The invention relates to a method and
system for predicting the maximum rotating speed of a
power turbine after an engine loses load, and belongs to the field of
aviation gas
turboshaft engines. The method comprises the following steps that a pressure
signal of a
gas compressor outlet of the engine, a pressure
signal of a main oil way of a
fuel oil distribution device and a pressure
signal of an auxiliary oil way of the
fuel oil distribution device are obtained; performing a
simulation over-
rotation test under the maximum state of the engine, and obtaining a
fuel oil rule of the maximum state over-rotation of the engine according to a test result; carrying out segmented iterative calculation on the rotating speeds of the
power turbine at different time points in the maximum state over-rotating process of the engine to obtain a relationship between the rotating speeds of the
power turbine and time; and according to the relationship between the power
turbine rotating speed and time, the maximum power
turbine rotating speed in the maximum state overrunning process of the engine is obtained. According to the method, the
response time, the fuel attenuation rule and the torque change rule of the over-rotation
protection system are fully considered, and the maximum rotating speed under the condition of shaft breakage of the engine can be accurately predicted.