STRUCTURE DE SUSPENSION D'UN TURBOPROPULSEUR A DOUBLE HELICES NON CARENEES SUR UN ELEMENT STRUCTUREL D'UN AERONEF A FIXATION RIGIDE DE LA STRUCTURE D'ENTREE D'AIR

STRUCTURE DE SUSPENSION D'UN TURBOPROPULSEUR A DOUBLE HELICES NON CARENEES SUR UN ELEMENT STRUCTUREL D'UN AERONEF A FIXATION RIGIDE DE LA STRUCTURE D'ENTREE D'AIR

A suspension structure for suspending a turboprop including two unducted propellers from a structural element of an aircraft, the structure including a suspension frame for fastening to a structural element of the aircraft and including a main beam extending parallel to a longitudinal axis of the tu...

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Bibliographische Detailangaben
Hauptverfasser: FLORENT NICOLAS, POISSON MATHIEU, ANGE, BELLABAL FRANCOIS, ROBERT
Format: Patent
Sprache:fre
Schlagworte:
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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Beschreibung
Zusammenfassung:A suspension structure for suspending a turboprop including two unducted propellers from a structural element of an aircraft, the structure including a suspension frame for fastening to a structural element of the aircraft and including a main beam extending parallel to a longitudinal axis of the turboprop, the suspension frame being fastened to an air intake structure of the turboprop by an attachment frame.