Patents
Patents for B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for (1,943)
01/2009
01/08/2009WO2009005895A2 Method and apparatus for multibarrier plasma actuated high performance flow control
01/07/2009EP2010429A1 Inlet distortion and recovery control system
12/2008
12/31/2008CN101332871A Airfoil trailing edge plasma flow control apparatus and method
12/25/2008US20080315012 Method and System for Regulating Internal Fluid Flow Within an Enclosed or Semi-enclosed Environment
12/24/2008WO2008155566A1 Winglet
12/24/2008EP2004484A2 Aircraft with aerodynamic lift generating device
12/24/2008CA2691233A1 Winglet
12/18/2008WO2008151843A1 Engine nacelle of an aircraft comprising a vortex generator arrangement
12/18/2008US20080308683 Controllable winglets
12/18/2008DE10302514B4 Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts Fluidically effective area of ​​a moving fluid in a device, in particular an aircraft, in particular wing of an aircraft
12/18/2008DE102007027697A1 Eddy generator arrangement for use at engine nacelle of aircraft, has eddy generators provided at side of engine nacelle at mutual distance from each other with respect to circumferential or longitudinal direction of engine nacelle
12/17/2008CN101326100A Rudder of a commercial aircraft
12/11/2008WO2008108881A3 Method and apparatus for mitigating trailing vortex wakes of lifting or thrust generating bodies
12/10/2008EP1999014A2 Systems and methods for destabilizing an airfoil vortex
12/10/2008CN101318554A Plasma flow control actuator system and method
12/04/2008WO2008105861A3 System and method for deforming surfaces
12/04/2008US20080296438 Control surface actuation system
12/04/2008DE102007004746A1 Aerodynamic propulsion system for aircraft, has aerodynamic lifting body, e.g. wing, which is fastened in enclosing channel and produces pressure of gas
11/2008
11/26/2008EP1995173A1 Plasma flow control actuator system and method
11/19/2008CN101306723A Process and device for changing air resistance of moving objects
11/13/2008WO2008136698A1 Method and apparatus for an efficient electrohydrodynamic flow control of a gas
11/12/2008CN101304918A Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
11/06/2008WO2008134193A1 Deployable flap edge fence
11/06/2008US20080272615 Airflow control devices based on active materials
11/05/2008EP1988266A2 Nacelle assembly having inlet airfoil for a gas turbine engine
11/05/2008EP1986912A2 Aerodynamic flap of an aircraft with a device which influences the flap turbulence
11/05/2008CN101300170A Brake flap for an aircraft
11/04/2008CA2163967C Method and apparatus for glow discharge plasma treatment of polymer materials at atmospheric pressure
10/2008
10/30/2008US20080265101 Vortex ring generator
10/29/2008CN101296842A Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
10/22/2008CN100427359C Apparatus and method for the control of trailing wake flows
10/07/2008US7431244 Device for the generation of eddies and method for operating of said device
10/02/2008US20080237395 Bvi noise reduction method and apparatus for helicopter
09/2008
09/30/2008US7429074 Airflow control devices based on active materials
09/30/2008US7429018 Variable fluid intake with ramp and inflatable bag
09/30/2008CA2372166C Aircraft wing and fuselage contours
09/25/2008WO2008037865B1 Vertical take-off and landing vehicle which does not have a rotary wing
09/24/2008CN101272950A Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
09/18/2008US20080223991 Wing Tip Device
09/12/2008WO2008108881A2 Method and apparatus for mitigating trailing vortex wakes of lifting or thrust generating bodies
09/12/2008WO2008051293A3 A translating active gurney flap to alleviate aircraft wake vortex hazard
09/12/2008WO2008051269B1 Systems and methods for destabilizing an airfoil vortex
09/11/2008US20080217485 Smart Vortex Generator, and Aircraft, Vessel, and Rotary Machine Being Equipped with the Same
09/11/2008US20080217484 Brake flap for an aircraft
09/10/2008CN101263052A Wing tip device
09/03/2008CN101258071A An element for generating a fluid dynamic force
09/02/2008US7421319 Systems and methods for preflight planning and inflight execution using portable electronic data storage and display devices
08/2008
08/28/2008US20080203233 Flueted aircraft wing
08/28/2008DE102007007709A1 Aircraft, particularly rocket or missile, has closed bodyshell, where number of recesses are formed in bodyshell
08/27/2008EP1960262A1 Rudder of a commercial aircraft
08/26/2008US7416155 Canard position and dihedral for boom reduction and pitch/directional control
08/21/2008WO2008100286A2 Apparatus and method for use on aircraft with spanwise flow inhibitors
08/14/2008US20080191099 Concept of a Variable Winglet for Lateral Load Reduction for Combined Lateral and Vertical Load Reduction, and for Improving the Performance of Means of Locomotion
08/12/2008CA2325763C Procedure to reduce the pressure and temperature on the front of a missile at ultrasonic speed
08/06/2008EP1951567A2 Roof and floor flows
08/05/2008US7407131 Method for creating an aeronautic sound shield having gas distributors arranged on the engines, wings, and nose of an aircraft
07/2008
07/30/2008EP1948504A1 Brake flap for an aircraft
07/30/2008CN101229822A Moving device
07/24/2008WO2008051269A3 Systems and methods for destabilizing an airfoil vortex
07/24/2008DE202008004531U1 Von Fluid umströmte Oberfläche eines Flug- oder Strömungskörpers Of fluid flow around an aircraft or surface flow body
07/23/2008EP1945502A1 Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations
07/23/2008CN101228067A Integrated wingtip extensions for jet transport aircraft and other types of aircraft
07/23/2008CN101224790A Aerocraft equipped with airstream channel
07/22/2008CA2358115C Electrostatic/pneumatic actuators for active surfaces
07/17/2008DE202007014781U1 Ablenkvorflügel Ablenkvorflügel
07/08/2008CA2372295C Passively driven acoustic jet controlling boundary layers
07/03/2008WO2008058011A3 Methods and apparatus for reducing drag via a plasma actuator
07/02/2008EP1937553A1 Device for controlling a vortex trail generated by the oblong element of an aircraft bearing surface
07/02/2008EP1937552A2 Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft
07/02/2008CN101213131A Retractable vortex generator
06/2008
06/25/2008EP1934090A1 Integrated wingtip extensions for jet transport aircraft and other types of aircraft
06/18/2008EP1931563A1 Drag-reduction, propulsion, and lift generating system
06/18/2008EP1720765B1 Apparatus and method for the control of trailing wake flows
06/17/2008US7389161 Aeronautical navigation plotting instrument
06/11/2008EP1721082B1 Cladding comprising an integrated polymer actuator for the deformation of said cladding
06/11/2008CN101195348A Fluid motion device for accelerating and energy-saving
06/10/2008CA2364319C Vibration-driven acoustic jet controlling boundary layer separation
06/10/2008CA2361824C Tangentially directed acoustic jet controlling boundary layers
05/2008
05/29/2008WO2008064104A2 Systems and methods for reducing drag and/or vortex induced vibration
05/29/2008WO2008064102A2 Systems and methods for reducing drag and/or vortex induced vibration
05/29/2008WO2008061739A1 Wing tip shape for a wing, in particular of aircraft
05/29/2008DE102006061709B3 Missile e.g. guided missile, for use with aircraft or combat aircraft, has aero-spike that extends from front face surface, where aero-spike has front body i.e. aero-disk, formed with porous material, whose open pores form flow channels
05/29/2008CA2669604A1 Wing tip shape for a wing, in particular of aircraft
05/28/2008EP1926353A1 Over-wing travelling-wave axial flow plasma accelerator
05/28/2008EP1924493A1 Wing tip device
05/28/2008CN100390407C Rotor blade of wind turbine
05/22/2008WO2008058368A1 Nacelle drag reduction device for a turbofan gas turbine engine
05/22/2008US20080116322 System And Method For Reducing Airfoil Vortices
05/22/2008CA2666190A1 Nacelle drag reduction device for a turbofan gas turbine engine
05/15/2008CA2668450A1 Methods and apparatus for reducing drag via a plasma actuator
05/14/2008EP1921329A1 Aerodynamic noise reducing method (variants) and low-noise structural element for operating in a fluid medium flow
05/14/2008CN101180210A Concept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion
05/08/2008WO2008031620A3 Aerodynamic body and carrier wing comprising an aerodynamic body, actuating drive control module, computer, computer program, and method for influencing post-turbulences
05/07/2008EP1478569A4 Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom
05/02/2008WO2008051293A2 A translating active gurney flap to alleviate aircraft wake vortex hazard
05/02/2008WO2008051269A2 Systems and methods for destabilizing an airfoil vortex
04/2008
04/24/2008WO2008048131A1 Wing tip of an aircraft and swirl generators therefor
04/15/2008US7357351 Linear shock wave absorber
04/15/2008CA2498834C Rotor blade for a wind turbine
04/15/2008CA2344950C Noise reducing vortex generators on aircraft wing control surfaces
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