Patents
Patents for B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for (1,943)
06/2011
06/08/2011CN102089207A Winglets with recessed surfaces, and associated systems and methods
06/07/2011US7954768 Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators
06/03/2011WO2011064456A1 Flying apparatus
06/02/2011US20110127383 Active winglet
05/2011
05/25/2011CN101421156B Inlet distortion and recovery control system
05/24/2011US7948152 Cladding comprising an integrated polymer actuator for the deformation of said cladding
05/19/2011US20110114795 Aerodynamic Flap and Wing
05/18/2011EP2321084A1 System and method for aerodynamic flow control
05/12/2011WO2011055062A1 Engine pylon comprising a vortex generator, and method for the production thereof
05/11/2011EP2318271A2 Aerodynamic flap and wing
05/11/2011CN102056796A Device for generating aerodynamic vortices, and regulating flap and wing comprising a device for generating aerodynamic vortices
05/05/2011US20110101173 Aircraft with Aerodynamic Lift Generating Device
05/05/2011US20110101169 Device for the generation of aerodynamic vortices and also a regulating flap and wing with a device for the generation of aerodynamic vortices
05/05/2011US20110101168 Method of Controlling an Aircraft in Flight, Especially to Reduce Wake Vortices
05/04/2011EP2316729A2 An element for generating a fluid dynamic force
05/04/2011EP2316728A2 Prismatic-shaped vortex generators
05/03/2011US7934686 Reducing drag on a mobile body
04/2011
04/27/2011EP2069199B1 Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift
04/27/2011CN102030104A Rotor platform of aerodynamic force and method of aerodynamic force generation
04/19/2011CA2471816C Vortex ring generator
04/19/2011CA2431488C Aircraft with elliptical winglets
04/14/2011WO2011043431A1 Wing structure and fairing device
04/13/2011EP2307273A2 Systems and methods for alleviating aircraft loads with plasma actuators
04/13/2011CN102015447A Non-planar wing tip device for wings of aircraft, and wing comprising such a wing tip device
04/06/2011EP2303685A1 Curved wing tip
03/2011
03/31/2011WO2010100048A3 Wing for an airplane having a winglet on the wing tip
03/24/2011WO2010063600A3 Vortex dynamics turbine
03/16/2011EP2293978A2 Device for generating aerodynamic vortices, and regulating flap and wing comprising a device for generating aerodynamic vortices
03/16/2011EP1907279B1 An element for generating a fluid dynamic force
03/08/2011US7900877 Active winglet
03/08/2011US7900876 Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
03/03/2011WO2011023270A1 Flow determination method
03/03/2011CA2745315A1 Flow determination method
02/2011
02/23/2011EP2287072A2 Fluidfoil tip vortex disruption
02/23/2011EP2286092A1 Wing-tip device for the tip of a wing, the blade of a wind generator or of a marine generator for reducing or even cancelling what are known as wing tip vortices
02/23/2011EP2285674A2 Boundary layer control system and methods thereof
02/10/2011WO2011016808A1 Solid state supersonic flow actuator and method of use
02/10/2011DE202010015816U1 Aufbau zur Leistungssteigerung und Geräuschverringerung für einen Propeller Structure to improve performance and noise reduction for a propeller
02/10/2011DE202010015814U1 Aufbau zur Verringerung von bei Bewegung eines Objektes entstehenden Widerständen Structure to reduce resulting from movement of an object resistors
02/09/2011EP2281747A2 Aircraft
02/09/2011CN101970294A Aerodynamic structure with asymmetrical shock bump
02/03/2011US20110024574 Aerodynamic Body And High-Lift System Comprising Such An Aerodynamic Body
02/03/2011US20110024573 Extended winglet with load balancing characteristics
02/02/2011CN101965291A Shock bump array
02/01/2011US7878457 Retractable vortex generator
01/2011
01/26/2011EP2276665A1 Winglets with recessed surfaces, and associated systems and methods
01/26/2011CN101959756A Shock bump
01/26/2011CN101959755A Aerodynamic structure with non-uniformly spaced shock bumps
01/25/2011US7874524 Methods and apparatus for a multi-segment flap fence
01/25/2011US7874523 Method of controlling an aircraft in flight, especially to reduce wake vortices
01/20/2011US20110011463 Reducing drag on a mobile body
01/19/2011EP2274202A1 Non-planar wing tip device for wings of aircraft, and wing comprising such a wing tip device
01/13/2011WO2011004262A1 Elastomeric vortex generators
01/13/2011WO2011004261A1 Application of conformal sub boundary layer vortex generators to a foil of aero / hydrodynamic surface
01/13/2011CA2767139A1 Elastomeric vortex generators
01/13/2011CA2767135A1 Application of conformal sub boundary layer vortex generators to a foil of aero/hydrodynamic surface
01/12/2011EP2272753A1 Gas flow control device
01/12/2011CN101224790B Aerocraft equipped with airstream channel
01/11/2011US7866608 Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
01/04/2011US7861966 Supersonic aircraft footprint spreading control system and method
12/2010
12/29/2010WO2010148508A1 Drag-reducing device
12/29/2010CN101932507A Aerodynamic structure with series of shock bumps
12/29/2010CA2765735A1 Drag-reducing device
12/23/2010WO2010124877A8 Non-planar wing tip device for wings of aircraft, and wing comprising such a wing tip device
12/21/2010US7854467 Airflow control devices based on active materials
12/16/2010US20100314500 Shock bump
12/15/2010EP1373066B1 Turbulent flow drag reduction
12/09/2010US20100308177 Plasma enhanced riblet
12/09/2010US20100308176 Aerodynamic structure with non-uniformly spaced shock bumps
12/08/2010EP2010429B1 Inlet distortion and recovery control system
12/08/2010EP1986912B1 Aerodynamic flap of an aircraft with a device which influences the flap turbulence
12/02/2010US20100301173 Aerodynamic structure with asymmetrical shock bump
12/02/2010US20100301172 Aerodynamic structure with series of shock bumps
12/02/2010US20100301171 Shock bump array
12/01/2010CN101898635A Duct single screw aircraft based on Magnus effect
11/2010
11/25/2010US20100294891 Wingtip extension for reduction of vortex drag in aircraft
11/25/2010US20100294890 Method and device for reducing the induced speeds in vortices in the wake of an aircraft
11/24/2010CN101896401A Wingtip extension for reduction of vortex drag in aircraft
11/18/2010US20100288876 Bluff body noise control
11/18/2010DE102009003084A1 Verkleidung für eine Auftriebshilfe Panel for a buoyancy aid
11/17/2010EP2250088A2 Aerodynamic structure with non-uniformly spaced shock bumps
11/17/2010EP2250087A2 Aerodynamic structure with series of shock bumps
11/17/2010EP2250086A2 Shock bump
11/17/2010EP2250085A2 Shock bump array
11/16/2010US7832689 Element for generating a fluid dynamic force
11/11/2010WO2010129722A1 Aircraft winglet design having a compound curve profile
11/11/2010CA2761317A1 Aircraft winglet design having a compound curve profile
11/10/2010EP2247498A2 Wing control devices
11/10/2010EP2247497A2 Aerodynamic structure with asymmetrical shock bump
11/09/2010CA2622938C Smart vortex generator and aircraft, vessel and rotary machine being equipped with the same
11/04/2010WO2010124877A1 Non-planar wing tip device for wings of aircraft, and wing comprising such a wing tip device
11/04/2010US20100276006 Ultrasonic drag modulation
11/04/2010CA2723084A1 Non-planar wing tip device for wings of aircraft, and wing comprising such a wing tip device
11/02/2010CA2613680C Integrated wingtip extensions for jet transport aircraft and other types of aircraft
10/2010
10/27/2010EP2019776B1 Aircraft comprising a device for reducing the induced drag
10/14/2010WO2010116658A1 Method of reducing noise of air vehicle, leg structure of air vehicle and air vehicle
10/14/2010CA2755265A1 Method of attenuating noise in aircraft, landing gear structure of aircraft, and aircraft
09/2010
09/30/2010DE202010010399U1 Schall-Auftrieb-Technologie Sound Boost Technology
09/30/2010DE102009001953A1 Vorrichtung zur Beeinflussung einer Überschall-Umströmung Device for influencing a supersonic flow around
09/29/2010EP2233395A1 Winglet with autonomously actuated tab
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