AIRCRAFT WITH DRIVE ELEMENT COUPLED TO GEARBOX HOUSING EXTERIOR

An aircraft is provided and includes a gearbox housing through which a drive shaft configured to drive propeller rotation extends and a pitch control apparatus. The pitch control apparatus includes a drive element coupled to an exterior of the gearbox housing and an annular electro-mechanical actuat...

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Bibliographische Detailangaben
1. Verfasser: DARROW, JR. DAVID A
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:An aircraft is provided and includes a gearbox housing through which a drive shaft configured to drive propeller rotation extends and a pitch control apparatus. The pitch control apparatus includes a drive element coupled to an exterior of the gearbox housing and an annular electro-mechanical actuator (EMA) configured to convert rotational energy generated by the drive element to thereby control a pitching of propeller blades about corresponding pitch axes.