Patents for B64C 3 - Wings (5,458)
08/2012
08/07/2012US8235329 Dynamically actuated adaptive control structures
08/02/2012WO2012101439A1 Stringer, aircraft wing panel assembly, and method of forming thereof
08/02/2012WO2012075990A3 Flexible wing profile
08/02/2012WO2012001205A3 Aircraft component comprising panels stiffened with stringers having two types of local flarings
08/02/2012US20120193473 Torsion box skin stiffened with non parallel stringers
08/02/2012DE102007021076B4 Interkostal für ein Luft- oder Raumfahrzeug Intercostal for an aircraft or spacecraft
08/01/2012EP2481667A1 Stiffened structure including an opening
08/01/2012EP1988012B1 Wing for an aircraft with a fiber composite load carrying structure
08/01/2012EP1713689B1 Methods and apparatuses for launching unmanned aircraft, including releasably gripping aircraft during launch and braking subsequent grip motion
08/01/2012CN202358297U Wall plate of airplane wing
08/01/2012CN102616371A Method and device for enforcing canard spanwise piston type jet indirect vortex control technology
08/01/2012CN102616367A Method for trimming fixed-wing airplane with high lift-drag ratio
08/01/2012CN102616366A Connection of stiffening frames between an aircraft fuselage and a wing box
08/01/2012CN102616096A Solar flying automobile with folding wings
07/2012
07/31/2012US8231084 Aircraft wing
07/26/2012US20120187254 Aircraft slat assembly with anti-icing system
07/26/2012US20120187253 Leading edge device for an aircraft
07/26/2012US20120187251 Multiple Controllable Airflow Modification Devices
07/26/2012US20120187246 Vent stringer and aircraft main wing
07/25/2012EP2479109A1 Vent stringer and aircraft main wing
07/25/2012EP2479106A2 Leading edge device for an aircraft
07/25/2012EP2479100A2 Propulsion device using fluid flow
07/25/2012EP2477890A1 Removable horizontal stabilizer for helicopter
07/25/2012CN202345909U Wing assembled with variant winglet
07/25/2012CN202345908U Wing with movable wing surface
07/25/2012CN102602529A Folding full-motion horizontal tail mechanism
07/24/2012US8226048 Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods
07/24/2012US8225731 Marine thrust wings
07/24/2012CA2489783C Rivet assembly apparatus and process for assembling panels, specifically aircraft fuselage, using the apparatus
07/21/2012CA2762748A1 Vent stringer and aircraft main wing
07/18/2012EP2475575A2 Elevon control system
07/18/2012CN102582824A Cruise vehicle with variable wings
07/18/2012CN102582823A Airfoil capable of realizing deformation in wingspan direction or chord length direction
07/18/2012CN102582822A Wing for realizing wing span direction and chord length direction deformation
07/17/2012US8220755 Hinge rib
07/17/2012US8220743 Aircraft wing assembly
07/17/2012US8220737 VTOL aerial vehicle
07/12/2012WO2011064456A9 Flying apparatus
07/11/2012EP2300314B1 Apparatus and method for forming a ramped stiffener
07/11/2012CN202320781U 山区输电线路巡检无人飞机 Mountainous transmission line inspection unmanned aircraft
07/11/2012CN202320774U 未来救援隐身航母所载短体飞机 Short-body aircraft coming out of stealth aircraft rescue
07/11/2012CN202320773U 一种抗鸟撞飞机尾翼 An anti-bird strike aircraft tail
07/11/2012CN202320772U 一种双通道大型客机的高升力装置 A dual-channel high-lift devices large aircraft
07/11/2012CN102574575A Elevon control system
07/11/2012CN102574570A Removable horizontal stabilizer for helicopter
07/11/2012CN102556342A Wing combination
07/11/2012CN102556337A Bevel gear guiding type wing unfolding mechanism
07/11/2012CN102556336A Wing fast unfolding device for folding-wing unmanned plane
07/11/2012CN102556335A Flying-wing layout aircraft provided with cycloidal propellers
07/11/2012CN102556331A Method and device for high-efficiency indirect vortex control technology of canard configuration airplane
07/10/2012US8215590 Aerofoil with leading edge projection
07/05/2012WO2012091695A1 Multi-directional load joint system
07/05/2012US20120168567 Electrical power transfer assembly
07/05/2012CA2820004A1 Multi-directional load joint system
07/04/2012EP2470422A1 Adaptive structural core for morphing panel structures
07/04/2012CN202295282U 一种固定翼无人机机翼翼尖防擦装置 UAV wing tip device Airplanes scuff
07/04/2012CN102530239A Double torsional spring folding-type maneuverable empennage mechanism
07/04/2012CN102530238A Unmanned aerial vehicle with variable sweepbacks and spans of wings
07/04/2012CN102530237A Aircraft having variable geometry
07/04/2012CN102530236A Central body of tailless blended wing body aircraft
07/04/2012CN102530235A Method and apparatus for reducing aircraft noise
07/03/2012US8210473 Folding wing root mechanism
07/03/2012US8210467 Method and apparatus for hurricane surveillance from the eye
07/03/2012CA2661123C Panel assembly and method of erecting a panel assembly
06/2012
06/28/2012US20120160968 Mid-Wing Airplane
06/28/2012DE102007021075B4 Verbindungsanordnung zum Verbinden zweier gekrümmter Spanten eines Luft- oder Raumfahrzeugs Connecting arrangement for connecting two curved ribs of an aircraft or spacecraft
06/27/2012EP2467270A2 Convertible vehicle for road, air, and water usage
06/27/2012CN102514709A Aircraft wing box using grid structure and design method
06/27/2012CN102514708A Integral central wing box made of composite materials
06/26/2012US8205840 Elongated, torsion-deformable aerodynamic element
06/26/2012US8205834 Support structure for a wing
06/26/2012US8205824 Aircraft fuselage structure
06/21/2012WO2012082252A1 Skew-angle radius filler to reduce the risk of delamination of a laminated stringer assembly
06/21/2012WO2012081700A1 Structure manufacturing method and structure manufacturing apparatus
06/21/2012WO2012042246A3 Stiffener run-out
06/21/2012US20120156038 Propulsion device using fluid flow
06/21/2012US20120156037 Foil, utilized such as an airfoil or hydrofoil, characterized by a duct moving relative to a mass of fluid. A constriction within the duct increases the speed of the fluid flowing within the duct and thereby produces a pressure drop inducing a mass of fluid external to the duct to accelerate into the duct. The acceleration of the fluid into the duct generates a resultant force, which can be varied and controlled to improve performance and reduce drag
06/21/2012US20120153085 Adjustment of wings for variable camber for optimum take-off and landing
06/20/2012EP2466288A2 Method of designing natural laminar flow wing for reynolds numbers equivalent to actual supersonic aircraft
06/20/2012CN202279235U 变体鸭式无尾气动布局 Variants canard tailless aerodynamic layout
06/20/2012CN202279230U 一种用于飞机增升的导流栅板 Deflector grid for an aircraft's lift
06/20/2012CN102501973A Small-sized multipurpose unmanned machine
06/20/2012CN102501965A Section for upper edge strip of wing rib of aircraft outer wing
06/20/2012CN101107161B An aircraft wing
06/19/2012US8201773 Flexible self-erecting substructures for sensor networks
06/19/2012CA2659448C Wing panel structure
06/17/2012CA2764340A1 Optimization of structures subjected to hot gas streams
06/15/2012CA2759478A1 Airfoil manufacturing system
06/14/2012WO2012077857A1 Airplane equipped with a wing booster
06/14/2012WO2012075990A2 Flexible wing profile
06/14/2012WO2012018382A3 Flying vehicle retractable wing hinge and truss
06/14/2012US20120145826 High-lift-device, wing, and noise reduction device for high-lift-device
06/13/2012CN202272168U 电子控制短距起降自动安装角可调机翼结构 Electronically controlled automatic installation angle adjustable STOL wing structure
06/13/2012CN102498037A 可重新配置的飞行器 Reconfigurable aircraft
06/13/2012CN101557979B Wing panel structure
06/13/2012CN101466595B Composite wing-body joint
06/12/2012US8197974 Energy storage system
06/07/2012WO2012012752A9 Roadable aircraft and related systems
06/07/2012WO2011154582A3 Procedure for the manufacture of large parts of composite material controlling the thickness of the edges thereof
06/07/2012US20120138751 Aircraft having a vertical lift system
1 ... 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 ... 55