An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure and a microwave system. The nacelle inlet structure extends circumferentially about a centerline. The nacelle inlet structure includes an exterior skin. The exterior skin includes dielectric material. The microwave system is configured to direct microwaves to the dielectric material for melting and/or preventing ice accumulation on the exterior skin.
THERMAL ANTI-ICING SYSTEM WITH MICROWAVE SYSTEM
2021-05-06
Patent
Electronic Resource
English