Patent application number | Description | Published |
20100242428 | AIR INTAKE STRUCTURE TO BE MOUNTED UPSTREAM OF A NACELLE MIDDLE STRUCTURE FOR AIRCRAFT ENGINE, AND NACELLE EQUIPPED WITH SUCH AIR INTAKE STRUCTURE - The invention relates to an air intake structure that can be mounted upstream of a nacelle middle structure for an aircraft engine, and that particularly includes: an outer wall ( | 09-30-2010 |
20100252689 | AIRCRAFT NACELLE GUIDANCE SYSTEM INSTALLATION - The present invention relates to a turbojet engine nacelle ( | 10-07-2010 |
20100314198 | AIRCRAFT TURBOJET ENGINE NACELLE AIR INTAKE MAINTENANCE TROLLEY - This maintenance trolley ( | 12-16-2010 |
20100314501 | LOCKING SYSTEM FOR AIR INTAKE STRUCTURE FOR TURBOJET ENGINE NACELLE - The invention relates to a nacelle for a turbojet engine that includes an air intake structure ( | 12-16-2010 |
20100320316 | AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE - The invention relates to an air intake for an aircraft nacelle that comprises a shroud ( | 12-23-2010 |
20110011981 | AIR INTAKE STRUCTURE FOR AN AIRCRAFT NACELLE - The invention relates to an air intake structure capable of being mounted upstream of a central structure of a nacelle for an aircraft engine, the said air intake structure comprising: —an external wall incorporating a lip, —an upstream partition ( | 01-20-2011 |
20110014044 | LOCKING SYSTEM FOR AIR INTAKE STRUCTURE FOR TURBOJET ENGINE NACELLE - The invention relates to a nacelle for a turbojet engine that comprises an air intake structure ( | 01-20-2011 |
20110182727 | TURBOJET ENGINE NACELLE - The invention relates to a nacelle ( | 07-28-2011 |
20110219783 | TURBOJET ENGINE NACELLE WITH TRANSLATABLE UPSTREAM COWL - Turbojet engine nacelle ( | 09-15-2011 |
20110284095 | TURBOJET ENGINE NACELLE - The invention relates to a turbojet engine nacelle ( | 11-24-2011 |
20140026582 | ANTI-FIRE SEAL ASSEMBLY AND NACELLE COMPRISING SUCH A SEAL - A seal assembly for a turbojet nacelle includes a first end fastened to a first structure, and a second end contacting against a bearing zone of a second structure. The seal assembly further includes a plurality of adjacent blades arranged along the first end and extending longitudinally and perpendicularly thereto. In particular, a portion of the blades has an accordion-shaped structure. | 01-30-2014 |
20140318149 | SEAL FOR A TURBOJET ENGINE PYLON AND NACELLE, AND TURBOJET ENGINE PYLON-NACELLE ASSEMBLY INCORPORATING SUCH A SEAL - A fire-resistant seal for a propulsion assembly which includes a pylon, an O-duct type nacelle of a turbojet engine. The nacelle includes an inner fixed nacelle structure and a combustion gas ejection primary nozzle, and the fire-resistant seal is placed in an annular sector defined by the inner fixed nacelle and the gas ejection primary nozzle. In particular, the fire-resistant seal includes a plurality of baffles, and the plurality of baffles are longitudinally disposed so as not to interfere each other during a longitudinal translational movement of the inner fixed nacelle structure relative to the combustion gas ejection primary nozzle. | 10-30-2014 |