| Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724) |
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| 07/17/2008 | WO2008057586A3 Oscillating vane actuator apparatus and method for active flow control |
| 07/17/2008 | WO2008054831A9 Aircraft payload retention system for interior loads |
| 07/10/2008 | WO2008048217A3 Oscillating vane actuator apparatus and method for active flow control |
| 07/08/2008 | CA2372295C Passively driven acoustic jet controlling boundary layers |
| 07/02/2008 | EP1937552A2 Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
| 06/26/2008 | WO2008075106A1 Establishment of laminar boundary layer flow on an aerofoil body |
| 06/26/2008 | CA2673594A1 Establishment of laminar boundary layer flow on an aerofoil body |
| 06/18/2008 | EP1931566A2 Oscillating vane actuator apparatus and method for active flow control |
| 06/12/2008 | WO2008069937A2 Active control of a body by altering surface drag |
| 06/10/2008 | CA2364321C Centrifugal air flow control |
| 06/10/2008 | CA2364319C Vibration-driven acoustic jet controlling boundary layer separation |
| 06/10/2008 | CA2361824C Tangentially directed acoustic jet controlling boundary layers |
| 06/05/2008 | US20080128561 Active control of a body by altering surface drag |
| 06/04/2008 | EP1926660A1 Advanced trailing edge control surface on the wing of an aircraft |
| 06/04/2008 | EP1401692B1 Hybrid air boost vehicle and method for making same |
| 05/28/2008 | EP1585665B1 Proprotor blade with leading edge slot |
| 05/22/2008 | CA2667619A1 Device for delaying boundary layer separation |
| 05/15/2008 | WO2008057586A2 Oscillating vane actuator apparatus and method for active flow control |
| 05/15/2008 | DE102006054428B3 Boundary layer defecting device for e.g. military missile, has body arranged in front edge area of airfoil, where arms of fuselage rest on upper and lower sides of airfoil and apex of device points towards body of missile |
| 05/14/2008 | EP1919772A2 System for aerodynamic flows and associated method |
| 05/08/2008 | WO2008054831A2 Aircraft payload retention system for interior loads |
| 05/08/2008 | DE10361390B4 Verfahren und Einrichtung zur Absaugung der Grenzschicht Method and apparatus for extracting the boundary layer |
| 05/02/2008 | WO2008051074A1 Object with surface for generating micro swirls |
| 04/30/2008 | DE102006049616A1 Aerodynamic component has slits at the trailing edge, running between the upper and lower main surfaces, to reduce air turbulence noise emissions |
| 04/29/2008 | US7364118 Propulsion arrangement |
| 04/24/2008 | WO2008048217A2 Oscillating vane actuator apparatus and method for active flow control |
| 04/17/2008 | WO2008044941A2 Method, system and apparatus for producing a potential over a body |
| 04/17/2008 | US20080087771 High performance synthetic valve/pulsator |
| 04/15/2008 | CA2344950C Noise reducing vortex generators on aircraft wing control surfaces |
| 04/09/2008 | EP1907279A1 An element for generating a fluid dynamic force |
| 04/03/2008 | WO2008037865A1 Vertical take-off and landing vehicle which does not have a rotary wing |
| 04/03/2008 | CA2664424A1 Vertical take-off and landing vehicle which does not have a rotary wing |
| 04/02/2008 | EP1905487A1 A flyable object and a method of manufacturing the same |
| 04/02/2008 | EP1592883B1 Device for improving wind turbine blade performance |
| 04/02/2008 | CN101155727A Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows |
| 03/27/2008 | DE102006043462A1 Aerodynamic component e.g. rotor blade, for use in wind turbine, has pair of surface units on high pressure side engaged between two surface units on low pressure side in main extension direction of trailing edge |
| 03/26/2008 | CN101148195A Wing knife and its intensified auxiliary tool wingtip air jetting wing |
| 03/20/2008 | US20080067283 Methods and apparatus for reducing noise via a plasma fairing |
| 03/19/2008 | EP1392562A4 Aerofoil with gas discharge |
| 03/13/2008 | WO2008029095A1 Flow control actuators |
| 03/13/2008 | WO2008029049A1 Panel assembly and method of erecting a panel assembly |
| 03/13/2008 | US20080061192 Method and apparatus for mitigating trailing vortex wakes of lifting or thrust generating bodies |
| 03/12/2008 | CN101139010A Device for improving airplane ascensional force |
| 03/05/2008 | CN100372735C Proprotor blade with leading edge slot |
| 02/14/2008 | WO2007133239A3 Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
| 01/31/2008 | US20080023590 Boundary layer pumped propulsion system for vehicles |
| 01/31/2008 | US20080023589 Systems and methods for controlling flows with electrical pulses |
| 01/15/2008 | US7318619 Method and apparatus for reducing drag and noise for a vehicle |
| 01/03/2008 | US20080001035 Fixing system for a leading edge to the structure of an aircraft lift plane |
| 01/02/2008 | EP1873395A1 Method for operating a device with at least one fluid dynamic uplift device, in particular in a wind farm |
| 12/26/2007 | EP1868890A1 Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows |
| 12/19/2007 | CN100356076C Solid body having microstructured surface |
| 12/12/2007 | EP1863703A1 Steering of vehicles through boundary layer control |
| 11/22/2007 | WO2007133239A2 Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft |
| 11/22/2007 | US20070266707 Boundary Layer Suction Arrangement |
| 11/22/2007 | CA2625520A1 Plasma actuators for drag reduction on wings,nacelles and/or fuselage of vertical take-off and landing aircraft |
| 11/20/2007 | US7296411 Method and system for regulating internal fluid flow within an enclosed or semi-enclosed environment |
| 11/14/2007 | EP1565659B1 Method and device for generating mixtures of fluids in a boundary layer |
| 11/06/2007 | US7290738 Dual jet emerging lift augmentation system for airfoils and hydrofoils |
| 11/01/2007 | WO2007123612A1 Inlet distortion and recovery control system |
| 11/01/2007 | WO2007095931A3 Aerodynamic flap of an aircraft with a device which influences the flap turbulence |
| 10/25/2007 | WO2007072259A3 Controlling the boundary layer of an airfoil |
| 10/24/2007 | EP1519873B1 Airship and method of operation |
| 10/11/2007 | DE102004024007B4 Flugzeugkomponente, insbesondere Flügel Aircraft component, in particular wing |
| 10/10/2007 | CN101052565A High-lift distributed active flow control system and method |
| 10/09/2007 | US7278825 Method and system for regulating fluid over an airfoil or a hydrofoil |
| 10/04/2007 | US20070228222 Method of improving lift of an aircraft wing |
| 10/04/2007 | CA2542920A1 Method of improving lift of an aircraft wing |
| 10/02/2007 | US7275721 Arrangement for generating vortexes |
| 09/27/2007 | US20070221788 Aircraft Component |
| 09/12/2007 | EP1585665A4 Proprotor blade with leading edge slot |
| 09/06/2007 | DE102006008864A1 Flow surface element for vehicle e.g. aircraft has plasma production unit arranged as dielectric obstructed unloading unit, and unit is inserted global approximately across incoming flow of element arranged by motion of vehicle |
| 09/05/2007 | EP1827974A2 High-lift distributed active flow control system and method |
| 09/05/2007 | EP1827970A2 Apparatus, system and method for drag reduction |
| 09/04/2007 | US7264444 Aerofoils |
| 08/30/2007 | WO2007095931A2 Aerodynamic flap of an aircraft with a device which influences the flap turbulence |
| 08/30/2007 | CA2643071A1 Aerodynamic flap of an aircraft with a device which influences the flap turbulence |
| 08/23/2007 | US20070194178 Passive micro-roughness array for drag modification |
| 08/22/2007 | EP1755947B1 Aircraft component, in particular a wing |
| 08/14/2007 | US7255309 Vernier active flow control effector |
| 08/09/2007 | US20070181743 Method for streamline traced external compression inlet |
| 08/09/2007 | DE10163585B4 Tragwerk-Profilstruktur eines Flugzeuges Wing unit profile structure of an aircraft |
| 08/01/2007 | CN1329244C Method and system for producing a potential over a body |
| 07/19/2007 | WO2007080333A1 Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method |
| 07/19/2007 | CA2632873A1 Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method |
| 07/12/2007 | WO2006137857A3 Vertical or short take off and landing vehicle |
| 07/11/2007 | CN1325327C Recesses on surface |
| 07/04/2007 | EP1578600B1 Drag reduction multilayer film and method of use |
| 06/26/2007 | US7234921 Method for increasing operating efficiency of the rotor blade of an aerogenerator (variants) |
| 06/14/2007 | WO2007022315A3 Integrated pulse detonation engine in a lifting surface with supercirculation |
| 06/14/2007 | CA2670268A1 Device for reducing a drag produced by the relative displacement of a body and fluid |
| 06/05/2007 | US7226015 Aircraft and missile forebody flow control device and method of controlling flow |
| 05/24/2007 | US20070113403 Method for increasing a blade performance (variants) |
| 05/23/2007 | CN1317163C Wave-shaped straight wing |
| 05/18/2007 | WO2007055088A1 Energy-saving jet aircraft |
| 05/18/2007 | WO2007054150A1 Advanced trailing edge control surface on the wing of an aircraft |
| 05/18/2007 | CA2622320A1 Advanced trailing edge control surface on the wing of an aircraft |
| 05/10/2007 | WO2007021480A3 System for aerodynamic flows and associated method |
| 05/08/2007 | US7213788 Microjet-based control system for cavity flows |
| 05/02/2007 | EP1778539A2 High performance airfoil with co-flow jet flow control |