CONTROLLING EXCITATION LOADS ASSOCIATED WITH OPEN ROTOR AERONAUTICAL ENGINES

An open rotor aeronautical engine may include a core engine, a plurality of unducted airfoils, and a pitch change assembly. The pitch change assembly may include an ensemble actuator assembly and a unitary actuator assembly. The ensemble actuator assembly may have one or more ensemble actuators and...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Zutshi, Amit, Cafaro, Stefan Joseph, Reepmeyer, James Ryan, Hegeman, Arjan Johannes, Mollmann, Daniel Edward, Sarba, Rafal, Khalid, Inenhe Mohammed
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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