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