Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724) |
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04/15/1993 | WO1993008076A1 Method for controlling boundary layer on an aerodynamic surface of a flying vehicle, and a flying vehicle |
04/15/1993 | CA2098278A1 Method for control of the boundary layer on the aerodynamic surface of an aircraft, and the aircraft provided with the boundary layer control system |
04/14/1993 | EP0536874A1 Control of boundary layer flow |
04/13/1993 | US5201829 Flight control device to provide directional control |
03/17/1993 | EP0532093A1 Perforated wing panel with variable porosity |
12/16/1992 | EP0518592A1 Vortex suppression for an eductor |
12/15/1992 | US5171623 Drag reducing surface depressions |
12/14/1992 | CA2068110A1 Vortex suppression for an eductor |
12/09/1992 | EP0517459A1 Aircraft gas turbine engine bleed air energy recovery apparatus |
12/05/1992 | CA2068177A1 Aircraft gas turbine engine bleed air energy recovery apparatus |
12/01/1992 | WO1992021560A1 Boundary layer control |
12/01/1992 | US5167387 Porous airfoil and process |
12/01/1992 | CA2106850A1 Boundary layer control |
12/01/1992 | CA1310943C Airfoil-shaped body |
10/27/1992 | US5158251 Aerodynamic surface tip vortex attenuation system |
10/20/1992 | US5156353 Aircraft pylon |
09/02/1992 | EP0500875A1 Rotor |
09/01/1992 | US5143329 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
08/25/1992 | US5141182 Gas turbine engine fan duct base pressure drag reduction |
08/12/1992 | EP0498559A1 Method of providing a patterned surface on a substrate |
08/11/1992 | US5137230 Aircraft gas turbine engine bleed air energy recovery apparatus |
08/07/1992 | CA2060583A1 Method of providing a patterned surface on a substrate |
07/28/1992 | US5133519 Drag reduction method and surface |
07/28/1992 | US5133516 Drag reduction article |
06/30/1992 | US5125597 Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system |
06/17/1992 | EP0489871A1 System and method for suppressing noise produced by rotors |
06/09/1992 | CA1302841C Diffuser |
05/19/1992 | US5114103 Aircraft engine electrically powered boundary layer bleed system |
05/19/1992 | US5114102 Boundary layer control |
05/19/1992 | US5114100 Anti-icing system for aircraft |
05/19/1992 | US5114099 Surface for low drag in turbulent flow |
04/28/1992 | US5107626 Method of providing a patterned surface on a substrate |
03/15/1992 | WO1992005341A1 Rotor |
03/15/1992 | CA2068539A1 Rotor |
03/11/1992 | EP0464158A4 Lightweight airfoil |
02/28/1992 | CA2046765A1 Aircraft engine electrically powered boundary layer bleed system |
01/08/1992 | EP0464158A1 Lightweight airfoil. |
12/24/1991 | US5075564 Combined solar and wind powered generator with spiral surface pattern |
12/10/1991 | CA1292931C Patterned, conformable sheet material for drag reduction |
12/04/1991 | EP0459816A1 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
12/04/1991 | EP0459815A1 Gas turbine engine fan duct base pressure drag reduction |
12/03/1991 | US5069403 Applying patterned radiation curable polymer; curing |
12/03/1991 | US5069397 Stabilized aero-optical free shear layer interface |
12/02/1991 | CA2042201A1 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
09/24/1991 | US5050819 Rotatable non-circular forebody flow controller |
07/11/1991 | WO1991009776A1 Venturi-enhanced airfoil |
07/10/1991 | EP0436243A2 Anti-icing system for aircraft |
06/25/1991 | US5026232 Boundary layer devices |
05/21/1991 | US5016837 Venturi enhanced airfoil |
05/02/1991 | EP0425136A1 Mask and method for the production of at least one groove, rib or different intensity strip in or on a surface |
04/22/1991 | CA2028039A1 Mask and method for the production of at least one groove, rib or different intensity strip in or on a surface |
03/21/1991 | WO1991003623A1 System and method for suppressing noise produced by rotors |
02/19/1991 | US4994639 Methods of manufacture and surface treatment using laser radiation |
02/19/1991 | US4993663 Engine of an aircraft |
02/05/1991 | US4989810 Method and apparatus for influencing a laminar turbulent boundary layer transition on bodies in flow |
01/22/1991 | US4986496 Drag reduction article |
01/10/1991 | WO1991000212A1 Lightweight airfoil |
12/19/1990 | EP0305374B1 Aerodynamic components having leading edge devices |
12/11/1990 | US4976349 Aerofoil/hydrofoil |
12/04/1990 | US4974633 System for controlling the flow of a fluid medium relative to an object |
12/01/1990 | CA2012248A1 Hybrid laminar flow nacelle |
09/05/1990 | EP0319574A4 Venturi enhanced airfoil |
08/29/1990 | EP0383852A1 Improvements in or relating to reduction of drag |
07/18/1990 | EP0378340A2 Methods of manufacture and surface treatment using laser radiation |
07/05/1990 | DE3913678C1 Boundary flow regulator for control bodies - uses evaluator circuit supplied by sensors measuring surface pressure and flow distribution |
06/12/1990 | US4932612 Method and apparatus for reducing turbulent skin friction |
06/12/1990 | US4932610 Active control of boundary layer transition and turbulence |
06/05/1990 | US4930729 Control of fluid flow |
05/10/1990 | DE3835213A1 Wing construction for energy transmission in the media of water and gas, and for a vehicle for movement on land or water and in the air |
05/03/1990 | DE3836673A1 Method and arrangement for reducing the induced drag of a wing |
04/03/1990 | US4913381 Aerodynamic components having leading edge devices |
03/14/1990 | CN1007171B Airstream eductor |
03/13/1990 | US4907765 Wall with a drag reducing surface and method for making such a wall |
03/08/1990 | WO1990002079A1 Generation of an aerodynamic force by lateral blowing of air at the underwing of aircraft wings from the wing extremities towards the wing root at the aircraft fuselage |
03/07/1990 | EP0356601A1 Improvements in jet-propelled aircraft |
02/07/1990 | EP0354022A2 Drag reduction article |
01/23/1990 | US4895323 Rag control for powered lift aircraft |
01/11/1990 | WO1989011343A3 Improvements in or relating to reduction of drag |
01/02/1990 | US4890803 Airfoil with fixed and variable upper camber portions |
12/20/1989 | EP0216384B1 Device to reduce friction drag |
11/30/1989 | WO1989011343A2 Improvements in or relating to reduction of drag |
10/10/1989 | US4872484 System for controlling the flow of a fluid medium relative to an object |
09/12/1989 | US4865271 Boundary layer devices |
09/05/1989 | US4863121 Boundary layer devices |
08/31/1989 | DE3804931A1 Method for directional control of a missile flying in the relatively high supersonic domain, and such a missile |
08/29/1989 | US4860976 Attached jet spanwise blowing lift augmentation system |
07/18/1989 | US4848701 Vertical take-off and landing aircraft |
07/04/1989 | US4844385 Pneumatic aerodynamic control surface |
06/14/1989 | EP0319574A1 Venturi enhanced airfoil |
06/06/1989 | US4836473 Apparatus for influencing a boundary layer on the surface of a body moving through a medium |
05/23/1989 | CA1254547A1 Surface exhibiting reduced flow resistance of a body over which turbulent flow takes place |
05/17/1989 | EP0315806A2 Method and device to cause the laminar-turbulent boundary layer transition on a body |
05/16/1989 | US4830315 Airfoil-shaped body |
05/10/1989 | EP0315563A1 Convoluted plate to reduce base drag |
03/21/1989 | US4813635 Projectile with reduced base drag |
03/21/1989 | US4813633 Airfoil trailing edge |
03/21/1989 | US4813631 Laminar flow control airfoil |
03/08/1989 | EP0305374A1 Aerodynamic components having leading edge devices. |
02/28/1989 | US4807831 Combination boundary layer control system for high altitude aircraft |
12/29/1988 | WO1988010210A1 Venturi enhanced airfoil |