Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724) |
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01/23/2014 | US20140021304 Profile plate portion for use as an outer wall of a flow body, method for manufacturing a profile plate portion and flow body component comprising a suction-extraction device for fluid |
01/23/2014 | US20140021302 Spin Resistant Aircraft Configuration |
01/22/2014 | EP2687439A1 Laminar flow panel |
01/22/2014 | CN103523208A Method for controlling plasma flow of wing lift-rising apparatus |
01/02/2014 | DE102007027697B4 Wirbelgeneratoranordnung an der Triebwerksgondel eines Flugzeugs Vortex generator assembly to the engine nacelle of an aircraft |
01/01/2014 | CN103482055A Active control method and device for aerofoil drag reduction |
12/31/2013 | US8616494 Switchable vortex generator and array formed therewith, and uses of the same |
12/27/2013 | WO2013064768A3 Turbo engine attachment pylon |
12/27/2013 | WO2013005113A3 Method for producing a surface of a component, said surface having reduced drag and component with reduced drag |
12/25/2013 | EP2675706A1 Laminar flow wing optimized for transonic cruise aircraft |
12/25/2013 | EP2389313B1 Aircraft wing with a main wing and a control flap installed on said wing |
12/19/2013 | WO2013187830A1 Miniature vortex generator |
12/19/2013 | US20130336781 Aircraft |
12/18/2013 | CN101765539B Translating flap drive door |
12/11/2013 | EP2670660A1 Method for manufacturing a flow body with a desired surface texturization and laser material removing device |
12/10/2013 | US8602361 Laminar flow monitor |
12/04/2013 | CN103419929A Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift |
12/03/2013 | US8596584 High-lift system for an aircraft with a main wing and an adjustable slat |
12/03/2013 | US8596573 Nacelle flow assembly |
11/27/2013 | EP2665909A2 Nacelle for an aircraft bypass turbojet engine |
11/27/2013 | EP2665908A2 Nacelle for an aircraft bypass turbojet engine |
11/27/2013 | CN103407570A Eddy current generating device for controlling lateral force of large-incidence-angle slender body |
11/20/2013 | EP2465772B1 Fluidic micro-generator of synthetic jets |
11/14/2013 | DE102009001953B4 Vorrichtung zur Beeinflussung einer Überschall-Umströmung Device for influencing a supersonic flow around |
11/07/2013 | US20130292511 Dielectric barrier discharge flight control system through modulated boundary layer transition |
11/06/2013 | EP2660442A2 Integrated thermal protection and leakage reduction in a supersonic air intake system |
11/06/2013 | EP2660148A1 Overpressure door for aircraft |
11/06/2013 | EP2660147A1 Unmanned air system (UAS) |
11/05/2013 | US8573541 Wavy airfoil |
11/02/2013 | CA2804729A1 Dielectric barrier discharge flight control system through modulated boundary layer transition |
10/31/2013 | WO2013163406A1 Method of using an active flow control system for lift enhancement or destruction |
10/31/2013 | US20130284294 Fluid actuator for influencing the flow along a flow surface, as well as blow-out device and flow body comprising a like fluid actuator |
10/24/2013 | US20130277502 Flow body having a leading edge, a surface and an active flow control system and vehicle comprising at least one such flow body and an air source |
10/23/2013 | CN103359281A Surface element for aircraft, aircraft and method for improving high-lift generation on a surface element |
10/22/2013 | US8561935 STOL and/or VTOL aircraft |
10/17/2013 | US20130270390 Aircraft having an aircraft fuselage and an air sucking fuselage component |
10/16/2013 | EP2650214A1 Structurally designed aerodynamic riblets |
10/16/2013 | EP2650213A1 Flow body having a leading edge, a surface and an active flow control system and vehicle comprising at least one such flow body and an air source |
10/16/2013 | EP2649310A2 Method and system of providing fluid flow for a rotor |
10/16/2013 | CN101332870B Plasma actuator system and method for use with a weapons bay on a high speed mobile platform |
10/15/2013 | US8556215 Aerodynamically efficient surfaces |
10/02/2013 | EP2644497A1 Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift |
10/02/2013 | EP2644496A1 Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element |
10/02/2013 | DE102012006194A1 Flugzeug mit einem Flugzeugrumpf und einer Luft absaugenden Flugzeugrumpfkomponente Airliner with a fuselage and an air aspirating fuselage component |
09/25/2013 | EP2641733A1 Elastomeric riblets |
09/25/2013 | CN103328800A Nacelle for an aircraft bypass turbojet engine |
09/19/2013 | US20130240676 High lift system for an aircraft |
09/18/2013 | CN103314219A Fluid actuator for influencing the flow along a flow surface, as well as blow-out device and flow body comprising a like fluid actuator |
09/18/2013 | CN103314206A Nacelle for an aircraft bypass turbojet engine |
09/11/2013 | EP2636594A1 Nose for supersonic flying object |
09/10/2013 | US8528601 Passive boundary layer control elements |
08/22/2013 | US20130214094 Nose for supersonic flying object |
08/22/2013 | DE102012002812A1 Flügel Wing |
08/22/2013 | DE102006008864B4 Strömungsflächenelement Flow surface element |
08/08/2013 | WO2013114342A1 Means for reducing air drag on an aircraft in flight |
08/07/2013 | EP2622230A1 Fluid actuator for influencing the flow along a flow surface, as well as blow-out device and flow body comprising a like fluid actuator |
08/07/2013 | CN103231796A Aircraft wing boundary layer separation inhibiting method based on plasma actuation |
08/07/2013 | CN102066196B Method for actively deforming an aerodynamic profile |
08/01/2013 | US20130193270 Structurally designed aerodynamic riblets |
07/31/2013 | EP2619085A1 Adaptive twist system for a rotor blade |
07/24/2013 | EP2616331A1 Plasma-enhanced active laminar flow actuator system |
07/23/2013 | US8490926 Multi-stage flow control actuation |
07/16/2013 | US8485476 Discrete co-flow jet (DCFJ) airfoil |
07/11/2013 | US20130175402 Air sucking vehicle fuselage component, method for producing an air sucking vehicle fuselage component and a vehicle, especially an aircraft, with an air sucking vehicle fuselage component |
07/10/2013 | CN103201172A Aircraft with wings and a system for minimizing the influence of unsteady flow states |
07/03/2013 | CN103183126A Anti-drag device of aircraft |
06/25/2013 | US8473122 Method for actively deforming an aerodynamic profile |
06/20/2013 | WO2013088068A1 Mounting pylon for an unducted fan |
06/20/2013 | DE102011121054A1 Riblet-Struktur auf einer Strömungsfläche, Verfahren zum Herstellen einer Riblet-Struktur auf einer Strömungsfläche und Verwendung von Verstärkungselementen in Riblets für eine Strömungsfläche Riblet structure on a flow surface, method of manufacturing a riblet structure on a flow surface and the use of reinforcement members in a flow area for riblets |
06/19/2013 | EP2604516A2 Minimally intrusive wingtip vortex wake mitigation using microvane arrays |
06/13/2013 | WO2013085671A1 Method of applying surface riblets to an aerodynamic surface |
06/13/2013 | CA2858540A1 Method of applying surface riblets to an aerodynamic surface |
06/12/2013 | CN101903245B Aircraft with aircraft cooling system |
06/11/2013 | US8459597 Integral suction device with acoustic panel |
05/29/2013 | EP2595880A1 Method and apparatus for controlling flow about a turret |
05/29/2013 | DE102011119421A1 Keel of e.g. underwater kite surfboard, has small recesses which are formed in round, ellipse or teardrop shape, in such a way that size, depth, and diameter of recess are set depending on size of keel |
05/29/2013 | CN103121505A Plate for reducing airflow resistance |
05/22/2013 | CN101318554B Plasma flow control actuator system and method |
05/15/2013 | EP2590858A1 Aircraft with wings and a system for minimizing the influence of unsteady flow states |
05/10/2013 | WO2013064768A2 Turbo engine attachment pylon |
05/10/2013 | CA2853903A1 Turbo engine attachment pylon |
05/07/2013 | US8434724 Air outlet system for aircraft leading edge |
05/07/2013 | US8434723 Low drag asymmetric tetrahedral vortex generators |
05/02/2013 | WO2013061276A1 Synchronization of fluidic actuators |
04/30/2013 | CA2691944C Translating flap drive door |
04/24/2013 | CN103057694A Open type control surface for Coanda effect aircraft |
04/23/2013 | US8424809 Control of aerodynamic forces by variable wetted surface morphology |
04/16/2013 | CA2565011C Boundary layer suction arrangement |
04/10/2013 | EP2578491A2 Boundary layer ingestion duct |
04/10/2013 | CN103029830A Double waverider splicing air suction type hypersonic aircraft forebody and design method thereof |
04/03/2013 | CN103010459A Method for reducing pneumatic noise of leading edge slat based on trailing edge micro-perforation |
03/26/2013 | US8403271 Passive robust flow control micro device |
03/20/2013 | CN202807091U Fixed wing for aircraft |
03/14/2013 | US20130062473 Flow body and method for taking in and/or blowing out fluid through a plurality of openings in a flow surface section of a flow body |
03/14/2013 | US20130062469 Surface entity for the reduction of the air resistance of an aviation vehicle |
03/14/2013 | DE102011112555A1 Strömungskörper und Verfahren zum Einsaugen und/oder Ausblasen von Fluid durch eine Mehrzahl von Öffnungen in einen Strömungsoberflächen-Abschnitt eines Strömungskörpers Flow body and method for sucking and / or blowing out of fluid through a plurality of openings in a flow surface portion of a flow body |
03/06/2013 | CN102951289A Low speed safety aircraft capable of controlling flight attitude by utilizing aerodynamic force |
03/06/2013 | CN102951167A High-speed railway based aerodynamic aerotrain with simulated wings on lateral sides of aerotrain body |
03/06/2013 | CA2788210A1 Aircraft tail surface with a leading edge section of undulated shape |
03/05/2013 | US8387923 Method for increasing the lift of aerodynamic surfaces and for reducing the drag |