| Patents for B64C 3 - Wings (5,458) |
|---|
| 07/26/2007 | WO2007082823A1 Component for arrangement in the duct of a turbine engine and spray method for production of a coating |
| 07/26/2007 | US20070170309 Flight device (aircraft) with a lift-generating fuselage |
| 07/19/2007 | WO2007020094A8 Framework wing box for a wing |
| 07/19/2007 | US20070164147 Aircraft internal wing and design |
| 07/18/2007 | EP1808508A1 Component located in the flow channel of a turbomachine and spraying process for generating a coating. |
| 07/17/2007 | US7243879 Lattice fin for missiles or other fluid-born bodies and method for producing same |
| 07/12/2007 | US20070158503 Fluid dynamic foil with Coanda energizer |
| 07/12/2007 | US20070158495 High lift and high strength aerofoil |
| 07/12/2007 | DE102005062919A1 Tragfläche für ein Flugzeug und Flugzeug Wing for an aircraft and aircraft |
| 07/11/2007 | EP1806285A1 Wing of composite material and method of fabricating the same |
| 07/11/2007 | CN1325683C Al-Cu-Mg-Si alloy and method for producing the same |
| 07/11/2007 | CN1325219C Method of repairing a crack in a component utilizing friction stir welding |
| 07/10/2007 | US7240878 High wing monoplane aerospace plane based fighter |
| 07/10/2007 | CA2522914C Determinant spar assembly |
| 07/10/2007 | CA2363405C Method and apparatus for localized digital radiographic inspection |
| 07/05/2007 | US20070152106 Wing, particularly airfoil of an aircraft, having changeable profile |
| 07/05/2007 | US20070152104 Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators |
| 07/05/2007 | US20070152098 Structural mechanism for unlocking and engaging a controllable surface on a hinged platform (wing) |
| 07/05/2007 | DE102005061752A1 Dreidimensionales Stapelpiezoelement und piezoelektrischer Aktuator mit einem solchen Stapelpiezoelement Three-dimensional stack of piezoelectric element and a piezoelectric actuator having a stack of such piezo element |
| 07/05/2007 | DE102005061750A1 Flexible Steuerfläche für ein Luftfahrzeug Flexible control surface for an aircraft |
| 07/03/2007 | US7237751 Helicopter rotor and method of repairing same |
| 06/28/2007 | WO2007071905A1 A joint for use in aircraft construction |
| 06/28/2007 | WO2007071398A1 Protection device |
| 06/28/2007 | WO2007071384A2 Flexible control surface for an aircraft |
| 06/28/2007 | WO2007071231A1 Three-dimensional stacked piezoelement, and piezoelectric actuator having such a stacked piezoelement |
| 06/28/2007 | CA2634519A1 Flexible control surface for an aircraft |
| 06/28/2007 | CA2633106A1 A joint for use in aircraft construction |
| 06/28/2007 | CA2629592A1 Protection device |
| 06/27/2007 | EP1799545A1 Air-launchable aircraft and method of use |
| 06/26/2007 | US7234668 Friction welding metal components |
| 06/21/2007 | WO2007068949A1 Assembly of aircraft components |
| 06/21/2007 | WO2007068943A1 Structural element and method of manufacture |
| 06/21/2007 | US20070138340 Protective skin for aircraft |
| 06/21/2007 | CA2631707A1 Assembly of aircraft components |
| 06/21/2007 | CA2628929A1 Structural element and method of manufacture |
| 06/14/2007 | DE102005059933A1 Fiber composite articles, especially tension or traction struts, comprise core with curved edges which surround inner peripheries of longitudinal bores whose outer edges are enclosed by peripheral flocked fiber composite strip |
| 06/12/2007 | US7229049 Unitized rotary actuator hinge fitting |
| 06/12/2007 | US7229046 Servo mounting system for direct drive of an aircraft control surface |
| 06/06/2007 | CN1977063A Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 06/06/2007 | CN1974323A Ground effect flyer |
| 06/05/2007 | US7226020 Apparatus for driving and adjusting flaps hinged to an aircraft |
| 05/31/2007 | US20070120007 Aerodynamic vehicle having a variable geometry, co-planar, joined wing |
| 05/31/2007 | DE102004029485B4 Impuls-absorbierendes Struktur-Bauteil Impulse-absorbing structural component |
| 05/30/2007 | EP1789316A1 Wing tip devices |
| 05/30/2007 | EP1268272B1 K-spar configuration for bonded wing construction |
| 05/29/2007 | US7222704 Damping of vibrations |
| 05/24/2007 | WO2007058906A1 Method of superplastic forming of titanium assemblies and aircraft structure manufactured thereby |
| 05/24/2007 | WO2007057638A1 Aircraft cooling duct |
| 05/24/2007 | DE102005054248A1 Braking flap for deceleration of aircraft against air-flow which surrounds aircraft, comprises many vortex edges, which resolve individual edge section into number of vortex part, are arranged at free edge |
| 05/24/2007 | CA2801975A1 Method of superplastic forming of titanium assemblies |
| 05/23/2007 | EP1788646A2 Planar sandwich type actuator and application for torsion of a structure |
| 05/23/2007 | EP1786667A1 Systems and methods for providing differential motion to wing high lift devices |
| 05/23/2007 | CN1317163C Wave-shaped straight wing |
| 05/22/2007 | CA2350136C A machine for laying up fabric to produce a laminate |
| 05/21/2007 | CA2568281A1 Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods |
| 05/16/2007 | EP1608555A4 Winged spacecraft |
| 05/16/2007 | CN2900356Y Blunt tail edge wing |
| 05/15/2007 | US7216835 Aircraft with extendable leading edge of fuselage and wings |
| 05/15/2007 | US7216830 Wing gull integration nacelle clearance, compact landing gear stowage, and sonic boom reduction |
| 05/10/2007 | WO2007019896A8 Double-shell design centre box |
| 05/10/2007 | US20070102589 Drive and Guide Arrangement for a Flap which is arranged on an Aircraft Mainplane |
| 05/10/2007 | US20070102587 Wing leading edge slat system |
| 05/10/2007 | US20070102586 Aircraft with rotatable leading edge of fuselage and wings |
| 05/10/2007 | US20070102578 Coordination hole apparatus and methods of use |
| 05/09/2007 | CN1960910A Air freight transport method, transport aeroplane and air freight transport system |
| 05/03/2007 | WO2007050073A1 A link between the wing and canard for flutter reduction |
| 05/03/2007 | DE102005052014A1 Conical bolt connection for connecting vertical tail to supporting structure of aircraft carcass cell, has bolt and/or sleeve with coating, where sleeve wedge surface has linear expansion that corresponds to expansion of bolt wedge surface |
| 05/02/2007 | EP1780120A2 Methods and systems for manufacturing a family of aircraft wings and other composite structures |
| 05/02/2007 | CN2895245Y Semiflexible-semirigid miniature aircraft |
| 04/24/2007 | US7207526 High efficiency tip vortex reversal and induced drag reduction |
| 04/24/2007 | US7207519 Blade restraint system |
| 04/18/2007 | EP1774183A1 Signal activated fastener array |
| 04/18/2007 | EP1773654A1 Hybrid aircraft |
| 04/18/2007 | CN1950617A Fastener networks |
| 04/12/2007 | US20070080262 Device for moving at least one moveable element in a gas turbine |
| 04/12/2007 | DE102005045759A1 Progressive aerofoil trailing edge for aircraft has flap, which can be adjusted both downward and upward by positive and by negative flap deflections respectively whereby aerofoil profile is closed on top side by sealing flap |
| 04/10/2007 | US7201700 Geared rotary actuators |
| 04/05/2007 | US20070075185 Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion |
| 04/04/2007 | CN1942363A Fairing for an aircraft structure |
| 04/03/2007 | US7198691 Fastenerless internal support for hollow structures |
| 04/03/2007 | US7198225 Aircraft control system |
| 03/29/2007 | WO2007015656B1 Aerodynamic noise reducing method (variants) and low-noise structural element for operating in a fluid medium flow |
| 03/29/2007 | US20070069084 Aircraft with extendable leading edge of fuselage and wings |
| 03/29/2007 | DE102005044549A1 Flugzeugflügel mit ausfahrbarer Nasenklappe Airplane wing with extendable nose flap |
| 03/29/2007 | DE102005031840A1 Drive-and guiding device for aircraft, has crank lever arranged, so that rotation direction of lever for driving of flap corresponds to direction of lever for flap, where rotation direction of lever for flap takes place anticlockwisely |
| 03/28/2007 | EP1767344A2 Wide area lightning diverter overlay |
| 03/28/2007 | EP1766102A1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 03/28/2007 | EP1658221B1 Rigid wing with variable sustentation due to deployment of a flexible wing |
| 03/27/2007 | US7195210 Fiber matrix for a geometric morphing wing |
| 03/27/2007 | US7195209 Aircraft high-lift system with overload protection |
| 03/27/2007 | US7195207 Winged spacecraft |
| 03/27/2007 | US7195203 Wing skin and method of manufacture thereof |
| 03/27/2007 | CA2454431C Aircraft structural components |
| 03/22/2007 | US20070063109 Rotary flap |
| 03/22/2007 | DE102006028885A1 Hybrid aircraft e.g. helicopter, has two wings arranged laterally at casing and engaging together with casing by rotating around axis using rotating mechanism, rotation symmetric and mirror symmetrical configuration |
| 03/21/2007 | EP1764307A1 Process for manufacturing a monolithic leading edge |
| 03/21/2007 | CN1934360A Signal activated fastener array |
| 03/15/2007 | US20070057123 Process for manufacturing a monolithic leading edge |
| 03/14/2007 | EP1762487A2 Improvements in and relating to aircraft wings and fuel tanks |
| 03/08/2007 | WO2006137869A3 System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft |