SYSTEME D'ANTI GIVRAGE ET DE DEGIVRAGE DE NACELLE DE MOTEUR D'AERONEF A TAPIS RESISTIF
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United States of America Patent
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N/A
Issued Date -
Aug 12, 2010
app pub date -
Jun 19, 2006
filing date -
Jun 22, 2005
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A deicing and anti-icing system for an aircraft engine pod, including an air intake provided with a lip followed by an air intake tubular part, equipped with a first sound attenuating panel, including deicing means having at least one array of resistive heating elements embedded in an insulating material, the deicing means being in the form of a mat incorporating the resistive element in the thickness of the air intake lip.
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