| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
|---|
| 10/29/2008 | EP1984248A1 Turbojet engine nacelle with lateral opening of covers |
| 10/23/2008 | US20080258016 Nacelle assembly without lower bi-fi splitter |
| 10/22/2008 | EP1982915A1 Flexible suspension for a turboengine |
| 10/21/2008 | CA2327374C Aircraft wing-shaped suspension mast |
| 10/16/2008 | CA2629096A1 Flexible suspension |
| 10/14/2008 | US7434303 Nacelle assembly for a gas turbine engine |
| 10/09/2008 | WO2008093003A8 Nacelle for turbofan |
| 10/08/2008 | EP1976758A1 Fixing system for a component of a turbojet pod |
| 10/07/2008 | CA2343432C Streamlined suspension strut for aircraft centre section |
| 10/02/2008 | WO2008085542A3 Aircraft engine inlet having zone of deformation |
| 09/25/2008 | WO2008113737A1 Rear lower aerodynamic fairing for the attachment device of an aircraft engine |
| 09/17/2008 | CN101267983A Engine suspension device inserted between an aircraft wing and said engine |
| 09/03/2008 | CN101258072A Nacelle cowling for turbojet and nacelle comprising at leastone such cowling |
| 08/28/2008 | WO2008102068A1 Nacelle for the jet engine of an aircraft |
| 08/28/2008 | CA2677423A1 Nacelle for the jet engine of an aircraft |
| 08/07/2008 | WO2008093003A1 Nacelle for turbofan |
| 08/07/2008 | CA2671556A1 Nacelle for turbofan |
| 08/05/2008 | US7407135 Aircraft provided with a belly fairing, and corresponding belly fairing |
| 07/30/2008 | CN101229849A Intake oblique cut inlet and method for designing the same |
| 06/18/2008 | EP1932759A1 Protection panel for aircrafts |
| 06/11/2008 | EP1928738A1 Engine mounting structure interposed between an aircraft wing system and said engine |
| 06/11/2008 | CN101198785A Control system for the nacelle of a turboreactor |
| 06/04/2008 | EP1927711A2 Command latch and pin latch system |
| 05/29/2008 | WO2008061336A1 Turbofan gas turbine engine and nacelle arrangement |
| 05/22/2008 | WO2008058368A1 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/22/2008 | US20080116323 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/22/2008 | CA2666190A1 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/21/2008 | EP1923310A2 Nacelle drag reduction device for a turbofan gas turbine engine |
| 05/21/2008 | EP1922251A1 Nacelle cowling for turbojet and nacelle comprising at least one such cowling |
| 05/21/2008 | CN101181934A Inlet seriously distorted lower asymmetric unsteady generator |
| 05/21/2008 | CA2610096A1 Articles comprising composite structures having mounting flanges |
| 05/20/2008 | CA2281172C Nacelle for grounded moving component turbofan |
| 05/08/2008 | WO2008053088A1 Jet engine nacelle member |
| 05/08/2008 | WO2008053087A1 Side-opening jet engine nacelle |
| 05/08/2008 | US20080105781 Aircraft with reduced environmental impact |
| 05/08/2008 | CA2666747A1 Jet engine nacelle member |
| 05/08/2008 | CA2666614A1 Side-opening jet engine nacelle |
| 04/30/2008 | CA2590892A1 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof |
| 04/10/2008 | WO2008040877A1 Removable air intake structure for turbojet engine nacelle |
| 04/10/2008 | CA2664034A1 Removable air intake structure for turbojet engine nacelle |
| 04/02/2008 | EP1905998A2 Asymmetric Serrated Nozzle For Exhaust Noise Reduction |
| 04/02/2008 | EP1905689A1 Integrated propulsion system comprising a turbofan engine |
| 03/28/2008 | CA2601288A1 Turbine exhaust case cowling for a gas turbine engine |
| 03/26/2008 | EP1902952A1 Fan conduit for a turbomachine |
| 03/26/2008 | EP1902951A1 Aircraft propulsion system with integrated pylon |
| 03/26/2008 | EP1740456B1 Aircraft turbine engine provided with an improved aerodynamic installation |
| 03/26/2008 | CN101148199A Non-axial-symmetry combination processing machine box |
| 03/20/2008 | CA2602176A1 Propellant system with integrated pylon for aircraft |
| 03/20/2008 | CA2602141A1 Integrated propellant system that includes a by-pass engine |
| 03/19/2008 | EP1351855A4 Integrated and/or modular high-speed aircraft |
| 03/11/2008 | US7341225 Aircraft wing and aeroengine arrangement for attenuating engine noise |
| 03/06/2008 | WO2008025890A1 Locking system for a movable nacelle cowl |
| 03/06/2008 | CA2659334A1 Locking system for a movable nacelle cowl |
| 03/05/2008 | EP1633935A4 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/05/2008 | EP1626900B1 Air input device for a turboprop engine |
| 03/05/2008 | CN101134508A Fan exhaust nozzle for turbofan engine |
| 02/29/2008 | CA2598304A1 Fan exhaust nozzle for turbofan engine |
| 02/27/2008 | EP1891318A1 Control system for the nacelle of a turboreactor |
| 02/26/2008 | US7334393 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls |
| 02/14/2008 | WO2007147965A3 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft |
| 02/07/2008 | WO2008015362A1 Structural element of an aircraft |
| 02/07/2008 | CA2659821A1 Element de structure d'un aeronef |
| 01/17/2008 | WO2008006826A1 Engine assembly for aircraft comprising an aerodynamic coupling fairing mounted on two separate elements |
| 01/17/2008 | CA2657402A1 Aircraft engine assembly comprising a junction aerodynamic fairing mounted on two separate elements |
| 01/16/2008 | CN101104441A Gas turbine engine and method of operating same |
| 01/03/2008 | WO2008000924A1 Structural nacelle |
| 01/03/2008 | US20080001038 Fuel cell/combustor systems and methods for aircraft and other applications |
| 01/03/2008 | CA2654398A1 Structural nacelle |
| 12/27/2007 | WO2007147965A2 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft |
| 12/27/2007 | CA2653067A1 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft |
| 12/12/2007 | CN101087928A Static gas turbine component and method for repairing such a component |
| 11/29/2007 | WO2007135270A1 Aircraft comprising a device for reducing the induced drag |
| 11/29/2007 | CA2650194A1 Aircraft equipped with a device for reducing induced drag |
| 10/11/2007 | WO2007113183A1 Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel |
| 10/11/2007 | CA2647762A1 Aircraft wing arrangement comprising an engine attachment strut defining in the front zone a lateral air flow channel |
| 10/09/2007 | CA2394296C Air intake for large-size nacelle with enhanced transportability |
| 10/04/2007 | WO2007110491A1 Air inlet shroud structure |
| 10/04/2007 | CA2637901A1 Air inlet shroud structure |
| 09/25/2007 | CA2292914C Air intake structure for aircraft engine |
| 09/20/2007 | US20070217913 Turboprop Unit For Aircraft With Improved Aerodynamic Installation |
| 09/12/2007 | EP1831505A1 Static gas turbine component and method for repairing such a component |
| 09/11/2007 | CA2281619C Aircraft propulsion unit with fan cowls equipped with maintaining and positioning safety elements |
| 08/23/2007 | WO2007093683A1 Turbojet engine nacelle with lateral opening of covers |
| 08/23/2007 | CA2642300A1 Turbojet engine nacelle with lateral opening of covers |
| 08/14/2007 | US7255307 Closure panel arrangement |
| 08/01/2007 | CN2928682Y Adjustable engine front cover ring |
| 07/26/2007 | WO2007083024A1 Fixing system for a component of a turbojet pod |
| 07/26/2007 | CA2637892A1 Fixing system for a component of a turbojet pod |
| 07/24/2007 | CA2411583C Lubricating oil filling structure for an engine |
| 07/18/2007 | EP0954469B1 Method for making a composite panel and resulting panel |
| 04/24/2007 | CA2247176C Laminar flow jet engine bay |
| 04/17/2007 | US7204458 Closing system interposed between two elements |
| 04/05/2007 | WO2007036519A1 Engine mounting structure interposed between an aircraft wing system and said engine |
| 04/05/2007 | CA2623792A1 Engine suspension device inserted between an aircraft wing and said engine |
| 04/04/2007 | EP1770011A2 Method of forming a composite panel |
| 03/22/2007 | US20070063097 Air input device for a turboprop engine |
| 03/21/2007 | EP1764499A1 Thrust reverser including a latching mechanism and method of manufacturing such a thrust reverser |
| 03/15/2007 | WO2007028916A1 Nacelle cowling for turbojet and nacelle comprising at least one such cowling |
| 03/15/2007 | CA2621216A1 Nacelle cowling for turbojet and nacelle comprising at least one such cowling |
| 02/06/2007 | US7172223 Magnetically reactive pivot latch system |