Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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12/10/2008 | EP1999022A1 Air inlet shroud structure |
12/10/2008 | EP1999021A1 Air inlet lip for a pod with electric defrosting |
12/10/2008 | EP1999020A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
12/09/2008 | US7461814 Dual action inlet door and method for use thereof |
12/09/2008 | US7461813 Air input device for a turboprop engine |
12/09/2008 | CA2538806C Annular acoustic panel |
12/04/2008 | WO2008145725A1 Propulsion assembly for aircraft with sliding nacelle |
12/04/2008 | US20080296440 Flow distribution system for inlet flow control |
12/04/2008 | CA2689111A1 Propulsion assembly for aircraft with sliding nacelle |
12/03/2008 | EP1998029A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operating method |
12/03/2008 | EP1998028A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operation method |
12/03/2008 | EP1692428B1 Support device for fire-detection system |
12/02/2008 | CA2447604C Smart surge bleed valve system and method |
11/27/2008 | WO2008142289A2 Air intake arrangement for a vehicle, in particular an aircraft |
11/27/2008 | WO2008142242A2 Nacelle rear assembly for turbojet engine |
11/27/2008 | CA2687454A1 Nacelle rear assembly for turbojet engine |
11/27/2008 | CA2681931A1 Air intake arrangement for a vehicle, in particular an aircraft |
11/20/2008 | WO2008097325A3 Airfoil having a movable control surface |
11/20/2008 | US20080283676 Variable contraction ratio nacelle assembly for a gas turbine engine |
11/13/2008 | WO2008102079A3 Nacelle for aircraft jet engine and aircraft including such nacelle |
11/13/2008 | US20080276596 Engine Wall Structure and a Method of Producing an Engine Wall Structure |
11/12/2008 | EP1989109A2 Infrared suppression system with spiral septum |
11/12/2008 | EP1718857A4 Integrated air inlet system for multi-propulsion aircraft engines |
11/06/2008 | WO2008132321A1 Lockable guiding system for a mobile part of a nacelle |
11/06/2008 | WO2008104716A3 Method for making an acoustic treatment coating and coating thus obtained |
11/06/2008 | CA2677567A1 Lockable guiding system for a mobile part of a nacelle |
11/05/2008 | EP1988266A2 Nacelle assembly having inlet airfoil for a gas turbine engine |
10/29/2008 | EP1985538A2 Using a stiffener to repair a part for an aircraft engine. |
10/28/2008 | CA2330397C Aircraft airfoil leading edge member equipped with a de-icing device |
10/16/2008 | DE102007017428A1 Ansaugschnorchel eines Luftansaugtrakts zum Ansaugen von Verbrennungsluft für eine Brennkraftmaschine The air intake tract of an intake snorkel for the intake of combustion air for an internal combustion engine |
10/14/2008 | US7434765 Heat exchanger systems and associated systems and methods for cooling aircraft starter/generators |
10/14/2008 | US7434303 Nacelle assembly for a gas turbine engine |
10/09/2008 | WO2008059168A3 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
10/09/2008 | US20080245930 High intensity laser power beaming receiver for space and terrestrial applications |
10/09/2008 | US20080245062 Passive cooling system for auxiliary power unit installation |
10/07/2008 | US7431126 Support means for an acoustic liner used in an auxiliary power unit exhaust muffler |
10/07/2008 | US7431125 Composite muffler for use with airborne auxiliary power unit |
10/01/2008 | CN101277871A Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
09/30/2008 | US7429018 Variable fluid intake with ramp and inflatable bag |
09/25/2008 | WO2008115273A2 Tandem air inlet apparatus and method for an airborne mobile platform |
09/18/2008 | WO2008045108A3 Isentropic compression inlet for supersonic aircraft |
09/18/2008 | US20080223992 High-Performance Low-Noise Aircraft Exhaust Systems and Methods |
09/17/2008 | CN101267986A 2387354t engine assembly comprising an engine and a suspension pylon for such an engine |
09/16/2008 | CA2623644A1 Nozzle with yaw vectoring vane |
09/11/2008 | US20080217466 Auxiliary on board power system for an aircraft |
09/10/2008 | EP1967449A2 Systems and methods for reducing pressure loss of air flowing froma first area to a second area |
09/04/2008 | US20080210778 Aircraft engine exhaust shroud |
09/04/2008 | CA2678476A1 Process for producing a coating for acoustic treatment including aclose d cell structure with a complex form and coating for acoustic treatment thus obtained |
08/28/2008 | WO2008102079A2 Nacelle for aircraft jet engine and aircraft including such nacelle |
08/28/2008 | US20080206044 Noise reduction assembly for aircraft turbojet |
08/28/2008 | US20080203218 Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area |
08/28/2008 | CA2674260A1 Nacelle for aircraft jet engine and aircraft including such nacelle |
08/27/2008 | EP1960266A2 Isentropic compression inlet for supersonic aircraft |
08/27/2008 | CN101253095A Dynamically self-locking catching device |
08/27/2008 | CA2621838A1 Aircraft engine equipped with means to transfer heat |
08/27/2008 | CA2621837A1 Aircraft engine oil removal system |
08/21/2008 | WO2008076471A3 Aircraft engine inlet pivotable barrier filter |
08/21/2008 | WO2008054500A3 Integrated engine exhaust systems and methods for drag and thermal stress reduction |
08/19/2008 | CA2621711A1 Process for drawing back-up power from a jet turbine engine and turbine engine equipped to implement such a process |
08/19/2008 | CA2328555C Hot air evacuation device for the nose inlet cowl of a jet engine, with de-icing system |
08/14/2008 | WO2008097325A2 Airfoil having a movable control surface |
08/07/2008 | WO2008093447A1 Low noise aircraft |
08/07/2008 | WO2008059169A3 Aircraft leading edge |
08/07/2008 | WO2008059169A2 Aircraft leading edge |
08/07/2008 | WO2008016341A3 Engine intake system with accessible, interchangeable air filters |
08/07/2008 | US20080185215 Integrated inlet attachment |
08/07/2008 | DE10361644B4 Luftleitklappe eines Luftfahrzeuges mit Regelung der auf sie wirkenden Druckkräfte, und Stauluftsystem mit einer solchen Luftleitklappe Air guiding an aircraft with control of the pressure forces acting on them, and ram air system with such a flow-rate control |
08/06/2008 | CN101238033A Unmanned helicopter |
08/06/2008 | CN100408431C Aircraft fluid cooling system and an aircraft provided with said system |
07/31/2008 | US20080179466 Dual Flow APU Inlet and Associated Systems and Methods |
07/31/2008 | US20080179448 Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
07/24/2008 | US20080174177 System and method for supplying power for actuators on board an aircraft |
07/24/2008 | US20080173768 Power plant for a rotary wing aircraft |
07/22/2008 | CA2204386C Self-locking sealing device |
07/16/2008 | EP1943419A2 Infrared suppression system |
07/10/2008 | US20080164378 Boundary-Layer-Ingesting Inlet Flow Control System |
07/09/2008 | CN101214857A Backpack S-shaped inlet channel |
07/08/2008 | US7395657 Flade gas turbine engine with fixed geometry inlet |
07/03/2008 | US20080156943 Cooled airfoil component |
06/26/2008 | WO2008076471A2 Aircraft engine inlet pivotable barrier filter |
06/26/2008 | WO2008014058A3 Jet engine exhaust nozzle flow effector |
06/18/2008 | EP1931870A1 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
06/18/2008 | CN101200220A Systems and methods for passively directing aircraft engine nozzle flows |
06/13/2008 | CA2605518A1 Engine propulsion system and methods of assembling the same |
06/12/2008 | US20080135689 Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems |
06/12/2008 | US20080135329 Monolithic acoustically-treated engine nacelle inlet panels |
06/11/2008 | EP1928744A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
06/11/2008 | EP1928743A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
06/10/2008 | CA2501766C Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
06/10/2008 | CA2442859C Tortuous path exhaust eductor system |
06/04/2008 | EP1928216A1 Inlet electromagnetic flow control |
06/03/2008 | CA2454362C Engine including electrical interference shield |
05/29/2008 | US20080120978 Propulsion system |
05/29/2008 | CA2569179A1 Vectorable nozzle with pivotable triangular panels |
05/28/2008 | EP1924498A1 Dynamically self-locking catching device |
05/22/2008 | WO2008059168A2 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
05/22/2008 | WO2008059167A2 Process and installation for anaerobic treatment of material having a high solids concentration |
05/22/2008 | CA2669178A1 Aircraft leading edge |
05/22/2008 | CA2669173A1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
05/20/2008 | CA2281172C Nacelle for grounded moving component turbofan |