| Patents for B64C 3 - Wings (5,458) |
|---|
| 08/16/2001 | WO2001058758A2 Remotely piloted aircraft |
| 08/16/2001 | WO2001058757A2 Communications system using high altitude, long endurance aircraft as relays |
| 08/16/2001 | WO2001058756A2 Aircraft |
| 08/16/2001 | WO2001058753A1 Assembling composite structures |
| 08/16/2001 | US20010013173 Method of fabricating leading edge nose structures of aerodynamic surfaces |
| 08/16/2001 | DE10005348A1 Aerodynamic surface edge structure manufacturing method uses screw movement between left and right mold parts for applying pressure to parallel metal stringers at rear of sheet metal outer skin |
| 08/16/2001 | CA2400048A1 Aircraft |
| 08/16/2001 | CA2400041A1 Aircraft |
| 08/16/2001 | CA2400022A1 Aircraft |
| 08/14/2001 | US6273367 Cover-skin structure |
| 08/07/2001 | US6269527 Wing panel assembly |
| 07/24/2001 | US6264136 High efficiency combination wing aircraft |
| 07/19/2001 | DE10001700A1 Variable-geometry aerodynamic component, with passive bending element between structures and active element |
| 07/17/2001 | US6260800 Aircraft power plant with two air intake fans |
| 07/17/2001 | US6260799 Aircraft wing fold actuation system |
| 07/17/2001 | US6260798 High-G compact folding wing |
| 07/17/2001 | US6260795 Oya computerized glider |
| 07/11/2001 | EP1114772A1 VTOL aircraft with variable wing sweep |
| 07/04/2001 | EP1112927A1 Aircraft lift arrangement |
| 07/04/2001 | EP1112176A1 Composite material construction |
| 06/19/2001 | US6247670 Active flaperon assembly |
| 06/13/2001 | EP1105281A1 A method of constructing skin for a member of a body such as an aircraft |
| 06/13/2001 | DE19957016A1 Combined flap profile for glider or micro-light aircraft has pivoted curvature flap at rear part of Fowler flap |
| 06/12/2001 | US6244542 Rotor driven edge |
| 06/06/2001 | EP1104741A1 Aircraft lift arrangement |
| 06/05/2001 | US6241195 Extendable/retractable airfoil assembly for fixed wing aircraft |
| 05/29/2001 | US6237873 Composite material wing structure |
| 05/22/2001 | US6234423 Composite airfoil structures and their forming methods |
| 05/22/2001 | CA1341239C Pale a faible signature radar |
| 05/17/2001 | WO2001034465A1 Device for guiding a gas flow |
| 05/17/2001 | WO2001034381A1 Reinforcement of a laminated member for an aircraft |
| 05/16/2001 | EP1099626A1 Aft egress and control device for an aircraft |
| 05/09/2001 | EP0973676A4 Extendable/retractable airfoil assembly for fixed wing aircraft |
| 05/08/2001 | US6227498 Single surface independent aircraft control |
| 05/03/2001 | WO2001030653A1 Reusable booster for the first stage of a launcher |
| 05/01/2001 | US6224012 Roadable aircraft combined vehicle for practical use |
| 04/19/2001 | WO2001026964A1 Heat shield |
| 04/11/2001 | EP1090835A1 Surface actuator for deforming an elastic plate structure |
| 04/10/2001 | US6215221 Electrostatic/pneumatic actuators for active surfaces |
| 04/10/2001 | US6213433 Leading edge for an aircraft |
| 04/04/2001 | CN1289705A Flying method and equipment |
| 04/04/2001 | CN1064016C Weak ground effect flying vehicle |
| 04/03/2001 | US6211497 Induction consolidation system |
| 03/22/2001 | WO2001019673A1 Improvements to convertible aircraft with tilting rotors |
| 03/22/2001 | WO2001019671A1 Weight-shift-controlled airplane |
| 03/22/2001 | CA2382879A1 Improvements to convertible aircraft with tilting rotors |
| 03/20/2001 | US6202304 Method of making a perforated metal sheet |
| 03/20/2001 | CA2108047C Shell structural component made of fiber composite material |
| 03/13/2001 | US6199796 Adaptive pneumatic wing for fixed wing aircraft |
| 02/20/2001 | US6190484 Monolithic composite wing manufacturing process |
| 02/15/2001 | DE19936721A1 Support wing profile for commercial aircraft; has profiled edge with skin parts and perpendicular ribs having planar elements connected between skin parts by rotating joints |
| 02/13/2001 | US6186443 Airborne vehicle having deployable wing and control surface |
| 02/07/2001 | EP1074466A1 Method of fabricating a composite material wing |
| 02/06/2001 | US6182929 Load carrying structure having variable flexibility |
| 01/31/2001 | EP1071607A2 Single surface multi axis aircraft control |
| 01/30/2001 | US6179248 Aircraft |
| 01/30/2001 | US6178991 Safety container for potentially explosive and/or environmentally hazardous substances |
| 01/24/2001 | EP1070661A2 Wing of composite material and method of fabricating the same |
| 01/18/2001 | WO2001004002A1 Aircraft aerofoil unit |
| 01/16/2001 | US6173925 Skin-rib structure |
| 01/16/2001 | US6173924 Low density flexible edge transition |
| 01/10/2001 | EP1066914A1 Method for assembling a flexible panel on an open structure and installation for carrying out the method |
| 01/09/2001 | US6170157 Determinant spar assembly |
| 01/04/2001 | WO2001000488A1 Laminar flow control system and suction panel for use therewith |
| 01/04/2001 | CA2370647A1 Laminar flow control system and suction panel for use therewith |
| 01/02/2001 | US6168384 Propeller blade configuration |
| 12/28/2000 | DE3428015C1 Überkritisches Tragflächenprofil Supercritical airfoil |
| 12/27/2000 | EP1062154A1 Assembly robot for wing |
| 12/26/2000 | US6164919 Propeller and impeller blade configuration |
| 12/26/2000 | US6164599 Aerofoil profile with variable profile adaptation |
| 12/26/2000 | US6164598 Adaptive control surface apparatus |
| 12/26/2000 | US6164596 Designs of and methodology for inward or outward, and partially inward or outward turning flow hypersonic air-breathing and rocket-based-combined-cycle vehicles |
| 12/26/2000 | US6164591 Ground-effect flying boats also applicable to aircraft, drones, and spacecraft |
| 12/20/2000 | EP1060984A2 Automatic leading edge flap |
| 12/19/2000 | US6161802 Trapped vortex airfoil nose |
| 12/19/2000 | US6161797 Method and apparatus for reducing airplane noise |
| 12/13/2000 | CN1276319A Wing-varying aircraft |
| 12/12/2000 | CA2123393C Structure having an aerodynamic surface for an aircraft |
| 12/06/2000 | EP0983188B1 Adaptive pneumatic wings for flying devices with fixed wings |
| 11/28/2000 | US6152405 Lift body having a variable camber |
| 11/23/2000 | WO2000055035B1 Aircraft wing and fuselage contours |
| 11/22/2000 | EP1053175A1 Double-walled panel |
| 11/21/2000 | US6149101 Aircraft wing and fuselage contours |
| 11/16/2000 | DE19916411A1 Dynamischer Hebel zur Verbesserung der Kraftübertragung Dynamic lever for improving power transmission |
| 11/14/2000 | US6145791 Elastomeric transition for aircraft control surface |
| 11/09/2000 | WO2000066427A1 Aeroplane wings |
| 11/02/2000 | EP1047593A1 System for varying a surface contour |
| 11/02/2000 | DE19919626A1 Aircraft with combined aerofoils and control surfaces has annulus on each side of fuselage and formed by aerofoils and control surfaces together with side walls of fuselage, and annulus accommodates propeller |
| 10/31/2000 | US6139268 Turbine blade having an extensible tail |
| 10/31/2000 | US6138957 Swept-back wings with airflow channeling |
| 10/31/2000 | US6138956 Aerofoil profile with variable profile adaptation |
| 10/26/2000 | WO2000063071A1 Aerodynamic surface of an aircraft with a leak baffle |
| 10/12/2000 | DE19916145A1 Bearing wing for increasing lift and stabilizing flight ratio, consisting of thin-walled flow channels joined to each other and open at bottom |
| 10/11/2000 | EP1043223A2 Enhanced aerodynamic profile |
| 10/10/2000 | US6129308 Delta-shaped aircraft with variable camber fuselage and wing |
| 10/04/2000 | EP1040999A2 Load carrying element with flexible outer skin |
| 09/28/2000 | WO2000056602A1 Modular air intake duct for aircraft |
| 09/28/2000 | WO2000056599A1 Aeroelastically stable forward swept wing |
| 09/28/2000 | DE19947633A1 W-shaped main lift wing for aircraft, with different setting angles of surface sections |
| 09/26/2000 | US6123297 Segmented flap with variable camber for aircraft wing |