| Patents for B64C 3 - Wings (5,458) |
|---|
| 03/06/2007 | US7185847 Winged vehicle with variable-sweep cantilevered wing mounted on a translating wing-support body |
| 03/01/2007 | WO2005099380A3 Lift augmentation system |
| 03/01/2007 | US20070045477 Aircraft wing slat |
| 03/01/2007 | DE102005038851A1 Wing box for aircraft wing, has framework connected to at least one exterior shell such that load acting on exterior shell is transferred by framework |
| 02/28/2007 | EP1755945A2 Lift augmentation system |
| 02/27/2007 | US7182297 Method and apparatus for supporting aircraft components, including actuators |
| 02/27/2007 | US7182293 Airfoil box and associated method |
| 02/22/2007 | WO2007022315A2 Integrated pulse detonation engine in a lifting surface with supercirculation |
| 02/22/2007 | WO2007020094A1 Framework wing box for a wing |
| 02/22/2007 | WO2007020069A1 Support structure for a wing |
| 02/22/2007 | WO2007019896A1 Double-shell design centre box |
| 02/22/2007 | WO2006135421A3 Leading edge flap apparatuses and associated methods |
| 02/22/2007 | WO2006043978A3 Amphibian delta wing jet aircraft |
| 02/22/2007 | DE102005038857A1 Center case for airplane wing, has side surfaces planking case at sides, where one surface comprises shells that are arranged spatially to each other by distance and connected with one another by U-profiles in longitudinal direction of case |
| 02/22/2007 | DE102005038849A1 Aerofoil supporting structure for use in airplane, has bar unit with connection mechanism which is formed, such that power is centrally transferred between bar unit and node unit, when mechanism is in contact with node unit |
| 02/22/2007 | CA2616929A1 Support structure for a wing |
| 02/22/2007 | CA2614878A1 Framework wing box for a wing |
| 02/21/2007 | EP1216816B1 Composite material stiffened panel and manufacturing method thereof |
| 02/21/2007 | CN1918033A Landing flap guide for aircraft |
| 02/15/2007 | WO2007018785A1 Integrated wingtip extensions for jet transport aircraft and other types of aircraft |
| 02/15/2007 | WO2007018772A2 Rotor blade assembly with high pitching moment airfoil section for a rotary wing aircraft |
| 02/15/2007 | US20070034749 Deployable airfoil assembly for aircraft |
| 02/15/2007 | US20070034748 Aerospace vehicle flow body systems and associated methods |
| 02/15/2007 | US20070034747 Translating conduit apparatus for an airplane or equipment |
| 02/14/2007 | EP1751434A1 Fastener networks |
| 02/14/2007 | EP1750998A2 Unitized rotary actuator hinge fitting |
| 02/14/2007 | EP1750929A1 Structural panels for use in aircraft fuselages and other structures |
| 02/13/2007 | US7175132 Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces |
| 02/08/2007 | WO2007015656A1 Aerodynamic noise reducing method (variants) and low-noise structural element for operating in a fluid medium flow |
| 02/08/2007 | US20070029443 Cover for an aircraft structure |
| 02/08/2007 | CA2617350A1 Aerodynamic noise reducing method (variants) and low-noise structural element for operating in a fluid medium flow |
| 02/06/2007 | US7172158 Ram air parachute canopy with trapezoidal cells |
| 02/01/2007 | US20070023573 Aircraft wing |
| 02/01/2007 | US20070023568 Unmanned aerial vehicle (UAV) deceleration system |
| 01/25/2007 | US20070020104 Rotor blade assembly with high pitching moment airfoil section for a rotary wing aircraft |
| 01/25/2007 | US20070018048 Winged structural joint and articles employing the joint |
| 01/25/2007 | US20070018033 Precision aerial delivery of payloads |
| 01/25/2007 | DE10128119B4 Verfahren zur Reduzierung der benötigten Energie für die Bewegung eines Objektes A method of reducing the energy required for the movement of an object |
| 01/24/2007 | EP1745914A2 Composite and method for making a composite |
| 01/23/2007 | US7165745 Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion |
| 01/18/2007 | US20070011970 Contact stiffeners for structural skins |
| 01/18/2007 | DE102006032453A1 Flow element e.g. for aerofoil, has range based variable profile thickness with element has outer skin which is adjustable transverse to profile line where profile thickness is changed |
| 01/10/2007 | EP1740455A2 Airfoil box and associated method |
| 01/03/2007 | EP1339601B1 Flap actuator system |
| 01/03/2007 | CN1890124A Airflow control devices based on active materials |
| 12/28/2006 | WO2006137869A2 System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft |
| 12/28/2006 | WO2006073750A3 Stowable design for unmanned aerial vehicle |
| 12/28/2006 | US20060289696 Electric flight control surface actuation system for aircraft flaps and slats |
| 12/28/2006 | DE102005027749A1 Auftriebserhöhende Klappe, insbesondere Nasenklappe, für einen aerodynamisch wirksamen Flügel High Lift flap, in particular nasal valve, for a aerodynamic wing |
| 12/28/2006 | DE10155119B4 Aktuator Actuator |
| 12/27/2006 | EP1735211A1 Fairing for an aircraft structure |
| 12/26/2006 | US7152827 Methods and apparatuses for launching, capturing, and storing unmanned aircraft, including a container having a guide structure for aircraft components |
| 12/21/2006 | WO2006133940A1 Lift-augmenting flap, in particular leading edge flap, for an aerodynamically effective wing |
| 12/21/2006 | US20060284022 Aerospace vehicle yaw generating systems and associated methods |
| 12/21/2006 | US20060284005 Bendable wing for micro air vehicle |
| 12/21/2006 | CA2610297A1 Lift-augmenting flap, in particular leading edge flap, for an aerodynamically effective wing |
| 12/21/2006 | CA2510333A1 Device for reinforcement of a hollow structure, especially a box structure for an aircraft and a hollow structure equipped with such a device |
| 12/20/2006 | EP1734333A1 Ammunition or ammunition component having the shape of a flying object such as a drone |
| 12/19/2006 | US7150435 Type aircraft |
| 12/19/2006 | CA2317845C Shaped metal panels and forming same by shot peening |
| 12/14/2006 | WO2006131532A1 Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft |
| 12/14/2006 | WO2006114493A3 Aircraft with low noise, such as during take-off and landing |
| 12/14/2006 | CA2607041A1 Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft |
| 12/12/2006 | US7147271 Airflow control devices with planar surfaces |
| 12/12/2006 | US7147269 Airflow control devices using current |
| 12/07/2006 | WO2005000671A3 Deployable, rigidizable wing |
| 11/30/2006 | US20060267376 Airflow control devices based on active materials |
| 11/29/2006 | EP1047593B1 System for varying a surface contour |
| 11/21/2006 | US7137202 Assembling composite structures |
| 11/16/2006 | WO2006119732A1 Metal, integral structural component having improved residual strength |
| 11/16/2006 | US20060255205 Small remotely controllable aircraft |
| 11/16/2006 | DE102005021852A1 Vehicle, flying machine or apparatus has curvature of airfoil along profile and also pitch angle of airfoil simultaneously positively and negatively variable by control means |
| 11/14/2006 | US7134629 Structural panels for use in aircraft fuselages and other structures |
| 11/09/2006 | US20060249627 Reinforced cover for cut-outs in an aeordynamic contour |
| 11/08/2006 | CN2835081Y Aircraft wing structure |
| 11/02/2006 | WO2006114493A2 Aircraft with low noise, such as during take-off and landing |
| 11/02/2006 | US20060243864 Unitized rotary actuator hinge fitting |
| 11/02/2006 | CA2603824A1 Aircraft with low noise, such as during take-off and landing |
| 10/31/2006 | US7130725 Method for correcting control surface angle measurements in single viewpoint photogrammetry |
| 10/31/2006 | US7128532 Transpiration cooling system |
| 10/31/2006 | US7128294 Methods and apparatuses for launching unmanned aircraft, including methods and apparatuses for launching aircraft with a wedge action |
| 10/26/2006 | WO2006112823A1 Method to eliminate undulations in a composite panel |
| 10/26/2006 | US20060237596 Wing, particularly airfoil of an aircraft, having changeable profile |
| 10/26/2006 | US20060237595 Wing for an aircraft or spacecraft |
| 10/26/2006 | US20060237580 Canard position and dihedral for boom reduction and pitch/directional control |
| 10/26/2006 | DE102006018378A1 Flugzeugnassflügel Aircraft wet wing |
| 10/26/2006 | DE102005018428A1 Träger in Schalenbauweise, insbesondere Tragflügel eines Flugzeugs Carrier shell construction, in particular wing of an aircraft |
| 10/26/2006 | DE102005015337A1 Box girder for aerodynamic load-bearing structure of wings or tail units, has aerodynamic panels with semi-ribbed parts that are connected with each other at a position and are held at distance with respect to each other at another position |
| 10/25/2006 | EP1714866A1 Monocoque structure |
| 10/25/2006 | EP1713689A2 Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion |
| 10/25/2006 | EP1713688A1 Landing flap guide for aircraft |
| 10/24/2006 | US7126096 Resistance welding of thermoplastics in aerospace structure |
| 10/24/2006 | CA2242868C Determinant wing assembly |
| 10/19/2006 | WO2006076018A3 Unitized rotary actuator hinge fitting |
| 10/19/2006 | US20060234007 Device for the protection against and detection of impacts on the edges of a layered composite structure |
| 10/18/2006 | EP1711399A2 Ducted fan vtol vehicles |
| 10/18/2006 | EP0988225B1 Blunt-leading-edge raked wingtips |
| 10/17/2006 | US7121503 Better balanced canard airplane with forward engine |
| 10/12/2006 | WO2006105589A1 Seals and fasteners |
| 10/12/2006 | US20060226296 Pivoted flap mechanism for adjusting an aerodynamic pivoted flap associated with a wing |