The invention belongs to the field of aero-engine
oil supply, and particularly relates to an
oil supply correction method in the case of starting an aero-engine at a
plateau. The method comprises thefollowing steps of obtaining a power characteristic coefficient epsilon of an auxiliary power
system and a power acting proportion coefficient
lambda of the auxiliary power
system, and calculating anauxiliary
power correction coefficient K<auxiliary>; obtaining a correction coefficient K<conventional> performed according to the engine characteristics and an engine ground starting rotating speed
rise rate N<2> Dot<ground>, and calculating an engine
plateau starting rotating speed
rise rate N<2> Dot<
plateau>; and calculating a main
fuel supply rule according to the engine plateau starting rotating speed
rise rate N<2>Dot< plateau>. According to the method, the more real auxiliary power is obtained through correction according to the auxiliary power
system power keeping characteristic, comprehensive conversion is performed to form the rotating speed rise rate correction amount according to the proportion relation between the
auxiliary system power in the starting rotating speed range and the
turbine power, the starting process is corrected, the rotating speed rise rate is more matched with the actual residual power, the
oil supply amount is corrected to fully exert the starting potential, the starting time is shortened, and the starting success rate is increased.