Aircraft Aerodynamic Probe Using Electromagnetic Wave Heating

The patent replaces the conventional electrical heating system with an electromagnetic radiation system. Instead of using resistive heating elements that consume significant electrical power, the invention uses electromagnetic waves (such as microwaves or infrared radiation) to heat the probe surface and prevent ice and water accumulation. This substitution maintains the anti-icing function while significantly reducing electrical power consumption.

The patent introduces electromagnetic radiation as an intermediary energy transfer mechanism. Rather than directly converting electrical energy to heat through resistors, the system uses electromagnetic waves as a mediator to transfer energy to the probe surface and water/ice particles. This intermediary approach allows for more efficient energy transfer and reduced electrical power consumption while maintaining effective ice prevention.

The patent extracts the heating function from the complex electrical heating system and implements it through electromagnetic radiation. By removing the need for intricate heating element wiring, thermal management systems, and control circuits associated with conventional electrical heating, the invention simplifies the overall device architecture while maintaining effective ice prevention capabilities.

The patent replaces the complex mechanical and electrical heating infrastructure with a streamlined electromagnetic radiation system. This substitution eliminates numerous components including heating elements, thermal insulation layers, temperature sensors, and control systems, thereby reducing device complexity while effectively preventing ice accumulation on the probe.