Protection device for an external aircraft probe

The device (10) has a rigid flange (22) for attachment to an outside surface (16) of an aircraft and a flexible envelope (24) for protection of an external probe (12). The probe comprises an outside part (18) that moves beyond the outside surface. The flange comprises a central passage (28) that is...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VIEULES, CHRISTOPHE, OUTTERS, XAVIER, MEREAU, PHILIPPE
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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Beschreibung
Zusammenfassung:The device (10) has a rigid flange (22) for attachment to an outside surface (16) of an aircraft and a flexible envelope (24) for protection of an external probe (12). The probe comprises an outside part (18) that moves beyond the outside surface. The flange comprises a central passage (28) that is broader than the outside part. The flexible envelope is closed at an outside end (30) and opened by a mouth (32) at an inside end (34), where an edge (36) of the mouth is connected in an airtight manner to the flange all around the central passage. The flexible envelope is made of an airtight material. L'objet de l'invention est un dispositif de protection (10) d'une sonde externe (12) d'un aéronef faisant saillie au travers d'une ouverture (14) réalisée dans la surface extérieure (16) de l'aéronef. Le dispositif de protection (10) comprend une bride rigide (22) de fixation à la surface extérieure (16) de l'aéronef et une enveloppe souple (24) de protection de la sonde. La bride est fixée par des moyens de fixation rapide sur la face extérieure de l'aéronef.