A mechanism for transitioning a tiltrotor aircraft between rotary and non rotary flight modes. The mechanism includes a gimbal lock positioned about a mast that is operable to selectively enable and disable a gimballing degree of freedom of a rotor assembly relative to the mast. A blade stop assembly, positioned about the mast, includes a plurality of arms having a radially contracted orientation and a radially extended orientation. A blade lock assembly is operably associated with each rotor blade assembly. Each blade lock assembly is operable to selectively enable and disable a folding degree of freedom and a pitching degree of freedom of the respective rotor blade assembly. A swash plate is operable to change the pitch of the rotor blade assemblies in the rotary flight mode and fold the rotor blade assemblies in the non rotary flight mode.
Tiltrotor Aircraft having Rotary and Non Rotary Flight Modes
2017-05-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
TILTROTOR AIRCRAFT HAVING ROTARY AND NON ROTARY FLIGHT MODES
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