WARM AIR FEED SYSTEM FOR AIRCRAFT

This invention concerns a hot air feed for an aircraft equipped with at least a fan (3) engine (2) and compressors (4). According to the invention, the regulation devices (14, 15, 16) for regulating the flow of hot and cold air sent by conduits 10 and 11 to the heat exchanger (12) are pneumatic, ele...

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Bibliographic Details
Main Authors PRADEAU, PIERRE MICHEL FRANCOIS, CAHINGT, HELENE LISE, POIRIER, DIDIER PASCAL ROBERT, MONFRAIX, JEAN HENRI
Format Patent
LanguageEnglish
French
Published 14.11.2006
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:This invention concerns a hot air feed for an aircraft equipped with at least a fan (3) engine (2) and compressors (4). According to the invention, the regulation devices (14, 15, 16) for regulating the flow of hot and cold air sent by conduits 10 and 11 to the heat exchanger (12) are pneumatic, electrically activated and commanded by a central controller (24). La présente invention concerne un système d'alimentation en air chaud pour un aéronef pourvu d'au moins un moteur (2) à soufflante (3) et compresseurs (4). Selon l'invention, les dispositifs de régulation (14, 15, 16) destinés à réguler les débits d'air chaud et d'air froid adressés par les conduites 10 et 11 à l'échangeur thermique (12) sont pneumatiques, à commande électrique, et sont commandés par un dispositif de gestion centralisée (24).
Bibliography:Application Number: CA19992261364