| Patents for B64C 3 - Wings (5,458) |
|---|
| 05/31/2006 | EP1268272A4 K-spar configuration for bonded wing construction |
| 05/31/2006 | EP0888201B1 Determinant spar assembly |
| 05/30/2006 | US7052573 Method to eliminate undulations in a composite panel |
| 05/30/2006 | US7051982 Fairing arrangements for aircraft |
| 05/30/2006 | US7051974 Pivoting aircraft wing and associated method |
| 05/30/2006 | US7051973 Airborne enhancement device |
| 05/25/2006 | US20060108479 Winged spacecraft |
| 05/25/2006 | US20060108474 Hollow assembly structure and fabrication method therefor |
| 05/24/2006 | EP1659359A1 Ammunition or ammunition part comprising a structural element made of energetic material |
| 05/24/2006 | EP1658221A1 Rigid wing with variable sustentation due to deployment of a flexible wing |
| 05/24/2006 | EP1658220A1 Protective skin for aircraft |
| 05/24/2006 | DE202006002764U1 Aircraft part e.g. fore flap and airfoil wing for protection of aircraft has gap between them and are connected to body of aircraft whereby gap between fore flap and airfoil wing has air-braking element |
| 05/23/2006 | US7048235 Slotted aircraft wing |
| 05/23/2006 | US7048234 Adaptive flap and slat drive system for aircraft |
| 05/23/2006 | US7048228 Slotted aircraft wing |
| 05/18/2006 | US20060102803 Leading edge flap apparatuses and associated methods |
| 05/18/2006 | US20060102802 Aircraft with forward opening inlay spoilers for yaw control |
| 05/18/2006 | US20060102778 Drive section of a lift truck |
| 05/11/2006 | WO2004076769A3 Contact stiffeners for structural skins |
| 05/09/2006 | US7040210 Apparatus and method for restraining and releasing a control surface |
| 05/09/2006 | CA2523630A1 Heat transferring cooling features for an airfoil |
| 05/04/2006 | US20060091263 Lifting foil |
| 05/04/2006 | DE102004051980A1 Structure, especially for aircraft, has deformability of outer shell limited to deformability of selected global portions of deformation acting on whole structure |
| 05/03/2006 | EP1425215B1 Composite material structure |
| 05/03/2006 | CN1767977A Winged spacecraft |
| 04/27/2006 | WO2006043978A2 Amphibian delta wing jet aircraft |
| 04/20/2006 | DE202006002433U1 Airbrake for wings of aeroplane, has edge with projection which runs in zigzag line or in similar line in which there is no straight line or bend, where point of zigzag line or similar line is truncated by straight line or bend |
| 04/20/2006 | DE202005020011U1 Three dimensional wing design for tailless airplane, has wing with leading edge that is swept between specific degrees, trailing edge proceeding through defined lapse of wing profile depth, where root of wing is formed of belly profiles |
| 04/20/2006 | DE19952976B4 Angetriebenes Scharnier mit automatischer, antriebsbetätigter Sperrvorrichtung Powered hinge with automatic, drive-operated locking device |
| 04/20/2006 | DE10156733B4 Aerodynamisches Profil mit verstellbarer Klappe An airfoil with adjustable flap |
| 04/19/2006 | EP1487696B1 Wing skin and method of manufacture thereof |
| 04/19/2006 | EP1213127B1 Method for producing stiffened hollow structure composed of fiber-reinforced composite |
| 04/19/2006 | CN2772961Y Fluid jet wing |
| 04/18/2006 | US7028954 Microfabricated translational stages for control of aerodynamic loading |
| 04/18/2006 | US7028948 Apparatus for increase of aircraft lift and maneuverability |
| 04/13/2006 | DE4417889B4 Flugzeugkörper sowie Verfahren zu dessen Herstellung Airplane body, as well as method for its preparation |
| 04/13/2006 | DE102004049504A1 Wing for aircraft has a rear auxiliary lift flap coupled to main wing and able to lie against main wing in retracted position and form air gap with it when extended |
| 04/12/2006 | EP1645506A2 Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect |
| 04/12/2006 | EP1511671A4 Control of an aircraft as a thrust-vectored pendulum in vertical, horizontal and all flight transitional modes thereof |
| 04/11/2006 | CA2217340C Slotted cruise trailing edge flap |
| 04/06/2006 | WO2006036183A1 Air-launchable aircraft and method of use |
| 04/06/2006 | DE4141166B3 Mechanische Verbindungsvorrichtung zwischen einem keramischen Material und einem Metall, insbesondere zur Verwirklichung einer Steuerflächen-Angriffskante Mechanical connection means between a ceramic material and a metal, in particular for realizing a control surface leading edge |
| 04/05/2006 | EP1551708B1 Vertical take-off and landing aircraft |
| 04/04/2006 | CA2520614A1 Reversible camber airfoil |
| 03/30/2006 | US20060065776 System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft |
| 03/30/2006 | DE102004045651A1 Variable-geometry wing section has transverse sectors with a combination of fixed and flexible outer skin surfaces |
| 03/29/2006 | EP1638841A2 Airborne enhancement device |
| 03/23/2006 | WO2006030213A1 Wing tip devices |
| 03/23/2006 | US20060060719 An aeronautical high-lift system with an overload safety device |
| 03/23/2006 | CA2577602A1 Wing tip devices |
| 03/22/2006 | EP1637450A2 Wing, in particular aircraft wing, with variable profile |
| 03/22/2006 | EP1636086A1 Wing, especially a carrier wing of an aeroplane, having an adaptable profile |
| 03/21/2006 | US7014143 Aircraft lightning strike protection and grounding technique |
| 03/21/2006 | US7014142 Low-drag rotor/wing flap |
| 03/09/2006 | US20060051592 First and second polymeric films covering aluminum foil include nylon, poly ether ether ketone (PEEK), polysulfonate, polyesters polyimide, polyolefins, polyurethane, halopolymers; protective coatings for aircraft skin; protection against lightning strikes and/or mitigation of P-static charging |
| 03/09/2006 | US20060049307 Flow-mechanically effective surface for minimizing induced resistance |
| 03/09/2006 | DE102004040313A1 Wing span load distribution setting system for aircraft, has inner and outer flaps displaceable relative to wing span direction, which are not mechanically connected to each other |
| 03/02/2006 | DE102005039649A1 Flugzeugflügel Aircraft wing |
| 03/02/2006 | DE102004039770A1 Flügelanordnung Wing assembly |
| 03/01/2006 | EP1332547B1 Electrostatic/pneumatic actuators for active surfaces |
| 02/28/2006 | US7004428 Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings |
| 02/23/2006 | WO2006019332A1 Aircraft lifting surface (variants) |
| 02/23/2006 | US20060038088 Aircraft wing |
| 02/23/2006 | US20060038086 System for setting the span load distribution of a wing |
| 02/23/2006 | CA2515276A1 Aircraft wing |
| 02/22/2006 | EP1628112A1 Wing arrangement |
| 02/21/2006 | US7001652 Composite fiber-resin tube with diametral fiber truss and method of manufacture |
| 02/21/2006 | US7000870 Laminar flow wing for transonic cruise |
| 02/19/2006 | CA2516283A1 System for setting the span load distribution of a wing |
| 02/16/2006 | WO2005110842A3 Airfoil box and associated method |
| 02/16/2006 | WO2005084156A3 Hydrogen powered aircraft |
| 02/16/2006 | US20060032982 Method of joining structural elements in an aircraft |
| 02/09/2006 | DE102004033068A1 Verkehrsflugzeug mit einem Hauptdeck und einem Unterdeck Airliner with a main deck and lower deck |
| 02/08/2006 | EP1624200A1 A device and a method for releasably holding two articles together |
| 02/07/2006 | CA2355366C Forming reinforcing components |
| 02/02/2006 | WO2006010817A1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 02/02/2006 | US20060022093 Flap interconnection system for aircraft |
| 02/02/2006 | US20060022085 Device and method of control of fixed and variable geometry rhomboid wings |
| 02/02/2006 | CA2570618A1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 02/01/2006 | EP1620310A1 Aircraft comprising a lift-generating fuselage |
| 01/31/2006 | US6991280 Airflow control devices based on active materials |
| 01/26/2006 | WO2005091873A3 Portable fume exhauster-carpet and floor drayer |
| 01/26/2006 | WO2005039972A3 Ducted fan vtol vehicles |
| 01/26/2006 | US20060016927 Method and apparatus for rotatably supporting movable components, including canards |
| 01/25/2006 | EP1619116A1 Fish-plating device between composite and metallic structural members |
| 01/22/2006 | CA2511847A1 Fish-jointed unit for composite structure elements with metal structure elements |
| 01/18/2006 | EP1616061A2 Contact stiffeners for structural skins |
| 01/17/2006 | US6986481 Extendable joined wing system for a fluid-born body |
| 01/17/2006 | CA2244747C Determinant spar assembly |
| 01/12/2006 | WO2006004416A1 Hybrid aircraft |
| 01/12/2006 | DE102004029485A1 Impuls-absorbierendes Struktur-Bauteil Impulse-absorbing structural component |
| 01/12/2006 | CA2572929A1 Hybrid aircraft |
| 01/11/2006 | EP1614531A2 Titanium-polymer hybrid laminates |
| 01/11/2006 | EP1169224B1 Aircraft wing and fuselage contours |
| 01/11/2006 | CN1720167A Slotted aircraft wing |
| 01/10/2006 | CA2290028C Spoiler for wings |
| 01/05/2006 | WO2006001859A1 Structural panels for use in aircraft fuselages and other structures |
| 01/05/2006 | WO2005081701A3 Blade and wing configuration |
| 01/05/2006 | US20060000952 Aircraft leading edge apparatuses and corresponding methods |
| 01/05/2006 | US20060000943 Horizontal augmented thrust system and method for creating augmented thrust |