| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
|---|
| 11/18/2004 | US20040226333 Method of manufacturing elliptic deep-drawn products |
| 11/11/2004 | WO2004096641A1 Air input device for a turboprop engine |
| 09/10/2004 | WO2004077400A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 09/01/2004 | CN1525920A Integrated and/or modular high-speed aircraft |
| 08/26/2004 | US20040163888 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 08/25/2004 | EP1449766A1 Structural frame for a turbo-prop and assembly including such a structural frame |
| 08/18/2004 | EP0960049B1 Telescopic rod for opening a mobile cowl, in particular of an aircraft engine bay |
| 08/10/2004 | US6772856 Fine jet control-type sound absorption system |
| 07/29/2004 | US20040144889 Aircraft engine nacelles and methods for their manufacture |
| 07/06/2004 | US6758439 Apparatuses and methods for attaching engine nacelles to aircraft |
| 06/29/2004 | US6755448 Blowout latch |
| 06/03/2004 | US20040104583 Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle |
| 05/20/2004 | US20040094664 Apparatuses and methods for attaching engine nacelles to aircraft |
| 05/12/2004 | EP0952920B1 Composite material panel with shock-protected edges |
| 04/27/2004 | US6725542 Method of assembling a gas turbine engine and nacelle |
| 03/10/2004 | EP1396422A1 Aircraft engine nacelle with a landing gear bay and method for its manufacture |
| 03/03/2004 | EP1394388A2 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 03/03/2004 | EP0960051B1 Aircraft propulsion unit with fan cowls equipped with maintaining and positioning safety elements |
| 02/10/2004 | CA2204825C Jet turbine engine thrust reverser employing doors fitted with upstream panel |
| 01/29/2004 | US20040016845 Integrated and/or modular high-speed aircraft |
| 01/22/2004 | US20040012212 Latch mechanism |
| 01/22/2004 | US20040012208 Externally adjustable latch |
| 01/01/2004 | US20040000615 Air intake for large-size nacelle with enhanced transportability |
| 12/23/2003 | US6666408 Closure fault indicator, particularly for an aircraft engine pod cowl |
| 12/16/2003 | US6663368 Spherical gear pump |
| 12/02/2003 | US6655632 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 11/25/2003 | US6651928 Aircraft engine nacelles and methods for their manufacture |
| 10/30/2003 | US20030201366 Hybrid exhaust heat shield for pylon mounted gas turbine engines |
| 10/16/2003 | US20030192987 System and method for controlling the movement of an aircraft engine cowl door |
| 10/15/2003 | EP1351855A2 Integrated and/or modular high-speed aircraft |
| 10/07/2003 | US6629712 Extendable latch |
| 09/25/2003 | US20030177797 Magnetically reactive pivot latch system |
| 09/23/2003 | US6622963 System and method for controlling the movement of an aircraft engine cowl door |
| 09/11/2003 | US20030168554 Device for fixing a member to an aircraft structure |
| 09/10/2003 | EP1342927A1 Device for attaching a component to an aircraft structure |
| 09/04/2003 | US20030163985 Cowl structure for a gas turbine engine |
| 08/27/2003 | EP1066195B1 Permanently connected remote latch mechanism |
| 08/20/2003 | EP1336707A1 Closing system mounted between two elements |
| 08/14/2003 | US20030151261 Closing system interposed between two elements |
| 07/16/2003 | EP0960050B1 Opening device for two adjacent cowls of an aircraft engine bay |
| 06/10/2003 | US6575406 Integrated and/or modular high-speed aircraft |
| 06/05/2003 | US20030102405 Aircraft propulsive power unit |
| 05/28/2003 | EP1314839A1 Closure default indicator for aircraft engine cowl panels |
| 05/02/2003 | EP0885141B1 Turbojet pod with laminar flow |
| 03/27/2003 | WO2002079031A3 Integrated and/or modular high-speed aircraft |
| 02/11/2003 | US6516606 Aeroengine nacelle afterbodies |
| 02/04/2003 | US6513841 Blowout latch |
| 01/09/2003 | US20030006089 Fine jet control-type sound absorption system |
| 01/02/2003 | EP1270406A2 Blowout latch |
| 12/26/2002 | US20020195827 Blowout latch |
| 11/12/2002 | US6479124 Composite material panel with shock-protected edges |
| 10/10/2002 | WO2002079031A2 Integrated and/or modular high-speed aircraft |
| 10/10/2002 | CA2434163A1 Integrated and/or modular high-speed aircraft |
| 10/03/2002 | US20020140238 Extendable latch |
| 10/02/2002 | EP1245769A2 Extendable latch |
| 07/25/2002 | US20020096598 Integrated and/or modular high-speed aircraft |
| 07/18/2002 | US20020092948 Apparatus and method for reducing jet engine noise |
| 06/25/2002 | US6409123 Aircraft wing structure profiled suspension pylon |
| 05/28/2002 | US6394389 Aircraft lift arrangement |
| 05/14/2002 | CA2170282C Multi-purpose aircraft |
| 05/02/2002 | EP1066195A4 Permanently connected remote latch mechanism |
| 04/30/2002 | US6378802 Enhance aerodynamic profile |
| 04/23/2002 | US6375121 Method for making a composite panel and resulting panel |
| 04/18/2002 | US20020043807 Safety enhancement method and apparatus |
| 04/17/2002 | EP1197619A1 Blowout latch |
| 03/28/2002 | US20020037231 Spherical gear pump |
| 03/26/2002 | US6360989 Nacelle assembly for a gas turbine engine |
| 03/06/2002 | CN1080228C Turbojet pod |
| 02/21/2002 | WO2002014149A1 Air intake for large-size nacelle with enhanced transportability |
| 02/13/2002 | EP1179473A1 Air intake with improved transportability for an aircraft engine nacelle of large dimensions |
| 01/23/2002 | EP1174341A1 Aircraft jet engine nacelle with an enhanced rear ejection block with common nozzle |
| 01/22/2002 | US6340135 Translating independently mounted air inlet system for aircraft turbofan jet engine |
| 01/17/2002 | US20020006333 Aeroengine nacelle afterbodies |
| 01/17/2002 | US20020006078 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 01/02/2002 | EP1167186A1 Safety enhancement method and safety latch |
| 01/02/2002 | EP1167185A2 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 01/01/2002 | US6334730 Telescopic rod for opening a mobile cowl, in particular of an aircraft engine bay |
| 01/01/2002 | US6334588 Aircraft propulsion unit fan cowls equipped with maintaining and positioning safety elements |
| 12/28/2001 | CA2350970A1 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 12/11/2001 | US6328258 Air intake structure for aircraft engine |
| 12/04/2001 | US6325428 Latch assembly including sensor |
| 10/30/2001 | US6308915 Detachable integral aircraft tailcone and power assembly |
| 10/30/2001 | US6308913 Method for reducing wave resistance in airplane |
| 10/17/2001 | EP1145953A1 Airfoiled engine pylon for aircraft wing |
| 10/11/2001 | US20010028019 Aircraft wing structure profiled suspension pylon |
| 08/28/2001 | US6279971 Latch with sensor |
| 07/31/2001 | US6267327 Coupling system for connecting a gas turbine engine to an aircraft mounted exhaust system |
| 07/04/2001 | EP1112931A2 Aircraft engine and associated aircraft engine cowl |
| 06/12/2001 | US6244539 Detachable integral aircraft tailcone and power assembly |
| 05/29/2001 | US6237325 Bypass turbojet-engine cowling comprising an electrically grounded displaceable component |
| 05/16/2001 | EP1099629A1 Seal fault display in particular for aircraft engine cowl panels |
| 05/16/2001 | EP1099625A1 Aircraft lift arrangement |
| 05/08/2001 | US6227485 Opening device common to two adjacent aircraft engine nacelle covers |
| 04/24/2001 | US6220546 Aircraft engine and associated aircraft engine cowl |
| 04/17/2001 | US6216980 System for closing a pivoting thrust reverser door |
| 04/11/2001 | EP1091059A2 Latch with sensor providing visual indication of the latch position |
| 03/21/2001 | EP1084951A2 A nacelle assembly for a gas turbine engine |
| 03/13/2001 | US6199798 Device for releasably fastening covering panels |
| 03/13/2001 | US6199795 Twin engine aircraft |
| 02/20/2001 | US6189832 Permanently connected remote latch mechanism |