| Patents for B64C 23 - Influencing air-flow over aircraft surfaces, not otherwise provided for (1,943) |
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| 09/04/2001 | US6283407 Fuselage nose for controlling aerodynamic vehicles and method of utilizing same |
| 09/04/2001 | US6283406 Use of flow injection and extraction to control blade vortex interaction and high speed impulsive noise in helicopters |
| 08/21/2001 | US6276636 Gas or fluid de-organizers for moving objects |
| 08/16/2001 | WO2001058754A1 Passive aerodynamic sonic boom suppression for supersonic aircraft |
| 08/16/2001 | CA2398528A1 Passive aerodynamic sonic boom suppression for supersonic aircraft |
| 08/14/2001 | US6273371 Method for interfacing a pilot with the aerodynamic state of the surfaces of an aircraft and body interface to carry out this method |
| 08/02/2001 | WO2001054975A2 Vortex generation for control of the air flow along the surface of an airfoil |
| 07/31/2001 | US6267331 Airfoil with dynamic stall control by oscillatory forcing |
| 07/19/2001 | DE19964114A1 Aerofoil section with lift-increasing trailing edge, in which trailing edge has spoilers on one or both sides to cause flow breakaway |
| 07/18/2001 | EP1115613A1 Load-bearing structure with reduced tip vortex |
| 07/18/2001 | EP1115612A2 Ion doping apparatus and method for aerodynamic flow control |
| 07/04/2001 | EP1112928A2 Airfoil with performance enhancing trailing edge |
| 07/04/2001 | EP1112927A1 Aircraft lift arrangement |
| 06/19/2001 | US6247671 Ion doping apparatus and method for aerodynamic flow control |
| 06/06/2001 | EP1104741A1 Aircraft lift arrangement |
| 05/23/2001 | DE19953701A1 Pressure and temperature reducing process for supersonic flight, involving use of spike with spherical, elliptical or teardrop tip |
| 05/22/2001 | US6234751 Oscillating air jets for reducing HSI noise |
| 05/15/2001 | US6231004 Fluid dynamic lift generation |
| 05/10/2001 | DE19950403A1 Verfahren zum und Flugzeug mit Mitteln zum Reduzieren der Wirbelstärke des Flügelhauptwirbelpaars A method for aircraft and with means for reducing the vorticity of the vortex pair main wing |
| 04/24/2001 | US6220549 Method and apparatus for fabricating panels used for the active control of surface drag |
| 04/18/2001 | EP1091870A1 Spiral cylindrical wing tip |
| 04/11/2001 | EP1090835A1 Surface actuator for deforming an elastic plate structure |
| 04/10/2001 | US6215221 Electrostatic/pneumatic actuators for active surfaces |
| 04/04/2001 | CN1064016C Weak ground effect flying vehicle |
| 03/20/2001 | US6202304 Method of making a perforated metal sheet |
| 03/13/2001 | US6199795 Twin engine aircraft |
| 03/08/2001 | WO1999000297A8 Active system for early destruction of trailing vortices |
| 02/22/2001 | WO2000055036A3 Tangentially directed acoustic jet controlling boundary layers |
| 02/13/2001 | US6186445 Method and apparatus for mitigating junction flows |
| 02/13/2001 | US6186412 Generating dynamically controllable oscillatory fluid flow |
| 01/25/2001 | WO2001006134A1 System and method for manipulating and controlling fluid flow over a surface |
| 01/24/2001 | CN1061005C Ejector for aeroplane wing tip |
| 01/23/2001 | US6176454 Apparatus for influencing the flow separation from a body immersed in the flow |
| 01/18/2001 | DE10012253A1 Air and/or water craft, with bow bulge able to be turned about axis parallel to longitudinal axis of craft's hull or fuselage |
| 01/09/2001 | US6170780 Twin engine aircraft |
| 01/04/2001 | DE19926832A1 Subsonic aircraft with swept-back wings, with streamlined rotation body consisting of at least two rotating segments at each wingtip |
| 01/03/2001 | EP0828618A4 Method and apparatus for cleaning surfaces with a glow discharge plasma at one atmosphere of pressure |
| 12/28/2000 | DE19926047A1 Helicopter airframe with tail boom and rotor shapes boom asymmetric to main boom and rotor stream impact aided by extensible sheets or boom skin-spiralling coils. |
| 12/19/2000 | US6161802 Trapped vortex airfoil nose |
| 12/19/2000 | US6161797 Method and apparatus for reducing airplane noise |
| 11/28/2000 | US6152404 Apparatus for influencing a wing root airflow in an aircraft |
| 11/23/2000 | WO2000055035B1 Aircraft wing and fuselage contours |
| 11/21/2000 | US6149101 Aircraft wing and fuselage contours |
| 11/14/2000 | US6146724 A laminate comprising a silicon oxide barrier layer, forming a container, such that the barrier layer is on the interior of the container; gas impermeability, resists impact, and resists abrasion |
| 11/07/2000 | US6142425 Apparatus and method for aerodynamic blowing control using smart materials |
| 10/31/2000 | US6138955 Vortical lift control over a highly swept wing |
| 10/17/2000 | US6131853 Micro-drag generators for aerodynamic and hydrodynamic braking and control |
| 10/10/2000 | US6128896 Aircraft air conditioner energy recovery device |
| 10/03/2000 | US6126118 Flow separator reducer |
| 09/21/2000 | WO2000055036A2 Tangentially directed acoustic jet controlling boundary layers |
| 09/21/2000 | WO2000055035A1 Aircraft wing and fuselage contours |
| 09/14/2000 | DE19909190A1 Aircraft air eddies also generate a break eddy between the wing tip and fuselage in an opposite twist to the main air eddy from the wings to merge them together to break down the main eddy behind the aircraft |
| 09/12/2000 | US6116015 Breather outlet |
| 08/31/2000 | WO2000050778A1 Vibration-driven acoustic jet controlling boundary layer separation |
| 08/31/2000 | WO2000050302A1 Passively driven acoustic jet controlling boundary layers |
| 08/31/2000 | DE19908223A1 Airfoil for aircraft |
| 08/29/2000 | US6109566 Vibration-driven acoustic jet controlling boundary layer separation |
| 08/24/2000 | WO2000020274A9 Ion doping apparatus and method for aerodynamic flow control |
| 08/22/2000 | US6105904 Deployable flow control device |
| 08/16/2000 | EP0664757B1 Multiple electromagnetic tiles for boundary layer control |
| 08/15/2000 | US6102328 Method for reducing wave resistance in airplane |
| 07/25/2000 | US6092990 Oscillating air jets for helicopter rotor aerodynamic control and BVI noise reduction |
| 07/18/2000 | US6089504 Single engine aircraft |
| 07/18/2000 | US6089502 Blunt-leading-edge raked wingtips |
| 07/13/2000 | WO2000020274A3 Ion doping apparatus and method for aerodynamic flow control |
| 07/13/2000 | WO2000009392A8 Twin engine aircraft |
| 07/06/2000 | WO2000039467A1 Electrostatic/pneumatic actuators for active surfaces |
| 07/04/2000 | US6082679 Active system for early destruction of trailing vortices |
| 07/04/2000 | US6082670 Method and arrangement for fluidborne vehicle propulsion and drag reduction |
| 06/15/2000 | WO2000001576A3 A device for generating an aerodynamic force by differentially accelerating the fluid in the two sides of a surface |
| 05/25/2000 | DE19854741C1 Flow modifier for aircraft wing has wedge shaped flow body mounted directly on underside of wing |
| 05/18/2000 | WO2000009392A3 Twin engine aircraft |
| 05/11/2000 | DE19850319A1 Flugzeugflügel mit stark gepfeilter Flügelvorderkante, insbesondere Deltaflügel Airplane wing with pronounced V wing leading edge, in particular delta wing |
| 05/10/2000 | EP0999126A2 Aircraft wing with high swept back leading edge, particulary delta wing |
| 05/10/2000 | CN1052201C Object with stromline profile, aspecially stabilizing foil in ship |
| 05/04/2000 | WO2000024633A1 Supersonic aeroplane with low engine burn and operating method |
| 05/02/2000 | US6056238 Supersonic ground vehicle |
| 04/26/2000 | EP0995675A2 Method for reducing wave resistance in airplane |
| 04/18/2000 | US6050527 Flow control device to eliminate cavity resonance |
| 04/13/2000 | WO2000020274A2 Ion doping apparatus and method for aerodynamic flow control |
| 04/13/2000 | WO2000002775A3 Device for reducing the vortex trail of a high-lift wing and variants |
| 04/13/2000 | CA2345260A1 Ion doping apparatus and method for aerodynamic flow control |
| 04/06/2000 | WO2000018641A1 Load-bearing structure with reduced tip vortex |
| 04/06/2000 | CA2345334A1 Load-bearing structure with reduced tip vortex |
| 04/04/2000 | US6045088 Aircraft air conditioning energy recovery device |
| 03/29/2000 | EP0988225A1 Blunt-leading-edge raked wingtips |
| 03/28/2000 | US6042059 System and method of vortex wake control using vortex leveraging |
| 03/23/2000 | WO2000015961A1 Wind turbine blade with vortex generator |
| 03/16/2000 | WO2000001580B1 Spiral cylindrical wing tip |
| 03/09/2000 | WO2000012382A1 Twin engine aircraft |
| 03/02/2000 | DE19837800A1 Rumpfnase zur Steuerung von Fluggeräten Fuselage nose for the control of aircraft |
| 02/24/2000 | WO2000009392A2 Twin engine aircraft |
| 02/23/2000 | EP0980823A2 Fuselage nose for aircraft flight control |
| 02/15/2000 | US6024119 Flow control system having actuated elastomeric membrane |
| 01/26/2000 | EP0974515A2 Aircraft airconditioning energy recovery device |
| 01/25/2000 | US6016992 STOL aircraft |
| 01/20/2000 | WO2000002775A2 Device for reducing the vortex trail of a high-lift wing and variants |
| 01/13/2000 | WO2000001580A1 Spiral cylindrical wing tip |
| 01/13/2000 | WO2000001579A1 Aerofoil having shock control |
| 01/13/2000 | WO2000001578A1 Aerofoil having improved buffet performance |