B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for

Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
11/2006
11/30/2006	US20060266412 System, method, and apparatus for designing streamline traced, mixed compression inlets for aircraft engines
11/24/2006	CA2507280A1 Auxiliary, rotatable, independent jet engines on plane fuselage
11/15/2006	CN1863703A Annular acoustic panel
11/08/2006	EP1718857A2 Integrated air inlet system for multi-propulsion aircraft engines
11/07/2006	US7131612 Nacelle inlet lip anti-icing with engine oil
11/02/2006	CA2537678A1 Bushing for thermally independent bypass air metering valve
10/2006
10/26/2006	US20060237261 Acoustic mechanical retainer
10/26/2006	US20060237260 Duct liner acoustic splice
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
10/25/2006	EP1714871A2 Acoustic dampers
10/24/2006	US7125237 Tooling for molding with keys particularly for the production of air intakes without clips
10/24/2006	US7124662 Reversible driving apparatus for PCU pumps
10/18/2006	EP1711726A1 Reversible driving apparatus for pcu pumps
10/17/2006	US7121128 Method of manufacturing elliptic deep-drawn products
10/14/2006	CA2542717A1 Aircraft engine exhaust nozzle
10/10/2006	CA2344128C Method and apparatus for the cooling of jet-engine turbine casings
10/05/2006	US20060219475 Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods
09/2006
09/28/2006	US20060214054 Piston type aircraft engine
09/27/2006	CN1836975A Swinging type aviation mechanism by polarized centrifugal force
09/21/2006	US20060207826 Composite muffler for use with airborne auxiliary power unit
09/20/2006	EP1594738B1 Apparatus and method for providing fireproofing to an oil cooler in an aircraft auxiliary power unit compartment
09/13/2006	EP1699698A1 Ram air channel for the supply of ambient air in an aircraft
09/13/2006	EP1699697A2 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap
09/12/2006	US7104500 Thrust reverser with sliding pivot joints
09/07/2006	US20060196993 Pre-hung inlet door system
09/07/2006	US20060196633 Aircraft fluid cooling system and aircraft provided with said system
08/2006
08/31/2006	US20060192049 Electrical generator fluid-flow-coolant filtration method
08/24/2006	DE102005007940A1 Foreign body e.g. stone, trapping device for use in turbo-prop driving mechanism, is fixed in inlet region of turbo-prop engine and traps foreign body sucked along with air when body hits device at specific velocity
08/23/2006	EP1692428A1 Support device for fire-detection system
08/22/2006	US7093666 Apparatus and method for providing fireproofing to an aircraft auxiliary power unit
08/17/2006	US20060180703 Heat exchanger systems and associated systems and methods for cooling aircraft starter/generators
08/17/2006	US20060179817 Nacelle assembly for a gas turbine engine
08/16/2006	EP1690790A1 Turbine engine arrangements
08/09/2006	CN2803924Y Wings
08/03/2006	US20060169533 Acoustic liner with a nonuniform depth backwall
08/03/2006	US20060169532 Acoustic liner with nonuniform impedance
08/02/2006	EP1685025A1 Aircraft fluid cooling system and an aircraft provided with said system
08/01/2006	US7083144 Apparatus and methods for support of propulsion systems interconnect members
08/01/2006	US7082769 Helicopter turbine engine protection system
07/2006
07/27/2006	US20060163425 Aircraft inlet assembly for reducing auxiliary power unit noise
07/25/2006	CA2531978A1 Auxiliary power unit exhaust duct bellmouth incorporating revolute joints to facilitate installation and removal of said auxiliary power unit
07/06/2006	US20060144959 Rocket engine chamber with layered internal wall channels
06/2006
06/28/2006	EP1674694A2 Compressor intake duct
06/28/2006	EP1673279A1 Annular acoustic panel
06/28/2006	EP1595068A4 Ventilated confluent exhaust nozzle
06/15/2006	US20060124801 Shape changing structure
06/07/2006	EP1663778A2 Variable cam exhaust nozzle
05/2006
05/31/2006	EP1485289B1 Apparatus and method for variation of a wall skin
05/23/2006	US7048230 Laminar flow nacelle for an aircraft engine
05/23/2006	US7047725 Assembly and method for aircraft engine noise reduction
05/23/2006	CA2294620C Cooling device for a gas turbine speed reducer
05/18/2006	WO2006034462A3 Quiet chevron/tab exhaust eductor system
05/18/2006	US20060102781 Dual action inlet door and method for use thereof
05/18/2006	US20060102780 Ducted spinner for engine cooling
05/18/2006	US20060102779 Dual flow APU inlet and associated systems and methods
05/18/2006	US20060102776 Dual action inlet door and method for use thereof
05/17/2006	EP1657156A1 An air intake appliance for an aircraft engine
05/16/2006	CA2414429C Oil receiver
05/11/2006	WO2006049553A1 An outlet device for a jet engine and a jet engine comprising such an outlet device
05/09/2006	US7040576 Fire shield apparatus and method
05/04/2006	CA2523195A1 Pressure lubrication for inverted flight
05/02/2006	CA2398903C Improved aerobatic aircraft
04/2006
04/20/2006	US20060080969 Helicopter turbine engine protection system
04/19/2006	EP1646560A2 Dual action inlet door and method for use thereof
04/18/2006	CA2379091C Supersonic external-compression diffuser and method for designing same
04/13/2006	US20060076456 Thrust/airflow control device
04/06/2006	DE102004046106A1 Drive and wing surface concept for aircraft includes an axial fans built into wing, driven by circular diesel engines
04/04/2006	CA2261730C Detachable integral aircraft tailcone and power assembly
03/2006
03/28/2006	US7017333 Wall structure
03/28/2006	US7017332 Lobe mixer for jet flow
03/23/2006	WO2005016748A3 Dual action inlet door and method for use thereof
03/23/2006	US20060060697 Device for assembly of a shroud placed between an aircraft engine air intake and a pylon
03/23/2006	US20060060417 Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
03/21/2006	US7014145 Variable position intake for an aircraft mounted gas turbine engine
03/21/2006	US7014144 Dual action inlet door and method for use thereof
03/16/2006	US20060054304 Cooling module arrangement with a sealing element
03/14/2006	US7010905 Ventilated confluent exhaust nozzle
03/07/2006	US7007483 Turbine engine nozzle
02/2006
02/23/2006	US20060038064 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop
02/22/2006	EP1257467A4 Improved aerobatic aircraft
02/16/2006	WO2006016031A1 Multi-engine aircraft
02/09/2006	US20060029849 System for water reclamation from an exhaust gas flow of a fuel cell of an aircraft
02/02/2006	US20060021351 Method for resistance welding two sheet metal elements together
01/2006
01/26/2006	US20060016932 Variable position intake for an aircraft mounted gas turbine engine
01/24/2006	US6988674 Method and apparatus for suppressing infrared signatures
01/19/2006	US20060011408 Acoustic liner for gas turbine engine
01/19/2006	CA2509788A1 Foreign object damage tolerant nacelle anti-icing system
01/10/2006	US6983912 Hybrid exhaust heat shield for pylon mounted gas turbine engines
01/10/2006	US6983602 Ejector cooled nozzle
01/04/2006	EP1612769A2 High admittance acoustic liner
12/2005
12/29/2005	US20050284690 High admittance acoustic liner
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
12/21/2005	EP1607611A2 Aircraft propulsion system comprising an apparatus for suppressing infrared signatures
12/21/2005	EP1607328A1 Engine nacelle for supersonic aircraft
12/08/2005	WO2005039978A3 Aircraft protection method and system
12/08/2005	US20050268595 Method and apparatus for suppressing infrared signatures
12/08/2005	US20050268593 Thermal management for aircraft auxiliary power unit compartment
12/06/2005	US6971240 Methods and apparatus for exhausting gases from gas turbine engines

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