Cockpit for aircraft, has attitude indicating system configured for tri-dimensionally spatializing sound signals to be transmitted to pilot according to attitude of aircraft by audio processing controller and loudspeakers

The cockpit has a seat utilized for a pilot and an attitude indicating system of an aircraft. The seat includes a headrest (6) with a reception face to accommodate a head of the pilot. The system comprises an audio processing controller and loudspeakers (20-22, 30-32). The system is configured to tr...

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Bibliographic Details
Main Authors COLIN MICHEL, CHATRENET NICOLAS
Format Patent
LanguageEnglish
French
Published 22.08.2014
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
DEAF-AID SETS
ELECTRIC COMMUNICATION TECHNIQUE
ELECTRICITY
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GYROSCOPIC INSTRUMENTS
LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKEACOUSTIC ELECTROMECHANICAL TRANSDUCERS
MEASURING
MEASURING DISTANCES, LEVELS OR BEARINGS
NAVIGATION
PARACHUTES
PERFORMING OPERATIONS
PHOTOGRAMMETRY OR VIDEOGRAMMETRY
PHYSICS
PUBLIC ADDRESS SYSTEMS
STEREOPHONIC SYSTEMS
SURVEYING
TESTING
TRANSPORTING
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Summary:The cockpit has a seat utilized for a pilot and an attitude indicating system of an aircraft. The seat includes a headrest (6) with a reception face to accommodate a head of the pilot. The system comprises an audio processing controller and loudspeakers (20-22, 30-32). The system is configured to tri-dimensionally spatialize sound signals to be transmitted to the pilot according to attitude of the aircraft by the controller and the loudspeakers. The loudspeakers are arranged in the headrest on the face and distributed on both sides of a median vertical plane (P1) of the face. L'invention concerne un poste de pilotage d'un aéronef, comprenant au moins un siège pour un pilote de l'aéronef et un système indicateur d'attitude (10) de l'aéronef, le siège comprenant un appui-tête présentant une face d'accueil destinée à accueillir la tête du pilote, le système indicateur d'attitude comprenant un calculateur de traitement audio (1) et au moins deux haut-parleurs (H1-H4, 20-22, 30-32), ledit système indicateur d'attitude étant configuré pour spatialiser tri-dimensionnellement un signal sonore (S1-S4) à transmettre au pilote en fonction de l'attitude de l'aéronef au moyen du calculateur de traitement audio (1) et des haut-parleurs (H1-H4, 20-22, 30-32), caractérisé en ce que les haut-parleurs sont agencés dans ledit appui-tête (6) au niveau de la face d'accueil, et sont répartis de part et d'autre d'un plan vertical médian de ladite face d'accueil (P1).
Bibliography:Application Number: FR20130058021