Turbojet equipped with a deicing system on the intake case

Details Turbojet equipped with a deicing system on the intake case Turbojet equipped with a deicing system on the intake case

1995-07-31

1997-04-29

Freay, Charles G.

Power plants

Combustion products used as motive fluid

With safety device

415175, 219679, 244134D, F02C 7047

Patent

active

056238215

ABSTRACT:
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.

REFERENCES:
patent: 4365131 (1982-12-01), Hansman, Jr.
patent: 4863354 (1989-09-01), Asselin et al.
patent: 5029440 (1991-07-01), Graber et al.
patent: 5061836 (1991-10-01), Martin

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