Patents
Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724)
03/2004
03/25/2004WO2001096178A8 Aerodynamic body comprising diffusor ducts between pressure and suction sides
03/18/2004US20040050064 Method and system for regulating internal fluid flow within an enclosed or semi-enclosed environment
03/03/2004EP1392562A1 Aerofoil with gas discharge
03/02/2004US6698687 Aircraft wing heat exchanger apparatus and method
02/2004
02/05/2004US20040021041 Sparkjet actuator
01/2004
01/29/2004US20040016853 Method and apparatus for modulating flow separation
01/28/2004EP1384897A2 Method and apparatus for modulating flow separation
01/28/2004EP1384896A2 Method and apparatus for modulating airfoil lift
01/27/2004US6682022 Boundary layer control of aerodynamic airfoils
01/22/2004US20040011923 Efficient wings
01/22/2004US20040011917 Shock wave modification via shock induced ion doping
01/21/2004EP1382526A1 Aircraft noise reduction device
01/02/2004EP1373066A1 Turbulent flow drag reduction
01/02/2004EP0788447B1 Movable sheet for laminar flow and deicing
12/2003
12/31/2003WO2004001267A2 Method and system for regulating external and internal fluid flow
12/31/2003WO2004000642A1 Airship and method of operation
12/25/2003US20030234320 Airship and method of operation
12/24/2003WO2003106260A1 Controlling boundary layer fluid flow
12/11/2003WO2002064422A8 Recesses on a surface
12/04/2003WO2002072421A3 Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators
12/03/2003EP1365950A1 Recesses on a surface
12/02/2003US6655206 Device using a local irregularity to reduce the extent of unwanted movements of weather balloons
11/2003
11/27/2003US20030218102 Microfabricated translational stages for control of aerodynamic loading
11/26/2003EP1159533B1 Centrifugal air flow control
11/25/2003US6651935 Method and apparatus for control of shock/boundary-layer interactions
11/11/2003US6644598 Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators
10/2003
10/30/2003WO2003089295A2 Perforated skin structure for laminar-flow systems
10/23/2003WO2003087604A1 Solid body having a microstructured surface
10/21/2003US6636320 Fiber optic tufts for flow separation detection
10/07/2003US6629674 Method and apparatus for modulating airfoil lift
09/2003
09/23/2003US6622973 Movable surface plane
09/18/2003US20030173832 Linear electromagnetic zero net mass jet actuator
08/2003
08/19/2003US6607168 Bearing structure with reduced tip vortex
08/14/2003WO2003067169A2 “system and method using a flexible composite sheet for enhanced heat transfer and reduced flow drag”
08/14/2003US20030150962 Method for controlling and delaying the separation of flow from a solid surface by suction coupling (controlling separation by suction coupling, CSSC)
08/14/2003US20030150955 Aircraft wing heat exchanger apparatus and method
08/07/2003US20030145980 System and method for using a flexible composite surface for pressure-drop free heat transfer enhancement and flow drag reduction
08/06/2003EP1332547A1 Electrostatic/pneumatic actuators for active surfaces
07/2003
07/31/2003WO2002102613A3 Hybrid air boost vehicle and method for making same
06/2003
06/05/2003WO2003045778A1 Method and system for producing a potential over a body
06/05/2003CA2468536A1 Method and system for producing a potential over a body
05/2003
05/15/2003WO2003039949A2 Wing with lift enhancement by internal air flow
05/08/2003US20030085324 Boundary layer control of aerodynamic airfoils
05/07/2003EP1079935B1 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
04/2003
04/16/2003EP0737146B1 Supersonic natural laminar flow wing
03/2003
03/13/2003WO2003020584A1 Wing of flying object for flapping motion
02/2003
02/12/2003EP1283163A2 Device for reducing fluidic friction drag
02/11/2003US6516652 Design of viscoelastic coatings to reduce turbulent friction drag
02/06/2003WO2002038442A3 Microfabricated translational stages for control of aerodynamic loading
01/2003
01/22/2003EP1277655A1 Method for reducing the skin friction of a surface in a fluid stream
01/08/2003EP1272387A1 Design of viscoelastic coatings to reduce turbulent friction drag
01/03/2003WO2003000483A1 Body with improved surface properties
01/03/2003CA2456251A1 Body with improved surface properties
12/2002
12/27/2002WO2002102613A2 Hybrid air boost vehicle and method for making same
12/26/2002US20020195526 Method and apparatus for boundary layer reattachment using piezoelectric synthetic jet actuators
12/19/2002US20020190165 Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators
12/19/2002US20020190164 Method and apparatus for control of shock/boundary-layer interactions
12/18/2002EP1266824A1 Body, especially aircraft component, exposed to flow stream
12/10/2002US6491260 Noise reducing vortex generators on aircraft wing control surfaces
12/05/2002US20020179777 Movable surface plane
12/03/2002US6488238 Boundary layer control of aerodynamic airfoils
11/2002
11/26/2002US6484971 Control of flow separation and related phenomena on aerodynamic surfaces
11/21/2002WO2002092428A1 Aerofoil with gas discharge
11/21/2002DE10117300A1 Verfahren zur Reduzierung von Schwingungen in einem Hohlraum und überströmte Flächenanordnung Method for reducing vibrations in a cavity and flowed over surface arrangement
11/06/2002CN1377809A Resistance reducing device
10/2002
10/17/2002WO2002081303A1 Turbulent flow drag reduction
10/09/2002EP1247735A2 Method to reduce vibrations in cavities and surface arrangement in a fluid flow
10/02/2002DE10113130A1 Fuselage for an airplane comprises necking on its outer periphery consisting of a steeply falling step surface and a gradually rising surface in the direction of air flow
10/01/2002US6457654 Micromachined synthetic jet actuators and applications thereof
09/2002
09/26/2002US20020134891 Ejector pump flow control
09/19/2002WO2002072421A2 Modification of fluid flow about bodies and surfaces through virtual aero-shaping of airfoils with synthetic jet actuators
08/2002
08/28/2002EP0888497B1 System and method for diverting boundary layer air
08/22/2002WO2002064422A1 Recesses on a surface
08/22/2002DE10105442A1 Oberflächenstrukturen zur Verminderung des Strömungswiderstandes von Gasen, insbesondere des Luftwiderstandes von schnell bewegten Körpern und Gegenständen Surface structures for reducing the resistance to flow of gases, and in particular the aerodynamic drag of fast moving objects and objects
07/2002
07/30/2002US6425553 Piezoelectric actuators for circulation controlled rotorcraft
07/09/2002US6416289 Axial flow turbines
07/03/2002EP1219537A2 Control of flow separation and related phenomena on aerodynamic surfaces
07/03/2002EP0865570B1 Noise suppression system for a jet engine
06/2002
06/27/2002US20020079405 Control of flow separation and related phenomena on aerodynamic surfaces
06/26/2002CN1086664C Leading edge high left devices with laminer flow control
06/25/2002US6409126 Passive flow control of bluff body wake turbulence
05/2002
05/21/2002US6390418 Tangentially directed acoustic jet controlling boundary layer
05/21/2002US6390417 Drag control system for flying machine, process for estimating drag of flying machine, boundary layer control system, and boundary layer control process
05/21/2002US6390116 Large amplitude pneumatic oscillator
05/16/2002WO2002038442A2 Microfabricated translational stages for control of aerodynamic loading
05/16/2002DE10052022A1 Insert for shear layers and vortical structures comprises densely packed flexible smooth hair-like structures of textiles or synthetic fibers of specified diameter length and structural density.
05/10/2002WO2002037661A1 Electrostatic/pneumatic actuators for active surfaces
05/10/2002CA2427822A1 Electrostatic/pneumatic actuators for active surfaces
05/01/2002CN1083948C Method for controlling turbulence in boundary layer and other wall bounded fluid flow fields
04/2002
04/18/2002DE10028450A1 Reduction of aerodynamic resistance at an aircraft/glider uses a compressor to remove the boundary layer flow from the fuselage skin by suction, and pass the air mass to a fuel cell system to generate energy
04/10/2002EP0862532A4 Staggered actuation of electromagnetic tiles for boundary layer control
04/09/2002US6368059 Controlled passive porosity systems to mitigate cavitation
04/02/2002US6363972 Structure for reducing fluid resistivity on body
03/2002
03/28/2002WO2001096178B1 Aerodynamic body comprising diffusor ducts between pressure and suction sides
03/20/2002EP1187762A1 Laminar flow control system and suction panel for use therewith
03/19/2002US6358021 Electrostatic actuators for active surfaces
03/13/2002EP1185890A1 Device using a local irregularity to reduce the extent of the unwanted movements of weather balloons
02/2002
02/21/2002US20020021023 Hybrid air boost vehicle and method for making same
02/12/2002US6345791 Streamwise variable height riblets for reducing skin friction drag of surfaces
02/06/2002EP1177564A1 Materials and composites activable into a state of enhanced conductivity
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