Aircraft Wing Ice Protection System - How Leading-Edge Slats and Engine Inlets Prevent Icing #143638 (License: Personal Use)

The image depicts a simplified aircraft wing with extended leading-edge slats and a turbofan engine inlet, highlighting regions vulnerable to ice accretion. Blue ovals represent supercooled water droplets impacting the wing’s leading edge, while star-shaped icons inside the engine fan indicate ice crystals ingested into the core. Dashed lines outline internal heating elements or bleed-air ducts used for thermal anti-icing.

Used on aviation safety, aerospace engineering, or aircraft maintenance webpages to explain in-flight icing hazards and mitigation strategies; targets pilots, engineers, and aviation students seeking technical understanding of ice protection systems.