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A turbojet having an air intake case including radial arms between an outer annular structure and an inner central structure, and a deicing unit configured to deice the radial arms by microwaves and located in the central structure. The deicing unit has a microwave generator and a transmitting eleme

A turbojet having an air intake case including radial arms between an outer annular structure and an inner central structure, and a deicing unit configured to deice the radial arms by microwaves and located in the central structure. The deicing unit has a microwave generator and a transmitting element configured to transmit energy and including an inside annular waveguide located inside of the central structure. An energy distributing element configured to eliminate ice is coupled with the transmitting element by a coupling element. The radial arms are made from a dielectric composite material.

대표청구항 ▼

A turbojet comprising: an air intake case having radial arms between an outer annular structure and an inner central structure, said radial arms being made from a dielectric composite material; a deicing unit configured to deice said radial arms by microwaves and located in said central structure, s

A turbojet comprising: an air intake case having radial arms between an outer annular structure and an inner central structure, said radial arms being made from a dielectric composite material; a deicing unit configured to deice said radial arms by microwaves and located in said central structure, said deicing unit having a microwave generator and a transmitting element configured to transmit energy supplied by said microwave generator, said transmitting element comprising an inside annular waveguide located inside of said central structure; an energy distributing element configured to eliminate ice; and a coupling element coupling said transmitting element and said energy distributing element.