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DEVICE FOR DE-ICING THE INLET OF A NACELLE OF AN AIRCRAFT ENGINE, METHOD FOR PRODUCING SUCH A DE-ICING DEVICE, AND AIRCRAFT ENGINE NACELLE PROVIDED WITH SUCH A DE-ICING DEVICE
DEVICE FOR DE-ICING THE INLET OF A NACELLE OF AN AIRCRAFT ENGINE, METHOD FOR PRODUCING SUCH A DE-ICING DEVICE, AND AIRCRAFT ENGINE NACELLE PROVIDED WITH SUCH A DE-ICING DEVICE
A de-icing device is provided that includes a piccolo tube integrated with a front bulkhead for limiting an inner volume of a perforated front lip. The piccolo tube is in contact with a noise reduction cellular structure provided with perforations and hot air circulation channels delivered by the piccolo tube, the de-icing hot air being diffused through the perforations and channels of the cellular structure, on the perforations facing the front lip.
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