Title :
Aircraft-electric-accessory-vibration investigations
Author_Institution :
General Electric Company, Schenectady, N. Y.
Abstract :
Flight and laboratory tests are in progress to determine changes in design of aircraft generators which will improve their resistance to vibration-fatigue failure. Vibrations near mountings of generator voltage regulators and reverse-current relays are being measured to provide data for design and testing of these accessories.
Keywords :
Aircraft; Damping; Engines; Flanges; Generators; Torque; Vibrations;
Journal_Title :
Electrical Engineering
DOI :
10.1109/EE.1944.6440679
