Icing condition detection system

Icing condition detection system

A method and apparatus for detecting an icing condition. The apparatus comprises a piezoelectric material (304) and a vibration detector (308). The piezoelectric material (304) has a surface proximate to a surface of a vehicle. The piezoelectric material (304) is configured to vibrate. The vibration...

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Hauptverfasser: Perry, George, A, Clemen, JR. Mark Joseph, Gardner, Scott Hutchinson, Meis, Charles Steven, Langhofer, Erik Marc, Wert, Jerry Lee
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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creator Perry, George, A
Clemen, JR. Mark Joseph
Gardner, Scott Hutchinson
Meis, Charles Steven
Langhofer, Erik Marc
Wert, Jerry Lee
description A method and apparatus for detecting an icing condition. The apparatus comprises a piezoelectric material (304) and a vibration detector (308). The piezoelectric material (304) has a surface proximate to a surface of a vehicle. The piezoelectric material (304) is configured to vibrate. The vibration detector (308) is configured to detect a change in vibrations in the piezoelectric material (304) that indicates a presence of an icing condition on the surface of the piezoelectric material (304).
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subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title Icing condition detection system
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