| Patent application number | Description | Published |
|---|
| 20080315034 | Turbojet Engine Nacelle with Lateral Opening of Covers - The present invention relates to a nacelle ( | 12-25-2008 |
| 20090107108 | NACELL FOR BYPASS ENGINE WITH HIGH BYPASS RATIO - This invention relates to a nacelle for bypass engine with a high bypass ratio comprising an interior flow channel for a secondary flow generated by the bypass engine and having an external structure provided with a reverse thrust device capable of alternately shifting from a closed position in which it enables circulation of the direct-jet secondary flow inside the interior channel, to an open position in which it uncovers an opening in the external structure so as to enable reorientation of the secondary flow in an angled flow via activation of the reverse thrust means; in open position, the reverse thrust device partially blocks the interior channel so as to provide a leakage section therein, enabling circulation of a controlled leakage flow, said nacelle being characterized in that, when the thrust reversal device is in open position and has an angled-jet reversal section and a leakage section through the interior channel the sum of which is substantially equal to a direct-jet secondary flow discharge section, when the thrust reversal device is in closed position. | 04-30-2009 |
| 20090134272 | AIR INLET LIP FOR A POD WITH ELECTRIC DEFROSTING - The present invention relates to a lip ( | 05-28-2009 |
| 20090188233 | THRUST REVERSER FORMING AN ADAPTIVE NOZZLE - The present invention relates to a thrust reverser for the nacelle of a turbojet engine comprising, on the one hand, means ( | 07-30-2009 |
| 20090255271 | STRUCTURAL NACELLE - The present invention relates, on the one hand, to a nacelle ( | 10-15-2009 |
| 20100001123 | TRANSLATABLE THRUST INVERTER FOR JET ENGINE - The invention relates to a thrust inverter with grids ( | 01-07-2010 |
| 20100008772 | NACELLE FOR THE JET ENGINE OF AN AIRCRAFT - The invention relates to a nacelle for a turbojet, of the type comprising a downstream structure having an outer structure ( | 01-14-2010 |
| 20100024435 | NACELLE FOR TURBOFAN - The nacelle of the invention includes an air-inlet front section, a middle section for encasing the fan of the turbofan ( | 02-04-2010 |
| 20100031629 | LOCKABLE GUIDING SYSTEM FOR A MOBILE PART OF A NACELLE - The invention relates to a guiding device ( | 02-11-2010 |
| 20100037587 | Turbojet Nacelle Equipped With Means For Reducing The Noise Produced By Said Turbojet - This nacelle ( | 02-18-2010 |
| 20100040466 | BYPASS TURBOJET ENGINE NACELLE - The nacelle ( | 02-18-2010 |
| 20100059634 | LOCKING SYSTEM FOR A MOVABLE NACELLE COWL - The present invention relates to a locking system ( | 03-11-2010 |
| 20100064660 | JET ENGINE NACELLE MEMBER - The invention relates to an nacelle member ( | 03-18-2010 |
| 20100084507 | REMOVABLE AIR INTAKE STRUCTURE FOR TURBOJET ENGINE NACELLE - The present invention relates to a nacelle ( | 04-08-2010 |
| 20100107599 | THRUST REVERSER FOR A JET ENGINE - The invention relates to a thrust reverser ( | 05-06-2010 |
| 20100132332 | CASCADE-TYPE THRUST REVERSER FOR JET ENGINE - A fan duct ( | 06-03-2010 |
| 20100139242 | THRUST REVERSER WITH GRIDS FOR JET ENGINE - The invention relates to a thrust reverser ( | 06-10-2010 |
| 20100181418 | SECURING PLATE AND LONGITUDINAL HANDLING MEMBER FOR A ONE-PIECE AIRCRAFT PROPULSION UNIT - The invention relates to a securing plate ( | 07-22-2010 |
| 20100218479 | LINEAR TELESCOPIC ACTUATOR FOR MOVING A FIRST AND A SECOND ELEMENT RELATIVE TO A STATIONARY ELEMENT - The invention relates to a linear telescopic actuator for moving a first ( | 09-02-2010 |
| 20100232932 | AIR INLET SHROUD STRUCTURE - The present invention relates to a nacelle for a turbojet, comprising an air inlet structure capable of channelling a flow of air to a turbojet fan and a middle structure ( | 09-16-2010 |
| 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 |
| 20100269511 | NACELLE FOR AIRCRAFT ENGINE HAVING A NOZZLE WITH A VARIABLE SECTION - The invention relates to a nacelle for an aircraft engine that comprises a front cowling ( | 10-28-2010 |
| 20100284806 | SIDE-OPENING JET ENGINE NACELLE - The invention relates to a nacelle including an air intake upstream from the jet engine ( | 11-11-2010 |
| 20110120076 | STRUCTURE FOR AN AIR INLET LIP OF AN ELECTRIC DE-ICING POD COMPRISING AN ACOUSTIC ATTENUATION ZONE - The present invention relates to a structure ( | 05-26-2011 |
