| Patents for B64C 3 - Wings (5,458) |
|---|
| 01/08/2009 | CA2690988A1 Elongate composite structural members and improvements therein |
| 01/07/2009 | EP1544099B1 Method of joining structural elements in an aircraft |
| 01/07/2009 | CN101341070A A joint for use in aircraft construction |
| 01/06/2009 | CA2314162C Assembly procedure for a flexible panel for an open structure and system for implementing the procedure |
| 01/02/2009 | DE102007030095A1 Rotorblatt für ein Drehflügelflugzeug Rotor blade for a rotary wing aircraft |
| 01/02/2009 | DE102007030026A1 Strukturbauteil mit Spant- und Querträgerelement Structural component with direction of the ribs and cross member |
| 01/02/2009 | DE102007029500A1 Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil Method for coupling stiffening profile elements and structural component |
| 01/01/2009 | US20090001225 High lift longitudinal axis control system |
| 01/01/2009 | US20090001223 Flexible Control Surface for an Aircraft |
| 01/01/2009 | US20090001218 Stifffened multispar torsion box |
| 12/31/2008 | WO2009002279A2 Sequential wing |
| 12/31/2008 | WO2009000911A2 Stiffened multispar torsion box |
| 12/31/2008 | CN101336192A Flexible control surface for an aircraft |
| 12/31/2008 | CA2692289A1 Stiffened multispar torsion box |
| 12/24/2008 | WO2008155720A2 Method and equipment for forming and assembling uncured spars for the horizontal stabilizers of aircraft |
| 12/24/2008 | DE102007027137A1 Brake unit for drive system for landing e.g. airbrake of aircraft, has brake electrically or hydraulically operated for configuring and/or releasing drive element, and mechanically operated at same time for limiting torque |
| 12/24/2008 | CN101331060A Assembly of aircraft components |
| 12/24/2008 | CN101331002A Structural element and method of manufacture |
| 12/24/2008 | CA2686628A1 Aluminium alloy products having improved property combinations and method for artificially aging same |
| 12/23/2008 | CA2617137C Aircraft wing modification and related methods |
| 12/18/2008 | US20080308669 composite aircraft component |
| 12/18/2008 | DE10302514B4 Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts Fluidically effective area of a moving fluid in a device, in particular an aircraft, in particular wing of an aircraft |
| 12/18/2008 | DE102007027697A1 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 |
| 12/17/2008 | EP2001739A1 Aerodynamic or hydrodynamic profile which can be deformed in a continuous and controlled manner |
| 12/17/2008 | CN201165329Y Wing tip injector capable of greatly saving energy and reducing emission of aeroplane |
| 12/17/2008 | CN101323371A Lift augmenter with united jet flow structure on wing flap |
| 12/13/2008 | CA2634732A1 Exhaust casing hub having stress distribution ribs |
| 12/11/2008 | WO2008150714A1 Bladderless mold line conformal hat stringer |
| 12/11/2008 | WO2008150712A1 Manufacturing process using bladderless mold line conformal hat stringer |
| 12/11/2008 | WO2007140147A3 Actuator and flap arrangement with actuator interconnection |
| 12/11/2008 | US20080305000 Aluminum-magnesium-silver based alloys |
| 12/11/2008 | US20080302919 Symmetric leading edge device and method to delay flow separation |
| 12/11/2008 | US20080302918 Control surface assemblies with torque tube base |
| 12/11/2008 | DE102007026765A1 Tragflügel mit verstellbarem Spoiler Wing with adjustable spoiler |
| 12/10/2008 | EP1999013A1 Aircraft component |
| 12/10/2008 | EP1766102B1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 12/10/2008 | CN101318551A Quick wing tip vortex weakening apparatus |
| 12/09/2008 | US7461820 Aerofoil arrangement |
| 12/04/2008 | WO2008125868A3 Aircraft |
| 12/04/2008 | US20080296428 Air Freight Transport Method, Transport Aeroplane and Air Freight Transport System |
| 12/04/2008 | CA2820246A1 High-lift device, wing, and noise reduction structure for high-lift device |
| 12/03/2008 | EP1997953A1 Cover fabric for aircraft |
| 11/27/2008 | WO2008054499A3 Composite wing-body joint |
| 11/27/2008 | DE102007024372A1 Verfahren und Einrichtung zur Lärmreduzierung an einem Hochauftriebssystem am Tragflügel eines Flugzeugs Method and apparatus for reducing noise in a high-lift system on the wing of an airplane |
| 11/27/2008 | DE102007024371A1 Verfahren und Einrichtung zur Strömungskontrolle an einem Hochauftriebssystem am Tragflügel eines Flugzeugs Method and apparatus for flow control in a high-lift system on the wing of an airplane |
| 11/25/2008 | US7455264 Reconfiguration control system for an aircraft wing |
| 11/20/2008 | WO2008139214A1 Reinforced panel |
| 11/20/2008 | WO2008138331A1 Covering fabric for aircraft in general air travel |
| 11/20/2008 | WO2007117275A3 An airfoil for a helicoptor rotor blade |
| 11/20/2008 | US20080283675 Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft |
| 11/20/2008 | US20080283674 Low-drag swept wings |
| 11/20/2008 | US20080283672 Drive system for a variable camber aircraft wing |
| 11/20/2008 | DE102007023394A1 Verfahren und Einrichtung zur Fehlerdetektierung im Lastpfad eines Spindelaktuators Method and apparatus for error detection in the load path of a Spindelaktuators |
| 11/20/2008 | CA2852191A1 Robot-deployed assembly tool and method for installing fasteners in aircraft structures |
| 11/20/2008 | CA2685505A1 Covering fabric for aircraft in general aviation |
| 11/20/2008 | CA2684551A1 Reinforced panel |
| 11/19/2008 | EP1991459A1 Aircraft wing |
| 11/19/2008 | CN101306722A Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft |
| 11/19/2008 | CN100434634C Contact stiffeners for structural skins |
| 11/18/2008 | US7451950 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint |
| 11/18/2008 | CA2519871C Winged spacecraft |
| 11/18/2008 | CA2459167C Composite material structure |
| 11/13/2008 | US20080277526 Aircraft Cooling Duct |
| 11/13/2008 | DE102007021748A1 Antriebssystem für einen wölbvariablen Flugzeugflügel Drive system for an aircraft wing wölbvariablen |
| 11/13/2008 | DE102007020952A1 Tragflügel für ein Luftfahrzeug mit einer in Faserverbundbauweise ausgebildeten tragenden Struktur Aerofoil for an aircraft having an opening formed in composite design supporting structure |
| 11/13/2008 | DE102007020870A1 Hochauftriebssystem am Tragflügel eines Flugzeugs High lift system on the wing of an airplane |
| 11/11/2008 | US7448578 Aircraft with forward opening inlay spoilers for yaw control |
| 11/06/2008 | WO2008132498A1 Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces |
| 11/06/2008 | WO2008132251A1 Multispar torsion box made from composite material |
| 11/06/2008 | WO2008132050A1 Fibre metal laminate panel |
| 11/06/2008 | US20080272615 Airflow control devices based on active materials |
| 11/06/2008 | US20080272244 Hybrid Aircraft |
| 11/06/2008 | US20080272226 Ducted Fan Air Vehicle with Deployable Wings |
| 11/06/2008 | DE102007021076A1 Inter-costal arrangement for aircraft or spacecraft, has cross-member movable between a first and a second position for relieving loading between struts |
| 11/06/2008 | DE102007021075A1 Verbindungsanordnung zum Verbinden zweier gekrümmter Spanten eines Luft- oder Raumfahrzeugs Connecting arrangement for connecting two curved ribs of an aircraft or spacecraft |
| 11/06/2008 | CA2684076A1 Composite structure comprising a stringer with a pad embedded in the recess of a panel and method of transmitting forces |
| 11/06/2008 | CA2680369A1 Fibre metal laminate panel |
| 11/05/2008 | EP1988014A2 Ducted fan air vehicle with deployable wings |
| 11/05/2008 | EP1988013A2 Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft |
| 11/05/2008 | EP1988012A2 Wing for an aircraft with a fiber composite load carrying structure |
| 11/04/2008 | US7445744 Process for forming a single piece co-cure composite wing |
| 10/30/2008 | US20080265103 Aerofoil |
| 10/30/2008 | US20080265094 Structural Element and Method of Manufacture |
| 10/30/2008 | US20080265088 Propulsion System for Model Airplane |
| 10/30/2008 | DE102007019716A1 Faser-Metall-Laminat-Panel Fibre metal laminate panel |
| 10/30/2008 | DE102007019692A1 Flügel-Rumpf-Sektion eines Flugzeugs Wing-fuselage section of an aircraft |
| 10/30/2008 | DE102007018188A1 Propellergetriebenes Fluggerät für die Durchführung von taktischen Aufgaben Propeller-driven aircraft for the implementation of tactical tasks |
| 10/30/2008 | CA2624214A1 Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft |
| 10/29/2008 | EP1984244A2 An airfoil for a helicoptor rotor blade |
| 10/29/2008 | EP1984241A1 Method for autoclave-free adhesive bonding of components for aircraft |
| 10/29/2008 | CN100429120C Aircraft with changeable wing shape |
| 10/29/2008 | CN100429119C Aircraft with wing sweepback angle change |
| 10/28/2008 | US7441724 System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft |
| 10/23/2008 | WO2008125868A2 Aircraft |
| 10/23/2008 | DE102006045633B4 Verfahren zum Anbinden eines Stringers an ein Strukturbauteil eines Luft- oder Raumfahrzeugs A method for attaching a stringer to a structural component of an aircraft or spacecraft |
| 10/22/2008 | CN100427358C Aircraft leading edge device systems and corresponding sizing methods |
| 10/16/2008 | WO2008124352A1 Methods and systems for composite structural truss |
| 10/16/2008 | WO2008124351A2 Methods and systems for composite structural truss |
| 10/09/2008 | WO2008121005A1 Aircraft component manufacture and assembly |
| 10/09/2008 | WO2008119664A2 Leading edge for aircraft made of reinforced composite material |