Patents for B64C 3 - Wings (5,458) |
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10/09/2008 | WO2008099097A3 Aircraft wing including a plurality of dismountable members |
10/09/2008 | US20080245928 Methods and systems for composite structural truss |
10/09/2008 | US20080245927 Methods and systems for composite structural truss |
10/09/2008 | CA2682289A1 Leading edge for aircraft made of reinforced composite material |
10/08/2008 | EP1976753A2 Flexible control surface for an aircraft |
10/07/2008 | CA2472247C Damping of vibrations |
10/02/2008 | US20080241621 Energy storage system |
10/02/2008 | US20080237404 Hydrogen powered aircraft |
10/02/2008 | US20080237403 Metal injection molding process for bimetallic applications and airfoil |
10/02/2008 | DE102007012167A1 Drillelastisches und biegesteifes Stabelement zum Lagern und Führen einer beweglichen Klappe gegenüber einem Flügel eines Luftfahrzeugs Drill elastic and resistant to bending rod member for supporting and guiding a movable flap over a wing of an aircraft |
10/01/2008 | EP1974071A1 Component for arrangement in the duct of a turbine engine and spray method for production of a coating |
09/30/2008 | US7429074 Airflow control devices based on active materials |
09/30/2008 | CA2372166C Aircraft wing and fuselage contours |
09/25/2008 | WO2007071384A8 Flexible control surface for an aircraft |
09/25/2008 | DE102004033068B4 Verkehrsflugzeug mit einem Hauptdeck und einem Unterdeck Airliner with a main deck and lower deck |
09/25/2008 | CA2665852A1 Highly efficient supersonic laminar flow wing |
09/24/2008 | EP1971520A2 Aircraft wing composed of composite and metal panels |
09/23/2008 | CA2444560C Method and apparatus for rotatably supporting movable components, including canards |
09/18/2008 | WO2008112686A1 Moveable wings on a flying/hovering vehicle |
09/18/2008 | US20080223992 High-Performance Low-Noise Aircraft Exhaust Systems and Methods |
09/18/2008 | US20080223987 Rib element and composite flange for aircraft |
09/18/2008 | US20080223986 Trussed Structure |
09/18/2008 | DE10340978B4 Kunstfaserelement für Rotorblätter Synthetic fiber element for rotor blades |
09/18/2008 | DE102007012984A1 Connecting unit for force transmission between flap drive and flap at e.g. airfoil wing, of e.g. fixed wing aircraft, has middle section arranged between two sections, where unit is designed as strap from fiber composite material |
09/18/2008 | CA2679491A1 Moveable wings on a flying/hovering vehicle |
09/17/2008 | EP1970303A2 Rib element and composite flange for aircraft |
09/17/2008 | EP1636086B1 Wing, especially a carrier wing of an aeroplane, having an adaptable profile |
09/17/2008 | CN101264795A Superaltitude low speed positioning flight pilotless aircraft |
09/12/2008 | WO2008084260A3 A leading edge structure for an aerofoil |
09/11/2008 | US20080217486 Small unmanned airborne vehicle airframe |
09/10/2008 | EP1967934A1 Thrust metering system |
09/10/2008 | EP1966839A1 Three-dimensional stacked piezoelement, and piezoelectric actuator having such a stacked piezoelement |
09/10/2008 | EP1819591B1 A trussed structure |
09/09/2008 | CA2413206C Hybrid fuel containment structure |
09/04/2008 | WO2008105806A2 Wing panel structure |
09/04/2008 | US20080210821 Rib support for wing panels |
09/03/2008 | EP1963186A1 Assembly of aircraft components |
09/03/2008 | EP1963178A1 A joint for use in aircraft construction |
09/03/2008 | EP1963095A1 Protection device |
08/28/2008 | WO2008103735A2 Aircraft, and retrofit components therefor |
08/28/2008 | US20080203236 CMC airfoil with thin trailing edge |
08/28/2008 | US20080203235 Apparatus for measuring a turbine blade |
08/28/2008 | US20080203228 Double-Shell Design Center Box |
08/28/2008 | US20080203222 Yaw Control System and Method |
08/28/2008 | US20080203219 Hydrogen powered aircraft |
08/28/2008 | DE102007009060A1 Spoiler für eine aerodynamisch wirksame Fläche eines Luftfahrzeugs Spoiler for an aerodynamically effective area of an aircraft |
08/27/2008 | EP1960152A1 Structural element and method of manufacture |
08/27/2008 | CN101249885A Rib support for wing panels |
08/26/2008 | US7416155 Canard position and dihedral for boom reduction and pitch/directional control |
08/21/2008 | WO2008100299A2 Mounting device for an aircraft |
08/21/2008 | WO2008100286A2 Apparatus and method for use on aircraft with spanwise flow inhibitors |
08/21/2008 | DE102004019496B4 Tragflügel für Fluggeräte mit Triebwerken Hydrofoil for aircraft with engines |
08/21/2008 | CA2676334A1 Aircraft wing including a plurality of dismountable members |
08/20/2008 | EP1957216A1 Method of superplastic forming of titanium assemblies and aircraft structure manufactured thereby |
08/14/2008 | WO2008097325A2 Airfoil having a movable control surface |
08/14/2008 | US20080191100 System for controlling flight direction |
08/13/2008 | EP1514797A4 Closed wing |
08/13/2008 | CN101242993A Double-shell design centre box |
08/13/2008 | CN101242992A Support structure for a wing |
08/13/2008 | CN101242991A Framework wing box for a wing |
08/12/2008 | US7410133 Miniature trailing edge effector for aerodynamic control |
08/12/2008 | US7410124 Lightweight air vehicle and pneumatic launcher |
08/07/2008 | US20080187809 Energy storage system |
08/06/2008 | EP1951567A2 Roof and floor flows |
08/06/2008 | CN100408428C Slotted aircraft wing |
07/31/2008 | US20080179465 Aircraft With Low Noise, Such as During Take-Off and Landing |
07/31/2008 | DE102007038634B3 Impulse-absorbent structure-component for aircraft, has open structure located behind impulse-absorbent layer extending toward propagation of catch bag such that catch bag is formed without reciprocal action with structure-component |
07/29/2008 | CA2328573C Composite junction for the assembly of at least one external device on a sandwich panel and panel incorporating at least one such junction |
07/24/2008 | WO2008087861A1 Leading edge structure of aircraft |
07/24/2008 | WO2008054876A3 Reinforced hybrid structures and methods thereof |
07/23/2008 | CN101228067A Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
07/23/2008 | CN101224788A Airplane multi-airfoils longitudinally aligned stepped distribution structure |
07/22/2008 | CA2358115C Electrostatic/pneumatic actuators for active surfaces |
07/17/2008 | WO2008084260A2 A leading edge structure for an aerofoil |
07/17/2008 | US20080169383 Support Structure For a Retractable and Extendable Flap, and Use of Said Structure |
07/17/2008 | CA2675127A1 A leading edge structure for an aerofoil |
07/15/2008 | US7398586 Methods and systems for manufacturing a family of aircraft wings and other composite structures |
07/10/2008 | WO2008067460A3 Composite shear tie |
07/10/2008 | US20080166613 Energy storage system |
07/10/2008 | US20080166603 Energy storage system |
07/09/2008 | EP1942053A2 Low-drag swept wings |
07/09/2008 | EP1942052A1 Rib support for wing panels |
07/09/2008 | CN101214853A Connecting structure for middle and outside wings of unmanned aerial vehicle |
07/09/2008 | CN100400375C Aerofoil with blunt tail edge |
07/03/2008 | US20080156941 Methods and apparatus for aircraft structural length of service enhancement |
07/03/2008 | US20080156936 Aircraft Wing |
07/02/2008 | EP1470463B1 Damping of vibrations |
07/02/2008 | CN100398397C Protective skin for aircraft |
06/28/2008 | CA2572448A1 Avio-car-ptfv |
06/26/2008 | US20080149779 Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles |
06/26/2008 | US20080149761 Main wing structure of aircraft |
06/26/2008 | US20080149758 Modular unmanned air-vehicle |
06/25/2008 | EP1934090A1 Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
06/19/2008 | WO2008070944A2 Flight control system |
06/19/2008 | US20080142641 Airplane configuration |
06/19/2008 | DE102006059112A1 Wing for manned aircraft has at least some of its ribs joined to cover at their end regions so wing can be assembled and dismantled by sliding cover along longitudinal axis of wing spar |
06/17/2008 | US7387277 Aircraft wing composed of composite and metal panels |
06/17/2008 | CA2270501C Method of reducing wind gust loads acting on an aircraft |
06/12/2008 | WO2008068523A1 Composite structure |
06/12/2008 | WO2008068472A1 Aerofoil member |