarm. This invention also relates to a device for implementing this process.

Abstract: This invention relates to an aircraft using such an antenna comprises: a structural element (8) that is conducting in the operating frequency band of the antenna, with size equal to at least one quarter of the wave length along the polarization direction of the electromagnetic wave for the minimum frequency of this frequency band, and comprising a cutout forming a cavity (9); a removable exciting element (10) placed in this cavity that acts as an exciter of this cavity (9); and a metallization that is electrically conducting at the operating frequencies of the antenna providing metallization between the exciting element (10) and the structural element (8).

Abstract: This invention relates to a distress beacon comprising at least one transmitter stage (22) connected to an antenna, and one receiver stage (21) locked onto a distress frequency connected to the said antenna (25), and a detection module connected to the output of this receiver stage (21) capable of activating a signal in order to indicate an alarm.

Abstract: This invention relates to an antenna for transmission/reception of radio frequency waves that comprises:

Abstract: A system is provided for the centralized control of two groups of radiocommunications apparatus and two groups of radionavigational apparatus mounted on board an aircraft provided with two flight management computers, each of said flight management computers controlling the operation of the radionavigational apparatus of one of said groups. This system comprises two control devices dialoguing with each other respectively associated with said groups of radiocommunications apparatus and each including computing means, radiocommunications apparatus selection means, radionavigational apparatus selection means, frequency adjustment means and switching means. These two control devices are adapted for controlling the radiocommunications apparatus associated with the other, as well as the radionavigational apparatus associated with one of said flight management computers.