AIRCRAFT PROPULSION UNIT COMPRISING A HIGH TEMPERATURE RESISTANT BRUSH SEAL

A seal is interposed between two surfaces of an aircraft propulsion assembly. The seal includes at least two layers each comprising a plurality of strands made of a heat-resistant material, the strands of a first layer being oriented in a first orientation and the strands of a second layer being ori...

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Bibliographische Detailangaben
Hauptverfasser: AUDART-NOEL, VIRGINIE, LETAY, BENOIT, GALINIER, MICHAEL, DUSSOL, LOÏC, VIALLET, NICOLAS, VIGNOBOUL, BENJAMIN, CAZEAUX, LAURENT
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A seal is interposed between two surfaces of an aircraft propulsion assembly. The seal includes at least two layers each comprising a plurality of strands made of a heat-resistant material, the strands of a first layer being oriented in a first orientation and the strands of a second layer being oriented in a second orientation different than the first orientation.