Patents
Patents for B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for (1,943)
09/2010
09/28/2010CA2593953C Active systems and methods for controlling an airfoil vortex
09/23/2010DE102009006212A1 Method for increasing lifting of e.g. aerofoil, for use in aerodynamically-flying aircraft, involves arranging body above another body in aerodynamic-flow, and moving aerofoil upwardly by parts during application of air flow
09/22/2010EP2230175A2 Microvanes for aircraft aft body drag reduction
09/21/2010US7798448 Flow-driven oscillating acoustic attenuator
09/16/2010WO2010103194A2 Mechanical movements adjusted by electromagnetic probe
09/16/2010WO2010103193A2 Complex balancing of a rotating mechanical part
09/16/2010CA2755295A1 Complex balancing of a rotating mechanical part
09/15/2010CN101830280A Aerodynamic configuration of aircraft
09/10/2010WO2010100048A2 Wing for an airplane having a winglet on the wing tip
09/09/2010DE102004056537B4 Anordnung zur Minderung des aerodynamischen Lärms an einem Zusatzflügel eines Flugzeuges Arrangement for reducing aerodynamic noise at a supplementary wing of an airplane
09/08/2010CN1571745B Aircraft configuration with improved aerodynamic performance
09/01/2010EP2223853A1 Fluid dynamic area with a turbine driven by the flow induced by the area subject to the flow
08/2010
08/26/2010US20100213320 Device which is subject to fluid flow
08/20/2010CA2693641A1 Device which is subject to fluid flow
08/18/2010EP2217491A2 Wingtip extension for reduction of vortex drag in aircraft
08/18/2010CN1845848B Flow-mechanically effective surface for minimizing induced resistance
08/17/2010US7775480 Flying object for transonic or supersonic velocities
08/17/2010CA2412913C Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing
08/11/2010EP2215330A1 Aerodynamic performance enhancements using discharge plasma actuators
08/11/2010CN101348170B Wing structure having lamellar flow flowing control and separation control
08/04/2010EP2212193A1 Method and device for reducing the induced speeds in vortices in the wake of an aircraft
08/03/2010US7766279 Vortex ring generator
07/2010
07/29/2010US20100187366 Reduction of Tip Vortex and Wake Interaction Effects in Energy and Propulsion Systems
07/22/2010US20100181432 Curved Wing Tip
07/21/2010CN101195348B Fluid motion device for accelerating and energy-saving
07/20/2010US7757991 Helicopter blade vortex interaction noise reducing method and device
07/15/2010WO2009149932A3 Device for generating aerodynamic vortices, and regulating flap and wing comprising a device for generating aerodynamic vortices
07/15/2010US20100176249 Engine Nacelle Of An Aircraft Comprising A Vortex Generator Arrangement
07/13/2010US7755519 Ultrasonic communication and drag modification
07/13/2010US7753316 Deployable flap edge fence
07/08/2010WO2010077464A1 System and method for reducing viscous force between a fluid and a surface
07/06/2010US7751948 Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information
06/2010
06/29/2010USRE41398 Design of viscoelastic coatings to reduce turbulent friction drag
06/29/2010US7744038 Controllable winglets
06/29/2010CA2556699C Apparatus and method for the control of trailing wake flows
06/24/2010US20100155541 Winglet
06/24/2010US20100155529 Landing gear with noise reduction fairing
06/17/2010US20100148010 Aircraft wing modification and related methods
06/16/2010EP2195236A2 Wingtip feathers, including paired, fixed feathers, and associated systems and methods
05/2010
05/19/2010CN101708742A Fluid movement device
05/19/2010CN101304918B Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
05/14/2010WO2010052446A1 Aircraft fairing
05/12/2010DE102005025004B4 Verfahren und Vorrichtung zum Abmindern der Zirkulation von Hauptwirbeln in Wirbelschleppen hinter Flugzeugen Method and apparatus for Abmindern the circulation of the main vortices in the wake behind aircraft
05/06/2010US20100108805 Aircraft Landing Gear Provided With At Least One Noise Reducing Means
05/04/2010US7708229 Circulation controlled airfoil
04/2010
04/29/2010WO2010046679A1 Bluff body noise control
04/29/2010WO2010006770A3 Aerodynamic flap and wing
04/29/2010WO2010002518A3 Systems and methods for alleviating aircraft loads with plasma actuators
04/27/2010US7703839 Airflow control devices based on active materials
04/27/2010CA2634307C Aircraft wing and fuselage contours
04/22/2010WO2010043834A1 Lift machine
04/14/2010EP2173616A1 Winglet
04/14/2010CN101300170B 飞机的制动襟翼 Aircraft brake flaps
04/08/2010US20100084508 High-lift device, wing, and noise reduction structure for high-lift device
04/01/2010WO2009143518A3 Boundary layer control system and methods thereof
04/01/2010US20100078863 Atmospheric turbulence isolation system and method
03/2010
03/31/2010EP2168869A1 Device for reducing the cross-stream force generated by the section of air refuelling booms
03/31/2010EP2167380A1 Engine nacelle of an aircraft comprising a vortex generator arrangement
03/31/2010CN101687543A Winglet
03/31/2010CN101687542A Engine nacelle of an aircraft comprising a vortex generator arrangement
03/09/2010US7673834 Vortex ring generator
02/2010
02/25/2010US20100044505 Helicopter blade vortex interaction noise reducing method and device
02/24/2010EP2156261A1 Surface vibration using compliant mechanical amplifiers
02/18/2010US20100038492 Retractable nacelle chine
02/16/2010US7661629 Systems and methods for destabilizing an airfoil vortex
02/11/2010DE102008035978A1 Method for blowout letting of eddies formed at flooded or drift surfaces, involves bringing thermal energy in current in such manner that it arrives in range of eddies
01/2010
01/28/2010US20100019094 Wing tip shape for a wing, in particular of aircraft
01/26/2010CA2264788C Active system for early destruction of trailing vortices
01/21/2010WO2009088780A3 Systems and methods for controlling flows with pulsed discharges
01/21/2010US20100012778 Torque link set
01/21/2010US20100012777 Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom
01/20/2010CN100581922C Upper surface control device of aircraft lift force surface
01/19/2010US7648100 Shock wave modification method and system
01/14/2010US20100006706 Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program and method for influencing post-turbulences
01/14/2010US20100006696 Landing gear noise reduction assembly
01/12/2010US7645969 Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus
01/12/2010US7644892 Blended winglet
01/07/2010WO2010002518A2 Systems and methods for alleviating aircraft loads with plasma actuators
01/06/2010EP2139763A1 Deployable flap edge fence
01/05/2010US7641153 Directed energy off-body heating for supersonic vehicle shockwave and sonic boom control
12/2009
12/31/2009US20090321559 Aircraft noise reduction apparatus
12/31/2009DE102008027618A1 Vorrichtung zur Bildung von aerodynamischen Wirbeln sowie Stellklappe und Tragflügel mit einer Vorrichtung zur Bildung von aerodynamischen Wirbeln Apparatus for forming vortices and aerodynamic control flap and wing with a device for formation of aerodynamic vortices
12/29/2009US7637462 Surface flow diverting and static charging ducted pores on wing or blade tip to reduce wake and BVI noise
12/24/2009US20090314885 System, method and apparatus for fluidic effectors for enhanced fluid flow mixing
12/23/2009WO2009124913A3 Flow controlling component
12/17/2009WO2009149932A2 Device for generating aerodynamic vortices, and regulating flap and wing comprising a device for generating aerodynamic vortices
12/17/2009WO2009079046A3 Systems and methods for control of engine exhaust flow
12/17/2009WO2009053649A8 Method and device for reducing the induced speeds in vortices in the wake of an airctaft
12/17/2009CA2727660A1 A device for the generation of aerodynamic vortices and also a regulating flap and wing with a device for the generation of aerodynamic vortices
12/10/2009DE102008025152A1 Triebwerksgondel eines Flugzeugs mit einer Wirbelgenerator-Anordnung Engine nacelle of an aircraft with a vortex generator assembly
12/03/2009WO2009074528A4 Wingtip extension for reduction of vortex drag in aircraft
11/2009
11/26/2009WO2009143518A2 Boundary layer control system and methods thereof
11/26/2009WO2009141536A1 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
11/26/2009US20090289149 Engine pod for an aircraft with a vortex generator arrangement
11/19/2009WO2009106871A3 Aerodynamic structure with non-uniformly spaced shock bumps
11/12/2009WO2009136012A1 Electron organization for dynamic chemical and mechanical performances
11/04/2009EP1960262B1 Rudder of a commercial aircraft
10/2009
10/28/2009CN101565102A Bionic airplane
10/22/2009WO2009129023A1 Winglets with recessed surfaces, and associated systems and methods
10/22/2009WO2009106873A3 Shock bump array
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