Patents
Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724)
01/2002
01/02/2002EP1167187A1 Surface quality enhancement of aerospace skin sheet
01/01/2002US6334753 Streamlined bodies with counter-flow fluid injection
12/2001
12/20/2001WO2001096178A1 Aerodynamic body comprising diffusor ducts between pressure and suction sides
12/13/2001DE10027938A1 Aerofoil section with lift-increasing trailing edge, in which trailing edge has spoilers on one or both sides to cause flow breakaway
12/05/2001EP1159533A1 Centrifugal air flow control
11/2001
11/28/2001EP1156962A2 Tangentially directed acoustic jet controlling boundary layers
11/08/2001DE10020177A1 Einrichtung zur Lärmminderung an Tragflügeln von Flugzeugen Means to reduce noise at wings of airplanes
10/2001
10/31/2001EP1149761A1 Noise damping device for aircraft wings
10/25/2001US20010032907 Noise reducing vortex generators on aircraft wing control surfaces
10/24/2001CN1319063A Load-bearing structure with reduced tip vortex
10/18/2001WO2001076934A1 Design of viscoelastic coatings to reduce turbulent friction drag
10/10/2001EP1141554A1 Electrostatic/pneumatic actuators for active surfaces
09/2001
09/11/2001US6288472 Electrostatic/pneumatic actuators for active surfaces
09/05/2001EP1019283B1 Leading edge high lift devices with laminar flow control
07/2001
07/19/2001DE19964114A1 Aerofoil section with lift-increasing trailing edge, in which trailing edge has spoilers on one or both sides to cause flow breakaway
07/18/2001EP1115613A1 Load-bearing structure with reduced tip vortex
07/04/2001EP1112928A2 Airfoil with performance enhancing trailing edge
06/2001
06/19/2001US6247670 Active flaperon assembly
05/2001
05/30/2001EP0852552B1 Aircraft with jet flap propulsion
04/2001
04/17/2001US6216982 Suction device for boundary layer control in an aircraft
04/10/2001US6215221 Electrostatic/pneumatic actuators for active surfaces
03/2001
03/28/2001EP0866920B1 Process for forming a surface for contact with a flowing fluid and body with such surface regions
03/20/2001US6203269 Centrifugal air flow control
03/20/2001US6202304 Method of making a perforated metal sheet
03/07/2001EP1081332A1 Axial flow turbines
03/07/2001EP1079935A1 Device for increasing the power of media flowing along a body at a high speed or a very fast moving body in a medium and use thereof as a high pressure nozzle
02/2001
02/27/2001US6193191 Modified surface for reducing the turbulences of a fluid and transportation process
02/22/2001WO2000055036A3 Tangentially directed acoustic jet controlling boundary layers
02/15/2001DE19938317A1 Coating for aeroplane or aircraft parts; has upper surface roughness that is sub-critical for laminar flow and reduces insect adhesion
01/2001
01/30/2001US6179251 Thin inlet lip design for low drag and reduced nacelle size
01/24/2001CN1061005C Ejector for aeroplane wing tip
01/23/2001US6176454 Apparatus for influencing the flow separation from a body immersed in the flow
01/04/2001WO2001000488A1 Laminar flow control system and suction panel for use therewith
01/04/2001CA2370647A1 Laminar flow control system and suction panel for use therewith
11/2000
11/28/2000US6152404 Apparatus for influencing a wing root airflow in an aircraft
11/23/2000WO2000070369A1 Device using a local irregularity to reduce the extent of the unwanted movements of weather balloons
10/2000
10/24/2000US6135395 Aircraft wing leading edge high lift device with suction
10/24/2000US6135238 Extended reaction acoustic liner for jet engines and the like
10/17/2000CA2083224C Method of and apparatus for controlling turbulence in a wall-bounded fluid flow field
10/12/2000DE19916145A1 Bearing wing for increasing lift and stabilizing flight ratio, consisting of thin-walled flow channels joined to each other and open at bottom
10/04/2000EP1040736A1 Synthetic jet actuators for cooling heated bodies and environments
10/03/2000US6126118 Flow separator reducer
09/2000
09/26/2000US6123296 Self-actuated flow control system
09/26/2000US6123145 Synthetic jet actuators for cooling heated bodies and environments
09/21/2000WO2000055036A2 Tangentially directed acoustic jet controlling boundary layers
09/05/2000US6113036 Boundary layer control system
08/2000
08/31/2000WO2000050779A1 Centrifugal air flow control
08/29/2000US6109565 Air craft wing
08/17/2000WO2000048206A1 Materials and composites activable into a state of enhanced conductivity
08/17/2000CA2362254A1 Materials and composites activable into a state of enhanced conductivity
08/16/2000EP0664757B1 Multiple electromagnetic tiles for boundary layer control
07/2000
07/25/2000US6092766 Process for forming a surface for contact with a flowing fluid and body with such surface regions
07/19/2000EP1019283A1 Leading edge high lift devices with laminar flow control
07/06/2000WO2000039467A1 Electrostatic/pneumatic actuators for active surfaces
07/04/2000US6082670 Method and arrangement for fluidborne vehicle propulsion and drag reduction
06/2000
06/27/2000US6079671 Passive porosity airfoil management device
05/2000
05/30/2000US6068328 Vehicular boundary layer control system and method
05/09/2000US6059236 Tangential force panel for active flow control of a conductive fluid
05/02/2000US6056204 Synthetic jet actuators for mixing applications
04/2000
04/18/2000US6050523 Leading edge construction for an aerodynamic surface and method of making the same
04/06/2000WO2000018641A1 Load-bearing structure with reduced tip vortex
04/06/2000CA2345334A1 Load-bearing structure with reduced tip vortex
03/2000
03/09/2000DE19840303A1 Micro turbulence generator system to reduce flow losses for motor vehicles consists of grained parts imprinted on self-adhesive foil for e.g. Formula 1 racing cars
03/07/2000US6033180 Rotor blade with a rotary spoiler
02/2000
02/22/2000US6027078 Method and apparatus using localized heating for laminar flow
02/02/2000CN1243485A Leading edge high lift devices with laminer flow control
12/1999
12/21/1999US6004095 Reduction of turbomachinery noise
11/1999
11/30/1999US5992792 Aircraft with jet flap propulsion
11/23/1999US5988568 Surface modification apparatus and method for decreasing the drag or retarding forces created by fluids flowing across a moving surface
11/23/1999US5988522 Synthetic jet actuators for modifiying the direction of fluid flows
11/18/1999WO1999058250A1 Device for increasing the power of media flowing along a body at a high speed or a very fast moving body in a medium and use thereof as a high pressure nozzle
11/18/1999DE19821449A1 High pressure jet nozzle to generate high pressure fluid jet
11/18/1999DE19820097A1 Anordnung zur Grenzschichtabsaugung und Stoßgrenzschichtkontrolle für ein Flugzeug Arrangement for the boundary layer and shock boundary layer control for an aircraft
11/18/1999CA2312425A1 Device for increasing the power of media flowing along a body at a high speed or a very fast moving body in a medium and use thereof as a high pressure nozzle
11/17/1999EP0865570A4 Noise suppression system for a jet engine
11/17/1999EP0646083B1 Electromagnetic device and method for boundary layer control
11/10/1999EP0955235A2 Boundary layer suction device for aircraft
11/02/1999US5975462 Integrated propulsion/lift/control system for aircraft and ship applications
10/1999
10/28/1999WO1999054199A1 Fluid flow control device using microelectromechanical (mems) valve means
10/26/1999US5971326 Surface for a wall subject to a turbulent flow showing a main direction of flow
10/12/1999US5964433 Staggered actuation of electromagnetic tiles for boundary layer control
09/1999
09/28/1999US5957413 Modifications of fluid flow about bodies and surfaces with synthetic jet actuators
09/10/1999WO1999044888A1 Method for producing a lift force and device for realising the same
09/01/1999EP0939028A2 Method and apparatus using localized heating for laminar flow
08/1999
08/31/1999US5944287 Ice protection for porous structure
08/24/1999US5941481 In an electrically conductive fluid
08/18/1999CN1044736C Method and apparatus for controlling turbulence in wall-bounded flow field
08/11/1999EP0934878A2 Low drag and reduced size aircraft engine nacelle
08/10/1999US5934611 Low drag inlet design using injected duct flow
08/04/1999CA2260668A1 Boundary layer control system
07/1999
07/13/1999US5923003 Extended reaction acoustic liner for jet engines and the like
06/1999
06/09/1999EP0921071A2 Noise suppression system for a jet engine
06/09/1999EP0920378A1 Drag reduction article
06/08/1999US5909782 For positioning transverse to a fluid flow
05/1999
05/27/1999WO1999026457A1 Synthetic jet actuators for cooling heated bodies and environments
05/11/1999US5901928 Active turbulence control technique for drag reduction
05/04/1999US5899416 Rudder assembly with a controlled boundary layer control for an aircraft
04/1999
04/29/1999WO1999020526A1 Engine inlet with blown air drag reduction
04/20/1999US5894990 Synthetic jet actuator and applications thereof
04/14/1999EP0788447A4 Movable sheet for laminar flow and deicing
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