Sealing device for use between two structures e.g. honeycomb composite panels, of aircraft turbojet nacelle, has body comprising free end that is in contact with one structure, and made of rubber material allowing radial deformation of body

The device (105) has a rectangle or oval shaped body (107) comprising an end (109) that is fixed on a structure (103) of a sealing assembly (100) of a nacelle. The body comprises a free end (111) that is in contact with another structure (101) arranged near the former structure. The body is made of...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	AVENEL PHILIPPE, CONET OLIVIER
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS CYLINDERS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS PISTONS SEALINGS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The device (105) has a rectangle or oval shaped body (107) comprising an end (109) that is fixed on a structure (103) of a sealing assembly (100) of a nacelle. The body comprises a free end (111) that is in contact with another structure (101) arranged near the former structure. The body is made of rubber material, which allows radial deformation of the body. The body comprises a core made of metal or glass and formed to maintain the body in position on the two structures. The fixed end of the body is provided with a seal. L'invention se rapporte à un dispositif d'étanchéité (105) destiné à être disposé entre deux structures (101; 103) d'une nacelle pour un turboréacteur (6) d'aéronef, ledit dispositif (105) comportant un corps (107) dont une extrémité (109) est destinée à être fixée sur une première structure (103) de la nacelle et l'autre extrémité (111) est destinée à rester libre et à être en contact sur une seconde structure (101) disposée à proximité de la première structure (103), ledit corps (107) étant réalisé dans un matériau en caoutchouc autorisant une déformation radiale dudit corps (107). L'invention se rapporte également à un ensemble d'étanchéité (100) pour une nacelle d'un aéronef et une nacelle comportant un tel dispositif (105).