Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64C - Aeroplanes; Helicopters › B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for
Patents for B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for (1,943)
05/2014
05/07/2014EP2727829A2 Wing fold controller
05/07/2014EP2727828A2 Wing fold system with latch pins through multiple mating lugs
05/07/2014EP2727827A2 Horizontal folding wingtip
05/07/2014EP2727826A2 Hinged raked wing tip
05/06/2014US8714473 Landing gear
05/01/2014WO2014065718A1 An integrated curved structure and winglet strength enhancement
05/01/2014US20140117166 Natural laminar flow wingtip
04/2014
04/30/2014EP2723640A1 Aircraft wing with wing tip device
04/30/2014CN103754354A Fluid power equipment with vortex control device and method for controlling vortex
04/16/2014EP2718183A1 The split spiroid
04/16/2014EP2718182A1 The split blended winglet
04/16/2014CN103732492A The split blended winglet
04/15/2014US8695915 Flap side edge liners for airframe noise reduction
04/09/2014EP2716544A1 horizontal airfoil tip fairing
04/09/2014CN103717490A The split spiroid
04/08/2014CA2620510C Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
04/03/2014WO2014049328A1 Airflow modification patch and method
04/03/2014US20140091180 Systems and Methods for Attenuation of Noise and Wakes Produced by Aircraft
04/01/2014US8684315 Active winglet
03/2014
03/27/2014WO2014046569A1 Method for optimizing the aerodynamic characteristics of elongate bodies with an ogive or pointed nose
03/26/2014CN203497169U Plane-body-top interceptor of unmanned plane
03/26/2014CN103661930A Integrated wingtip extensions for an jet transport aircraft and other types of aircrafts
03/26/2014CN103661929A Plasma unmanned aerial vehicle
03/26/2014CN102239084B System and method for reducing viscous force between a fluid and a surface
03/13/2014WO2014039636A1 Multicant winglets
03/13/2014US20140070056 Aricraft with improved aerodynamic performance
03/05/2014CN102549274B Wing structure and fairing device
02/2014
02/27/2014WO2012131335A9 Joint
02/27/2014US20140053914 Shock Wave Modification Method and System
02/25/2014US8657236 Aircraft provided with aerodynamic seal for reduction of noise generated by aircraft control surfaces
02/25/2014US8656957 Vortex generators to control boundary layer interactions
02/20/2014WO2013181722A3 Road-and-air transport vehicle
02/19/2014EP2697114A1 Propulsion device having unducted counter-rotating and coaxial rotors
02/18/2014US8651427 Wing tip device with recess in surface
02/18/2014US8651426 Jet engine installation
02/12/2014CN103569354A Aerodynamic, blunt aft body
02/12/2014CN103569351A Canard with double-rear-sweep-angle leading edge
02/06/2014DE102012214734B3 Portion of supersonic flow channel used in jet engine, has plane that is extended upstream of recess, and introducing portion and projection that are arranged in cross-section recess
02/05/2014EP2692632A1 High-lift device for aircraft
02/04/2014US8640995 System and method for aerodynamic flow control
01/2014
01/31/2014CA2822665A1 Aircraft wing having continuously rotating wing tips
01/29/2014EP2690008A1 Aerodynamic, blunt aft body
01/29/2014CN103547505A 接头 Connector
01/28/2014US8636254 Dynamically controlled cross flow instability inhibiting assembly
01/21/2014US8632031 Systems and methods for attenuation of noise and wakes produced by aircraft
01/16/2014WO2014008549A1 An aerolance system
01/15/2014EP2684797A1 Airplane wingtip device
01/14/2014US8628040 Aircraft configuration
01/02/2014DE102007027697B4 Wirbelgeneratoranordnung an der Triebwerksgondel eines Flugzeugs Vortex generator assembly to the engine nacelle of an aircraft
01/01/2014CN103482060A Turbulence device based on piezoelectric bimorph
01/01/2014CN103482055A Active control method and device for aerofoil drag reduction
12/2013
12/27/2013WO2013064768A3 Turbo engine attachment pylon
12/25/2013EP2676878A2 Swing tip assembly rotation joint
12/25/2013EP2675712A1 Aircraft with improved aerodynamic performance
12/25/2013CN103476675A Aircraft with improved aerodynamic performance
12/19/2013WO2013187830A1 Miniature vortex generator
12/11/2013CN103434641A Novel propeller utilizing Magnus effect
12/11/2013CN103434640A High-altitude unmanned plane equipped with Magnus effect propulsion system
12/10/2013US8602361 Laminar flow monitor
12/05/2013US20130320150 Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift
12/05/2013US20130320144 Aircraft landing gear
12/04/2013EP2669187A2 Method of coupling aerofoil surface structures and an aerofoil assembly
12/03/2013US8596568 Exhaust silencer with baffles
11/2013
11/28/2013US20130313360 Landing gear for an aircraft
11/28/2013US20130312857 Systems for modifying a fluid flow of a vehicle
11/26/2013CA2732100C System and method for aerodynamic flow control
11/21/2013US20130306788 Unmanned air system (uas)
11/21/2013US20130306177 Modification system for a vehicle in a fluid media
11/20/2013EP1892184B2 Active systems and methods for controlling an airfoil vortex
11/20/2013CN203294309U Electromagnetic air fluid decompression, propulsion and lifting device
11/19/2013US8585371 Wingtip device for the tip of a wing, blade of a wind generator or marine generator for reducing or even eliminating marginal swirl
11/19/2013US8584363 Method for making an acoustic panel for the air intake lip of a nacelle
11/16/2013CA2815846A1 An improved aircraft landing gear
11/14/2013US20130299643 Vortex Generation
11/14/2013US20130299002 Shock Wave Modification Method and System
11/14/2013DE102009001953B4 Vorrichtung zur Beeinflussung einer Überschall-Umströmung Device for influencing a supersonic flow around
11/13/2013EP2662282A2 Vortex generation
11/07/2013WO2012131335A3 Joint
11/07/2013US20130291979 Plasma-enhanced active laminar flow actuator system
11/06/2013EP2660149A2 Dielectric barrier discharge flight control system through modulated boundary layer transition
11/06/2013CN103381884A Dielectric barrier discharge flight control system through modulated boundary layer transition
11/02/2013CA2804729A1 Dielectric barrier discharge flight control system through modulated boundary layer transition
10/2013
10/24/2013US20130277504 Fixed wing of an aircraft
10/24/2013US20130277495 Device and method for increasing the aerodynamic lift of an aircraft
10/19/2013CA2802139A1 Continuous moldline technology (cmt) elastomeric control surface
10/17/2013US20130270392 Interface arrangement for aircraft lifting surface
10/17/2013US20130270391 Aircraft fuselage drag reduction blivet
10/16/2013CN101332870B Plasma actuator system and method for use with a weapons bay on a high speed mobile platform
10/10/2013WO2013151810A1 Multiple controllable airflow modification devices
10/03/2013US20130256460 Performance-enhancing winglet system and method
10/02/2013EP2644498A2 Performance-enhancing winglet system and method
10/02/2013EP2644497A1 Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift
10/02/2013CN203222109U 等离子体涡流发生器 Plasma vortex generators
10/01/2013US8544800 Integrated wingtip extensions for jet transport aircraft and other types of aircraft
09/2013
09/30/2013CA2800627A1 Performance-enhancing winglet system and method
09/26/2013WO2013014080A3 Method for retrofitting vortex generators on a wind turbine blade
09/24/2013CA2654772C A wind turbine blade and a pitch controlled wind turbine
09/18/2013CN103303469A Device for controlling flow separation caused by interference between high-Mach-number shock waves and boundary layers
09/17/2013US8534595 Shock wave modification method and system
09/12/2013DE102004034367B4 Betankungs-Pod eines Flugzeugs mit einer Ablenkvorrichtung Refueling pod of an aircraft with a deflector
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