| Patents for B64C 3 - Wings (5,458) |
|---|
| 07/19/1994 | US5330092 Multiple density sandwich structures and method of fabrication |
| 06/29/1994 | EP0603352A1 Plastic-composite profiled girder, in particular a wing spar for aircraft and for wind-turbine rotors |
| 06/23/1994 | DE4243203A1 Support wing or tail-plane profile for glider |
| 06/21/1994 | US5322242 High efficiency, supersonic aircraft |
| 06/14/1994 | US5320491 Wind turbine rotor aileron |
| 06/14/1994 | US5320310 Articulated wing mechanism |
| 06/14/1994 | US5320306 Aircraft construction |
| 06/07/1994 | US5318249 Curled trailing edge airfoil |
| 06/01/1994 | EP0599788A1 Device for the continuous adjustment, in flight, of the inclination of the wing structure in an ultralight aircraft of the pendular type |
| 05/25/1994 | EP0373160B1 Divergent trailing-edge airfoil |
| 05/24/1994 | US5314142 Wing root aerofoil for forward swept wings |
| 05/17/1994 | US5312070 Segmented variable sweep wing aircraft |
| 05/10/1994 | US5310138 Wing fold actuator system for aircraft |
| 05/04/1994 | EP0594625A1 Supersonic aircraft shock wave energy recovery system. |
| 05/03/1994 | US5308228 Gas turbine blade comprising layers of composite material |
| 04/13/1994 | EP0591705A1 Composite shell construction |
| 02/22/1994 | US5288039 Spanwise graded twist panel |
| 02/17/1994 | WO1994003363A1 Spanwise gradient twist panel |
| 02/01/1994 | US5282591 Active vortex control for a high performance wing |
| 01/26/1994 | CN1081153A Weak ground effect flying vehicle |
| 01/25/1994 | US5280863 Lockable free wing aircraft |
| 01/20/1994 | WO1994001325A1 Wind turbine rotor aileron |
| 01/20/1994 | WO1994001277A1 Spliced laminate for aircraft fuselage |
| 01/20/1994 | WO1994001271A1 Plastic-composite profiled girder, in particular a wing spar for aircraft and for wind-turbine rotors |
| 01/20/1994 | CA2115350A1 Plastic-composite profiled girder, in particular a wing spar for aircraft and for wind-turbine rotors |
| 01/12/1994 | CN1080608A Method for raising wing elevating force |
| 01/06/1994 | WO1994000346A1 Aeroplane and method of its transforming into parking configuration |
| 01/05/1994 | EP0576806A1 Airplane and the way of its transforming to parking position |
| 01/04/1994 | US5275358 Wing/winglet configurations and methods for aircraft |
| 01/04/1994 | CA1325765C Composite leading edge/spar member for an aircraft control surface |
| 12/28/1993 | US5273238 Twin-hull seaplane |
| 12/14/1993 | US5269657 Aerodynamically-stable airfoil spar |
| 11/30/1993 | US5265830 Trailing edge splitter |
| 11/18/1993 | DE4215577A1 Aircraft or airship with improved stability in flight - has angled wings formed with wide downturned tips to create increased aerodynamic support |
| 11/11/1993 | WO1993022196A1 Lifting body with reduced-strength trailing vortices |
| 11/11/1993 | DE4208751A1 Reducing resistance to aerofoil or hydrofoil passing through medium e.g. air or water - uses array of teeth formed on leading and/or trailing edge of aerofoil or hydrofoil section |
| 11/11/1993 | CA2134197A1 Lifting body with reduced-strength trailing vortices |
| 10/27/1993 | EP0567350A1 Improved control system |
| 10/14/1993 | WO1993019978A1 Foil device |
| 10/12/1993 | US5252381 Airfoil with thick trailing edge |
| 10/12/1993 | US5251846 Supersonic aircraft shock wave energy recovery system |
| 09/16/1993 | WO1993017908A1 Thrust vectoring free wing aircraft |
| 09/16/1993 | CA2131986A1 Thrust vectoring free wing aircraft |
| 08/17/1993 | US5236152 Heat exchanging to cool vehicle surfaces and produce fuel from hydrocarbons concurrently |
| 08/17/1993 | US5236149 Boundary layer control device for tilt rotor configuration |
| 08/17/1993 | CA1321382C Profiles for air shrouded propeller blade |
| 07/27/1993 | CA1320715C Airfoiled blade |
| 07/20/1993 | US5229562 Process for consolidation of composite materials |
| 07/13/1993 | US5226618 Lift enhancement device |
| 07/06/1993 | US5224826 Piezoelectric helicopter blade flap actuator |
| 07/06/1993 | US5224670 Composite focused load control surface |
| 07/06/1993 | US5224665 Split span vee tail control arrangement for air vehicle |
| 06/29/1993 | US5222699 Variable control aircraft control surface |
| 06/24/1993 | WO1993012001A1 Aerodynamic profile with fixed external contour |
| 06/24/1993 | WO1993012000A1 Aerodynamic profile with fixed external contour |
| 06/23/1993 | CN1073406A Aircraft having light and small wings without airfield |
| 06/14/1993 | EP0594625A4 Supersonic aircraft shock wave energy recovery system. |
| 06/09/1993 | DE4140139A1 Aircraft which can be converted from biplane to monoplane - has short take-off and landing capability but high cruising speed |
| 06/08/1993 | US5216799 Carbon fibre composite wing manufacture |
| 05/27/1993 | WO1993010000A1 Lockable free wing aircraft |
| 05/25/1993 | US5213287 Wing modification method and apparatus |
| 05/18/1993 | US5211358 Airfoil deployment system for missile or aircraft |
| 04/28/1993 | EP0538963A1 Three-position variable camber krueger leading edge flap |
| 04/27/1993 | US5205519 Boundary layer relaminarization device |
| 04/15/1993 | DE4133491A1 Adaptation of bird wing structures to glider wing - involves top line curvature on wing suction side with the same curvature over entire span |
| 04/13/1993 | US5201479 Self-monitoring latch pin lock for folding wing aircraft |
| 04/08/1993 | DE4132665A1 Wing profile for aircraft - enables short take-off and landing capability and is suitable for flying speeds of 800 KM/HR. |
| 03/31/1993 | EP0533915A1 Rotor flap apparatus and method |
| 03/23/1993 | US5195702 Rotor flap apparatus and method |
| 03/17/1993 | EP0532016A1 Composite focused load control surface |
| 03/09/1993 | US5192037 Double-pivoting deployment system for aerosurfaces |
| 03/03/1993 | EP0529917A1 Fusion bonded thermoplastic leading edge for aircraft aerodynamic surfaces |
| 02/18/1993 | WO1993002915A1 Aerofoil with variable geometry expansion surface |
| 02/16/1993 | US5186420 Articulated fin/wing control system |
| 02/03/1993 | EP0525912A1 Wing/winglet configurations and methods for aircraft |
| 01/26/1993 | US5181678 Flexible tailored elastic airfoil section |
| 01/14/1993 | DE4120908A1 Wind energy extraction aerofoil - has trough-shaped front sheet and flatter rear sheet leading into trough at front end |
| 01/12/1993 | US5178348 Contoured wing/flap assembly and method |
| 10/29/1992 | WO1992018383A1 Rotor flap apparatus and method |
| 10/27/1992 | US5158252 Three-position variable camber Krueger leading edge flap |
| 10/15/1992 | DE4210065A1 Wing for light aircraft - has supporting ribs with hinged joints to enable ribs to be folded for convenient transport |
| 10/13/1992 | US5154373 Integral structure and thermal protection system |
| 09/29/1992 | US5151014 Lightweight airfoil |
| 09/29/1992 | US5150864 Variable camber control of airfoil |
| 09/23/1992 | EP0505133A1 Wing root aerofoil for forward swept wings |
| 08/20/1992 | WO1992013758A1 Flexible tailored elastic airfoil section |
| 08/18/1992 | CA1306455C Wing trailing edge air dam |
| 08/18/1992 | CA1306384C Torsion spring powered missile wing deployment system |
| 08/12/1992 | CN1017792B Airfoiled blade |
| 07/23/1992 | WO1992012049A1 Airfoil with fixed and variable upper and lower camber portions |
| 06/19/1992 | CA2057762A1 Mechanical linkage device between a ceramic material and a metal, specifically for a leading edge on a rudder |
| 06/02/1992 | US5118052 Variable geometry RPV |
| 05/19/1992 | US5114104 Articulated control surface |
| 05/13/1992 | EP0485027A2 Carbon fibre composite wing manufacture |
| 05/13/1992 | EP0245435B1 Torsion spring powered missile wing deployment system |
| 05/12/1992 | US5112120 Natural flow wing |
| 05/07/1992 | DE4034511A1 Aircraft propeller with two blades mounted one above other - with gap between blades functioning as nozzle |
| 04/14/1992 | US5104061 Dual eccentric bearing for adjustment of pivoting aircraft wings |
| 03/24/1992 | US5098034 Vertical/short takeoff or landing aircraft having a rotatable wing and tandem supporting surfaces |
| 03/11/1992 | EP0464158A4 Lightweight airfoil |