The invention belongs to the technical field of pneumatic
safety monitoring of aircrafts, and provides a bionic intelligent
skin of a fixed-wing aircraft applied to stall early warning, the bionic intelligent
skin comprises a flexible substrate and a bionic micro-beam type
airflow sensing array, the flexible substrate is conformally arranged on the upper surface of a wing, the sensing array comprises at least two rows of subarrays arranged in the chordwise direction of the wing, and the subarrays are arranged on the flexible substrate. And each row of subarrays comprises a plurality of sensing units arranged along the spanwise direction of the wing. The principle of a
dragonfly seta sensor is simulated,
airflow force is directly sensed through a micro-
cantilever structure, the sensor is extremely sensitive to tiny flow field changes, and early capture of stall omen can be achieved; moreover, through array
layout, traditional point type measurement is upgraded into two-dimensional flow field imaging, the occurrence, development and migration process of the
airflow separation area can be visually presented in real time, and early warning information is richer and more reliable. Finally, a flexible substrate and a micro-
nano machining technology are adopted, the sensor can be integrated on the surface of the
skin in a light and thin array mode, the aerodynamic configuration is not damaged, and installation and maintenance are easy.