| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
|---|
| 01/25/2007 | WO2004101357A3 Homeostatic flying hovercraft |
| 01/23/2007 | US7165744 Turbine engine arrangements |
| 01/10/2007 | EP1740456A1 Aircraft turboprop engine provided with an improved aerodynamic installation |
| 01/10/2007 | EP1451067B1 Disengageable support for engine cowls |
| 01/02/2007 | CA2278548C Telescopic rod for opening a mobile cowl, in particular of an aircraft engine bay |
| 12/21/2006 | WO2006134253A1 Control system for the nacelle of a turboreactor |
| 12/21/2006 | CA2611556A1 Control system for the nacelle of a turboreactor |
| 12/14/2006 | DE10203523B4 Verriegelungs-Vorrichtung zur Verriegelung zweier Strukturteile Locking device for locking two structural parts |
| 12/12/2006 | US7147185 Device for assembly of a shroud placed between an aircraft engine air intake and a pylon |
| 11/15/2006 | CN1863703A Annular acoustic panel |
| 11/07/2006 | US7131672 Latch mechanism |
| 10/25/2006 | EP1715160A1 Aircraft engine nacelle inlet having electrical ice protection system |
| 10/25/2006 | EP1715159A1 Aircraft engine nacelle inlet having access opening for electrical ice protection system |
| 10/17/2006 | US7121512 Drain particularly for engine support strut |
| 10/17/2006 | US7121128 Method of manufacturing elliptic deep-drawn products |
| 10/04/2006 | EP1707718A2 Lock arrangement |
| 09/05/2006 | US7100869 Turboprop carrier structure and an assembly including such a carrier structure |
| 08/17/2006 | US20060179817 Nacelle assembly for a gas turbine engine |
| 08/15/2006 | US7090165 Aeroengine nacelle |
| 08/08/2006 | US7086219 Cowl structure for a gas turbine engine |
| 07/04/2006 | US7070147 Lubricating oil filling structure for an engine |
| 06/29/2006 | WO2006068599A1 Static gas turbine component and method for repairing such a component |
| 06/29/2006 | CA2588470A1 Static gas turbine component and method for repairing such a component |
| 06/28/2006 | EP1673279A1 Annular acoustic panel |
| 05/24/2006 | DE202006002981U1 Aircraft engine and engine shroud parts, has closed edge, where parts are fastened to engine of aircraft, where edge or segment of edge of engine shroud runs into trapezoidal line, and corners of trapezoidal line is rounded |
| 05/10/2006 | EP1654715A2 Wireless engine monitoring system |
| 05/09/2006 | US7040578 Locking the cowl doors of a turbojet |
| 04/04/2006 | CA2261730C Detachable integral aircraft tailcone and power assembly |
| 03/30/2006 | US20060065784 Aircraft provided with a belly fairing, and corresponding belly fairing |
| 03/23/2006 | US20060060697 Device for assembly of a shroud placed between an aircraft engine air intake and a pylon |
| 03/15/2006 | EP1633935A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/14/2006 | CA2193272C Coating for aerospace aluminum parts |
| 03/07/2006 | US7007890 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 02/23/2006 | US20060038064 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop |
| 02/22/2006 | EP1626900A1 Air input device for a turboprop engine |
| 02/09/2006 | US20060027707 Drain particularly for engine support strut |
| 01/25/2006 | CN2753672Y Vector thrust culvert pipe fan type single aircraft |
| 01/19/2006 | US20060011708 Friction plug welding method, for a hole in a metal part, use of a metal bar and of a bearing supporting part for implementing the method |
| 01/10/2006 | US6983912 Hybrid exhaust heat shield for pylon mounted gas turbine engines |
| 01/05/2006 | WO2006000781A1 Fire resistant seal assembly |
| 12/28/2005 | EP1609719A1 Method for braking aircraft and turbo fan jet engine for implementing the method |
| 12/22/2005 | US20050279081 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/14/2005 | EP1604900A1 Aircraft belly fairing and aircraft equipped with said belly fairing |
| 12/08/2005 | WO2004077400A8 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 12/06/2005 | US6971240 Methods and apparatus for exhausting gases from gas turbine engines |
| 12/01/2005 | US20050263643 Cowl structure for a gas turbine engine |
| 11/30/2005 | EP1600240A1 Method for stopping off, using friction welding, of a hole in a metallic part, use of a metallic bar and a support assembly for performing the method. |
| 11/24/2005 | WO2005110845A1 Aircraft turboprop engine provided with an improved aerodynamic installation |
| 11/24/2005 | CA2564619A1 Aircraft turboprop engine provided with an improved aerodynamic installation |
| 11/22/2005 | US6966524 Aircraft engine nacelles and methods for their manufacture |
| 11/15/2005 | US6964397 Nacelle chine installation for drag reduction |
| 11/10/2005 | US20050247821 Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim |
| 11/09/2005 | EP1593594A1 Transition shim between a means for fastening a wing to a fuselage of an aircraft and the wing, and aircraft comprising such a shim |
| 10/27/2005 | CA2505058A1 Process for closing a hole in a metal part by means of friction welding, use of a metal bar and a bearing bracket to carry out the process |
| 10/13/2005 | US20050223693 Engine cooling |
| 10/06/2005 | US20050217239 Methods and apparatus for exhausting gases from gas turbine engines |
| 10/05/2005 | EP1582730A1 Apparatus for exhausting gases from gas turbine engines |
| 09/30/2005 | CA2502374A1 Methods and apparatus for exhausting gases from gas turbine engines |
| 09/29/2005 | WO2005090156A1 Annular acoustic panel |
| 09/29/2005 | US20050211824 Turbine engine arrangements |
| 09/20/2005 | US6945573 Externally adjustable latch |
| 09/06/2005 | US6938854 Integrated and/or modular high-speed aircraft |
| 08/18/2005 | US20050178887 Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position |
| 08/03/2005 | CN1648000A Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 07/26/2005 | US6920958 Annular acoustic panel |
| 07/13/2005 | EP1553019A1 Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 07/12/2005 | CA2222470C Device for linking a thrust reverser to a turbine engine |
| 07/07/2005 | WO2004077400B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 07/05/2005 | US6913297 Rotary latch mechanism |
| 06/22/2005 | EP1544106A1 Drain in particular for engine pylon support |
| 06/01/2005 | EP1535840A1 Device for mounting a fairing between a nacelle of an aircraft engine and a pylon |
| 05/26/2005 | US20050109557 Soundproofing panel with beads, and a method of manufacture |
| 05/25/2005 | EP1533787A1 Sound insulation panel containing balls and method for producing it |
| 05/17/2005 | US6892526 Cowl structure for a gas turbine engine |
| 05/10/2005 | US6889939 Device for fixing a member to an aircraft structure |
| 04/28/2005 | US20050087996 Rotary latch mechanism |
| 04/21/2005 | US20050082112 Annular acoustic panel |
| 04/20/2005 | EP1524190A2 Engine cooling |
| 04/12/2005 | CA2213792C Aircraft labyrinth fire seal |
| 03/29/2005 | US6871725 For use in a sound attenuation panel in the high velocity air flow region of an engine nacelle |
| 03/24/2005 | US20050060982 Method and system for reduction of jet engine noise |
| 03/23/2005 | EP1517022A2 Method and system for reduction of jet engine noise |
| 03/22/2005 | US6869046 Aircraft propulsive power unit |
| 03/17/2005 | US20050056726 Closure panel arrangement |
| 03/16/2005 | EP1515006A1 A closure panel arrangement |
| 03/03/2005 | US20050045774 Laminar flow nacelle for an aircraft engine |
| 03/03/2005 | US20050045767 Locking the cowl doors of a turbojet |
| 02/10/2005 | WO2004077400A3 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 02/03/2005 | US20050024815 Latch fuse |
| 02/03/2005 | US20050023411 Lubricating oil filling structure for an engine |
| 01/20/2005 | US20050011993 Nacelle chine installation for drag reduction |
| 01/20/2005 | US20050011988 Aircraft configuration |
| 01/05/2005 | EP1493665A1 Aircraft configuration for attenuation of engine noise |
| 01/05/2005 | EP1493664A1 Latch for turbine nacelle cowls |
| 01/04/2005 | US6837459 Air intake for large-size nacelle with enhanced transportability |
| 12/23/2004 | US20040255572 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls |
| 12/22/2004 | EP1488999A1 Aircraft engine cowling with reduced gap |
| 12/02/2004 | US20040238687 Aeroengine nacelle |
| 11/30/2004 | US6824175 Device for indicating incorrect closure of locking means located between two fan cowlings of an aircraft engine nacelle |
| 11/18/2004 | US20040227033 Turboprop carrier structure and an assembly including such a carrier structure |