An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure (22) and a microwave system (80). The nacelle inlet structure extends circumferentially about a centerline (16). The nacelle inlet structure includes an exterior skin (78). The exterior skin includes dielectric material (82). The microwave system is configured to direct microwaves (88) to the dielectric material for melting and/or preventing ice accumulation on the exterior skin.
THERMAL ANTI-ICING SYSTEM WITH MICROWAVE SYSTEM
THERMISCHES VEREISUNGSSCHUTZSYSTEM MIT MIKROWELLENSYSTEM
SYSTÈME ANTIGIVRAGE THERMIQUE COMPRENANT UN SYSTÈME À MICRO-ONDES
2023-03-22
Patent
Electronic Resource
English