Spherical motor for active side lever system of airplane

The invention discloses a spherical motor for an active side lever system of an airplane, and the spherical motor is connected with the left and right sides of a conventional airplane operating panel (10A), thereby forming a double-sphere motor operating system. The spherical motor comprises an A se...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: YAN LIANG, JIAO ZONGXIA, LIU YINGHUANG, SHANG YAOXING
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention discloses a spherical motor for an active side lever system of an airplane, and the spherical motor is connected with the left and right sides of a conventional airplane operating panel (10A), thereby forming a double-sphere motor operating system. The spherical motor comprises an A semi-sphere stator (1), a B semi-sphere stator (2), a rotor (3), an output rod (4), a pedestal (5), an armature winding assembly (6), a magnetic block assembly (7), and a universal ball bearing assembly (8). The A semi-sphere stator (1) and the B semi-sphere stator (2) are connected in a manner of butt joint to form a hollow sphere, and the rotor (3) is disposed in the hollow sphere. The output rod (4) is installed at the upper part of the rotor (3), and the A semi-sphere stator (1) and the B semi-sphere stator (2) are installed on the pedestal (5). The armature winding assembly (6) and the universal ball bearing assembly (8) are installed on the A semi-sphere stator (1) and the B semi-sphere stator (2). The magnetic