HULL SYSTEM AND AIRCRAFT

The present invention relates to a fairing system (5) provided with a hull and a rotor (10). The faired system comprising a collective modification device (30) for the pitch of the blades (11) of the rotor, the collective modification device (30) for the pitch of the blades having a spider plate (32...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	SERR, Christophe, JALAGUIER, Jean-Pierre
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention relates to a fairing system (5) provided with a hull and a rotor (10). The faired system comprising a collective modification device (30) for the pitch of the blades (11) of the rotor, the collective modification device (30) for the pitch of the blades having a spider plate (32) movable in rotation jointly with a hub (15) carrying the blades (11) around a drive axis (AXROT) and movable in translation relative to the hub (15) along the drive axis (AXROT). The faired system comprises for each blade (11) a mechanical connection (40). Each mechanical connection (40) comprises a tab (35) integral with the spider plate (32) as well as a pitch lever (17) of the foot (13) of a blade (11) and a ball joint (41) connecting the tab (35) to the pitch lever (17). The mechanical connection of at least one of the blades is different from the mechanical connection of at least another of the blades.