AIRCRAFT AND AIRCRAFT GEAR MOTOR ASSEMBLY

This invention concerns a gear motor reduction group (10) including a power transmission box (20) and at least one motor (40). The said at least one motor (40) is borne solely by the power transmission box (20) through a fastening system (60), the said fastening system (60) comprising at least three...

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Bibliographische Detailangaben
Hauptverfasser:	BELMONTE, JÉRÔME, ZAMPONI, LAURENT, MARIE, ADRIEN
Format:	Patent
Sprache:	eng ; pol
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	This invention concerns a gear motor reduction group (10) including a power transmission box (20) and at least one motor (40). The said at least one motor (40) is borne solely by the power transmission box (20) through a fastening system (60), the said fastening system (60) comprising at least three fastening bars (61) each connecting an outer casing (21) of the power transmission box (20) to the motor (40), the said fastening system (60) including a linking element (65) secured to the said outer casing (21) and to the said outer envelope (45), the said linking element (65) being rigid in torsion around the said drive axis (AX) and allowing a predetermined relative displacement between the said power transmission box (20) and the said motor (40).