Patents
Patents for B64C 7 - Structures or fairings not otherwise provided for (830)
08/2009
08/26/2009EP2091812A1 Wing of an aircraft
08/19/2009CN101512212A Method for manufacturing a panel assembly
08/18/2009CA2389856C Aircraft with belly fairing and gasket for such aircraft
08/12/2009CN101503114A Vertically taking off and landing flyer with ring shaped wing
08/06/2009WO2009095910A2 Apparatus for splitting and removing a shroud from an airborne vehicle
07/2009
07/28/2009CA2397190C Aircraft having a belly fairing, and seal joint for such aircraft
07/23/2009US20090184204 Distribution of point loads in honeycomb panels
07/02/2009WO2009080904A1 Aircraft nacelle guidance system installation
07/02/2009DE102007062111A1 Shielding arrangement for lightning protection of e.g. electrical conductor, in aircraft, has installation space protectively arranged in region of floor framework, and delimitation surface provided with electrical conducting shield
07/02/2009CA2705598A1 Aircraft nacelle guidance system installation
06/2009
06/25/2009WO2009053573A3 Reinforced block made from composite material and method for reinforcing a composite block
06/18/2009WO2009042549A3 Method for manufacturing and attachment of wing fairings
06/18/2009CA2647439A1 Intermediate casing extension for an aircraft jet engine, comprising a sectorised annular groove for receiving the nacelle covers
06/18/2009CA2647438A1 Intermediate casing for an aircraft jet engine, of improved design
06/10/2009CN100497089C Fibre-reinforced metal/ceramic sheet-like composite container casing and its manufacture method
06/04/2009WO2009029306A3 Aerospace vehicle fairing systems and associated methods
06/03/2009CN101448701A Aircraft comprising a device for reducing the induced drag
05/2009
05/20/2009EP2059714A1 Method for manufacturing a panel assembly
05/13/2009EP1945502B1 Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
04/2009
04/30/2009WO2009053573A2 Reinforced block made from composite material and method for reinforcing a composite block
04/30/2009US20090109223 System and Method for Virtual Journey Futuring
04/30/2009US20090108649 System and method for an anticipatory passenger cabin
04/30/2009US20090107620 Manufacturing method for composite material structural component for aircraft and its structural component
04/30/2009CA2702009A1 Reinforced block made from composite material and method for reinforcing a composite block
04/29/2009EP2051906A2 Aerodynamic device for improvement of sustentation coefficient
04/21/2009US7520465 Aircraft fluid cooling system and aircraft provided with said system
04/16/2009DE102008018249A1 Flugzeug mit Kraftübertragungselement zwischen einem Kabinenstrukturelement und einer Primärstruktur Aircraft power transmission element between a cabin structural element and a primary structure
04/15/2009CN101410294A Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel
04/09/2009WO2009043635A1 Locking device comprising a telescopic connecting rod equipped with return means
04/09/2009CA2696831A1 Locking device comprising a telescopic connecting rod equipped with return means
04/02/2009WO2009042549A2 Method for manufacturing and attachment of wing fairings
04/02/2009US20090084894 Landing gear
03/2009
03/26/2009US20090078825 Method for manufacturing and attachment of wing fairings
03/25/2009EP2038176A1 Engine assembly for aircraft comprising an aerodynamic coupling fairing mounted on two separate elements
03/19/2009DE202008012308U1 Schwingungsgedämpftes Befestigungsmittel für Haltemittel in Fahrzeugzellen Vibration-damped mounting means for retaining means in vehicle cells
03/19/2009DE202008012307U1 Befestigungsmittel für Haltemittel von Einbauteilen in Fahrzeugzellen, mit stufenlos einstellbarem Adapter Attachment means for holding means of built-in components in vehicle cells, with infinitely adjustable adapter
02/2009
02/26/2009WO2008151843A4 Engine nacelle of an aircraft comprising a vortex generator arrangement
02/04/2009EP2019776A1 Aircraft comprising a device for reducing the induced drag
02/04/2009EP2019775A1 Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel
02/03/2009US7484688 Landing gear noise reduction
01/2009
01/15/2009US20090014588 Aircraft structural element provided with a cavity and drainage element
01/13/2009US7475848 Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
12/2008
12/30/2008US7469528 Aircraft braking method and ducted fan jet engine for implementing the method
12/18/2008WO2008151843A1 Engine nacelle of an aircraft comprising a vortex generator arrangement
12/18/2008WO2008127481A3 Fuel range for an aircraft
12/18/2008DE102007027697A1 Eddy generator arrangement for use at engine nacelle of aircraft, has eddy generators provided at side of engine nacelle at mutual distance from each other with respect to circumferential or longitudinal direction of engine nacelle
12/17/2008CN101326099A Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing
12/11/2008US20080305000 Aluminum-magnesium-silver based alloys
12/02/2008US7458542 Landing gear door assembly
11/2008
11/18/2008CA2382773C A fairing arrangement for an aircraft
11/13/2008WO2008135647A1 Aircraft landing gear provided with at least one noise reducing means
11/13/2008CA2680530A1 Train d'atterrissage d'avion pourvu d'au moins un moyen de reduction de bruit
11/12/2008CN101304918A Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
11/06/2008WO2008134193A1 Deployable flap edge fence
10/2008
10/21/2008CA2327374C Aircraft wing-shaped suspension mast
10/08/2008EP1977969A1 Method of reducing the aerodynamic noise generated by an aircraft landing gear
10/07/2008CA2343432C Streamlined suspension strut for aircraft centre section
10/01/2008CN101277869A Polyurethane lacquers as abrasion-resistant coatings
09/2008
09/24/2008CN101272950A Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
08/2008
08/26/2008US7416155 Canard position and dihedral for boom reduction and pitch/directional control
08/20/2008EP1957361A1 Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing
08/06/2008CN100408431C Aircraft fluid cooling system and an aircraft provided with said system
08/05/2008US7407136 Static port skin applique apparatus and method
08/05/2008US7407135 Aircraft provided with a belly fairing, and corresponding belly fairing
07/2008
07/31/2008WO2008071399B1 Wing of an aircraft
07/31/2008DE102007011627A1 Innenverkleidung für ein Luftfahrzeug Interior trim for an aircraft
07/30/2008CN101233045A Rotor hub fairing system for a counter-rotating, coaxial rotor system
07/24/2008US20080173759 Apparatus with an expanding band drive, and its use in aircraft construction
07/24/2008DE202008004151U1 Befestigungsanordnung Mounting arrangement
07/24/2008DE102007003273A1 Lokalisierte Bearbeitung von verstärkten Schaumwerkstoffen sowie Kernverbundbauteil Localized processing of reinforced cellular materials and sandwich component
07/23/2008EP1945502A1 Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
07/17/2008US20080169383 Support Structure For a Retractable and Extendable Flap, and Use of Said Structure
07/17/2008DE202008005734U1 Modulares System zur Befestigung von vorzugsweise Leitungen oder Rohren in einem Flugzeug Modular system for the attachment of pipes or tubes, preferably in a plane
07/17/2008DE202007014781U1 Ablenkvorflügel Ablenkvorflügel
07/09/2008EP1940680A2 Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
07/08/2008CA2281130C A process for making a dismountable and/or fixed traction-compression coupling to be applied to composite materials
07/03/2008WO2008054360A3 Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
07/02/2008EP1939460A2 Intertial particle separator for compressor shroud bleed
07/02/2008EP1937553A1 Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
06/2008
06/26/2008US20080152500 Inertial particle separator for compressor shroud bleed
06/19/2008WO2008071399A1 Wing of an aircraft
06/19/2008CA2672068A1 Wing of an aircraft
06/18/2008EP1931565A1 Polyurethane lacquers as abrasion-resistant coatings
06/12/2008DE102006058006A1 Anordnung und Verfahren zur Montage eines Bauelements in einem Flugzeug Arrangement and method for mounting a component in an aircraft
06/11/2008CN101196203A Composite device for accelerating movement body and energy-saving with fluid cavity
05/2008
05/14/2008CN101180209A 航空飞行器整流装置系统及相关方法 Aviation aircraft fairing systems and associated methods
05/08/2008US20080105402 Combined thermal protection and surface temperature control system
05/07/2008EP1918203A1 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof
05/07/2008EP1918194A2 Ventral fairing for an aircraft
04/2008
04/17/2008DE102006048376A1 Cabin structure unit for mounting cabin installation unit for airplane, has reinforcing rib arranged between support frames, where structure unit is designed in self-supportable manner and is mounted in airplane and floor structures
04/17/2008DE102005012610B4 Klemmhalter Toolholder
04/10/2008DE102005042400B4 Crashsicherheiterhöhende Ausrüstungs-Befestigungsvorrichtung eines Luftfahrzeugs Crashsicherheiterhöhende Equipment attachment device of an aircraft
04/01/2008US7350752 Fairing and installation methodology for sensor pressure belts
03/2008
03/27/2008US20080073465 Multi-Layer Interior Fitting Component
03/27/2008DE102006043020A1 Carrier unit for use in fastening system for fastening e.g. seat of aircraft, has coupling section connecting vehicle part section at carrier section and comprising uniformly engaged cross section profile in longitudinal direction of unit
03/19/2008EP1351855A4 Integrated and/or modular high-speed aircraft
03/13/2008WO2008029048A1 Method for manufacturing a panel assembly
03/13/2008DE102006040383A1 Deflector trap for rainwater or de-icing fluid retracts into recess above fuselage entry door
03/13/2008DE102006039292A1 Frame element for use in aircraft air-conditioning system, has longitudinal struts, each having air-inlet connection connected to air-conditioning unit, and air-outlet connection connected to cabin region
03/13/2008DE102006039291A1 Frame element for use in installation of storage bin in aircraft, has longitudinal parallel struts that extend parallel to ribs of aircraft structure, when frame element is mounted to aircraft structure
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