Bracket assembly for supporting terminal leads in auxiliary generator for aircraft
Abstract:
A bracket assembly for supporting terminal leads in an auxiliary generator of an aircraft, which includes a first bracket adapted and configured to be fastened to a stator housing of the generator to retain a main stator within the stator housing, and a second bracket adapted and configured to be fastened to a top surface of the first bracket to support a plurality of terminal leads in such a manner so that they are not susceptible to damage from resonance and vibration.
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