Turboprop carrier structure and an assembly including such a carrier structure

The carrier structure of the invention is used for carrying a turboprop and it is designed to be mounted beneath and/or in front of an airplane wing. In characteristic manner, the carrier structure comprises: a top portion comprising a front arch, a rear arch, and longitudinal beams; an upwardly-ope...

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Bibliographische Detailangaben
Hauptverfasser:	PICARD JEAN-LOUIS, MAZEAUD GEORGES
Format:	Patent
Sprache:	eng
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:	The carrier structure of the invention is used for carrying a turboprop and it is designed to be mounted beneath and/or in front of an airplane wing. In characteristic manner, the carrier structure comprises: a top portion comprising a front arch, a rear arch, and longitudinal beams; an upwardly-open removable bottom portion comprising at least two bottom arches and longerons; the bottom portion being demountably fixed to the top portion by centering and fixing devices, the bottom and top portions together defining a housing suitable for receiving said turboprop, and a suspension for carrying said turboprop.