Ice detection assembly installed on an aircraft

Aeronautics and astronautics – Aircraft structure – Ice prevention

Reexamination Certificate

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Details

C340S580000

Reexamination Certificate

active

07000871

ABSTRACT:
Ice detection assembly (100) designed for installation on an aircraft, comprising a vibrating finger (110) and a mast (120), the vibrating finger (110) extending into the air from the mast (120) and capable of being vibrated by vibration means at a resonant frequency that is sensitive to an ice deposit on its surface, characterised in that it comprises a cooling system capable of cooling at least part of the detection assembly (100).

REFERENCES:
patent: 3341835 (1967-09-01), Werner
patent: 3541540 (1970-11-01), Hughes
patent: 4222044 (1980-09-01), Boschung
patent: 4532806 (1985-08-01), Bruchmuller
patent: 4570881 (1986-02-01), Lustenberger
patent: 5003295 (1991-03-01), Kleven
patent: 5585551 (1996-12-01), Johansson et al.
patent: 6320511 (2001-11-01), Cronin et al.
patent: 6456200 (2002-09-01), Bostrom et al.

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