Patents
Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724)
03/2015
03/05/2015DE102013109489A1 Strukturelement zur Ausbildung einer Oberfläche mit veränderbarer Luftdurchlässigkeit Structural element to form a surface with variable air permeability
03/04/2015EP2841338A1 Method of using an active flow control system for lift enhancement or destruction
03/03/2015US8967964 Boundary layer energiser
02/2015
02/26/2015DE102013013817A1 Strukturbauteil mit einer Ribletoberfläche Structural component with a Ribletoberfläche
02/19/2015DE102013013667A1 Vorrichtung zur Verstärkung der Leistung aerodynamischer Anlagen und Fluggeräte durch schwingende Saiten an Tragflächen und Rotorblätter. A device for amplifying the power plants and aircraft aerodynamic by vibrating strings to the wings and rotor blades.
02/11/2015CN103010459B 一种基于尾缘微穿孔降低前缘缝翼气动噪声的方法 Based on the trailing edge of a micro-perforated slats method for reducing the aerodynamic noise
02/11/2015CN102887223B 适用于尖后缘机翼的等离子体环量控制方法 Applicable to the trailing edge of the wing tip of the plasma ring volume control method
02/05/2015DE102008039061B4 Trennvorrichtung zur Vermeidung der Kontamination der Grenzschicht auf gepfeilten Tragflächen eines Flugkörpers durch den Rumpf oder ähnliche Körper Separator to avoid contamination of the boundary layer on swept wings of a missile through the torso or similar body
02/04/2015CN204137321U 吸盘式飞行器 Sucker-type aircraft
01/2015
01/27/2015US8941291 Plasma actuator
01/27/2015US8939410 Boundary layer flow disruptors for delaying transition to turbulent flow
01/27/2015CA2872375A1 Profiled element for generating a force
01/21/2015EP2826708A2 Wind turbine rotor blade assembly with surface features
01/21/2015CN104290923A 高速运动物体表面凹坑凹槽技术增效方法 Fast moving objects notch technical efficiency method of surface pits
01/13/2015US8931518 Shaping a fluid cavity of a flow control actuator for creation of desired waveform characteristics
01/07/2015EP2821342A1 Flow control structure and associated method for controlling attachment with a control surface
01/06/2015US8925870 Morphing wing leading edge
01/03/2015CA2852507A1 Flow control structure and associated method for controlling attachment with a control surface
12/2014
12/10/2014CN104192302A 基于绕尖头冯卡门曲线回转体基准流场的乘波体设计方法 Waverider design methods around the tip of the rotator von Karman curve based on the reference flow field
12/10/2014CN104191726A 刚性带尖端拉条 With the tip of the rigid brace
12/10/2014CN102642613B 波纹套低阻整流罩 Bellows low resistance fairing
11/2014
11/25/2014US8894019 Method of using microjet actuators for the control of flow separation and distortion
11/13/2014US20140332631 Amorphous metal riblets
11/11/2014US8882049 Airfoil system for cruising flight
11/06/2014US20140326834 Laminar Flow Panel
11/04/2014US8876064 Oscillatory vorticity generator and applications thereof
11/04/2014US8876052 Structurally designed aerodynamic riblets
10/2014
10/28/2014US8870275 Active and passive boundary layer control for vehicle drag reduction
10/28/2014US8870124 Application of elastomeric vortex generators
10/28/2014US8869725 Method and system for sensor-based intelligent sails
10/21/2014US8864082 Device for reducing the aerodynamic drag of a leading surface of an aircraft
10/21/2014US8864078 Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
10/14/2014US8857767 De-icing system for an aircraft
10/09/2014WO2014165106A1 Fibrillar structures to reduce viscous drag on aerodynamic and hydrodynamic wall surfaces
09/2014
09/30/2014US8844571 Fluid actuator for producing a pulsed outlet flow in the flow around an aerodynamic body, and discharge device and aerodynamic body equipped therewith
09/25/2014US20140284430 Synchronization of fluidic actuators
09/25/2014US20140283921 Airplane
09/18/2014WO2014140589A1 Cavity acoustic tones suppression
09/17/2014EP2778044A1 Cavity acoustic tones suppression
09/10/2014EP2773557A2 Turbo engine attachment pylon
09/09/2014US8827212 Method and apparatus for supplying a gas jet over an aerodynamic structure
09/09/2014US8827201 Rotorcraft structural element for reducing aerodynamic drag
09/09/2014CA2744753C Amorphous metal riblets
09/04/2014US20140248469 Rigid Tipped Riblets
09/03/2014EP2771239A1 Synchronization of fluidic actuators
08/2014
08/28/2014WO2014131055A1 Method and apparatus for providing high control authority atmospheric plasma
08/27/2014EP2769912A1 Vortex generating apparatus and method
08/26/2014CA2632873C Method of de-icing the leading edge of an aerodynamic surface and aircraft implementing such a method
08/21/2014US20140233769 Diaphragm arrangement for generating sound
08/12/2014US8800915 Device for boundary layer suction and composite component therefor
08/07/2014US20140217240 Vortex generating apparatus and vortex generating method
08/05/2014US8794574 Micro-array surface for passive drag modification
07/2014
07/30/2014CN203740128U 乘波体飞行器 Waverider body aircraft
07/22/2014US8783624 Laminar flow panel
07/22/2014US8783337 System for changing the convective heat transfer coefficient for a surface
07/22/2014CA2745622C Shape memory riblets
07/09/2014CN103917444A 涡轮发动机的连接吊架 Turbine engine hanger connection
07/08/2014CA2563572C Boundary layer control for an aircraft component
07/03/2014US20140182695 Method of Using Microjet Actuators For The Control Of Flow Separation And Distortion
06/2014
06/26/2014WO2014096255A1 Layer for reducing fluid resistance
06/26/2014US20140174642 Elastomeric riblets
06/26/2014DE102013020830A1 Fluid dynamic profile e.g. rotor blade for wind turbine, has suction and pressure sides, which are formed with projections and/or depressions, where flow resistance of suction side is lower than that of pressure side
06/24/2014US8757556 Aerodynamic body, regulating flap or main wing or fin of an aircraft as well as a structural component with such an aerodynamic body
06/19/2014WO2014092601A1 Streamlined surface
06/10/2014US8746624 Boundary layer control system and methods thereof
05/2014
05/28/2014CA2829743A1 High heat transfer rate reusable thermal protection system
05/15/2014DE102013102181B3 Strömungskörper mit reibungsarmer Oberflächenstruktur und Verfahren zur Modifizierung der Oberfläche eines Strömungskörpers Flow body with low-friction surface structure and method for modifying the surface of a flow body
05/14/2014EP2729363A2 Method for producing a surface of a component, said surface having reduced drag and component with reduced drag
05/07/2014CN103770935A 乘波体外形设计方法 Waverider body shape design method
04/2014
04/30/2014EP2724933A1 Fluidic traverse actuator
04/27/2014CA2823943A1 Fluidic traverse actuator
04/23/2014EP2722275A2 Externally driven flow control actuator
04/23/2014EP2722274A2 Flow control actuator with an adjustable frequency
04/23/2014CN101415605B Lift augmentation system and associated method
04/22/2014US8702042 Flow body, in particular for aircraft
04/16/2014CA2821470A1 Externally driven flow control actuator
04/10/2014US20140099475 Shape memory riblets
04/08/2014US8690107 High-lift system for an aircraft
04/08/2014US8690106 Ejector driven flow control for reducing velocity deficit profile downstream of an aerodynamic body
04/03/2014WO2014049328A1 Airflow modification patch and method
04/03/2014US20140091180 Systems and Methods for Attenuation of Noise and Wakes Produced by Aircraft
04/01/2014US8684310 Rigid tipped riblets
03/2014
03/26/2014CN203497174U Flexible strip-shaped plasma exciter
03/26/2014CN101998920B Flow element, and high-lift system comprising such a flow element
03/25/2014US8678316 Amorphous metal riblets
03/13/2014WO2014037857A1 Panel for controlling the aerodynamic phenomena on a body
03/12/2014CN103625639A Method for controlling noises of leading edge slat of airplane
03/11/2014US8668166 Shape memory riblets
03/06/2014US20140061387 Surface element for an aircraft, aircraft and method for improving high-lift generation on a surface element
02/2014
02/27/2014DE102007014226B4 Verfahren und Vorrichtung zur Homogenisierung einer Einlaufströmung in einen fächerförmigen Einlauf mit einem flachen Eingangsquerschnitt Method and apparatus for homogenizing an inlet flow in a fan-shaped spout with a shallow inlet section
02/25/2014US8657238 Retractable vortex generator for reducing stall speed
02/25/2014US8657237 Flying object for transonic or supersonic velocities
02/25/2014US8656957 Vortex generators to control boundary layer interactions
02/20/2014WO2014026246A1 Improved wing configuration
02/13/2014WO2014023951A1 Aircraft wing with system establishing a laminar boundary layer flow
02/11/2014CA2563571C Aircraft with a fluid-duct-system
02/05/2014CN103552684A Interplane air grid system based large angle-of-attack flying airflow separation control apparatus
02/04/2014US8640986 Turbojet nacelle and method for controlling separation in a turbojet nacelle
01/2014
01/30/2014WO2014016326A1 Wind turbine blade having a shaped stall fence or flow diverter
01/26/2014CA2815926A1 Aerodynamic, blunt aft body
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