METHOD FOR AIRCRAFT INLET DISTORTION CONTROL

摘要

The present invention relates to a method for controlling the distortion of an aircraft air scoop. By using a sensor including a pressure sensor, a temperature sensor, a velocity sensor, an acceleration sensor, and a posture sensor, the distortion of an inlet can be sensed, and the sensed information is provided, after being classified into one among normal, warning, and danger levels. When the distortion rate of the inlet reaches a limit value of a graph showing the planning margin of a compressor, a forced control is conducted, in order to reduce the distortion of the inlet. [Reference numerals] (AA) Normal, Warning; (BB) Danger; (S01) Measurement step; (S02) Operation step; (S03) Inlet distortion determination step; (S03a) First output step; (S03b) Second output step; (S03c) Third output step; (S04) Control range calculating step; (S05) Air suction hole control step