System and method for utilization of transmitted digital flight data acquisition information to accomplish vibration balance solutions

摘要

A system and method is provided for monitoring, collecting, storing, transmitting, calculating and uploading to a secure web server real-time balancing solutions for at least the N1 Low Pressure Compressor portion of a jet engine. The method comprises collecting a series of engine vibration data strings and transmitting a data string set to a ground stations for conditioning, formatting and forwarding to a source for calculating and providing fan balance solutions to a secure server wherein the data strings comprise at least phase angle of imbalance data, N1 RPM and the magnitude of the N1 vibration. The balance solution determined comprises the required weight (mass) and location of weight (mass) installation necessary to correct a fan imbalance in a turbine engine.