A MOUNTING ARRANGEMENT FOR MOUNTING A GEAR BOX OF A ROTORCRAFT TO A FUSELAGE OF A ROTORCRAFT

The invention is related to a mounting arrangement 7 for mounting at least a gear box 6 of a rotorcraft to a fuselage 2 of a rotorcraft, said mounting arrangement 7 comprising a gear box 6 of a rotorcraft and at least two support plates 8 that are rigidly attached to at least approximately opposing...

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Bibliographische Detailangaben
Hauptverfasser:	WEHLE, CHRISTIAN, STEGER, JUSTUS, GUNN, HENRY
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GEARING GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The invention is related to a mounting arrangement 7 for mounting at least a gear box 6 of a rotorcraft to a fuselage 2 of a rotorcraft, said mounting arrangement 7 comprising a gear box 6 of a rotorcraft and at least two support plates 8 that are rigidly attached to at least approximately opposing sides of said gear box 6, each one of said at least two support plates 8 comprising at least two attachment means 8c that are adapted to allow attachment of said at least two support plates 8 to a fuselage 2 of a rotorcraft by means of associated struts 11a in order to enable transfer of induced loads occurring in operation, which are directed into a predetermined load direction, via said associated struts 11a. Linvention a trait à un agencement de montage (7) pour fixer au moins une boîte à engrenages (6) dun giravion à un fuselage (2) dun giravion, ledit agencement de montage (7) comprenant une boîte à engrenages (6) dun giravion et au moins deux plaques de support (8) qui sont fixées de manière rigide au moins à des parois approximativement opposées de ladite boîte à engrenages (6), chacune desdites au moins deux plaques de support (8) comprenant au moins deux moyens de fixation (8c) qui sont conçus pour permettre la fixation desdites au moins deux plaques de support (8) à un fuselage (2) dun giravion au moyen dentretoises correspondantes (11a) afin de permettre le transfert de charges induites survenant durant le fonctionnement, qui sont dirigées dans une direction de charge prédéterminée, par lesdites dentretoises correspondantes (11a).