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7367530 |
Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle...
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7357358 |
Aircraft leading edge device systems and corresponding sizing methods
Aircraft leading edge device systems and methods for sizing such systems are disclosed. In one embodiment, a spanwise lift coefficient distribution for an airfoil corresponding to at least one...
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7338018 |
Systems and methods for controlling aircraft flaps and spoilers
Systems and methods for controlling aircraft flaps and spoilers. Systems in accordance with some embodiments include a wing having a trailing edge, and a flap positioned proximate to the wing...
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7338011 |
Method making it possible to prevent vibration of a rudder of an aircraft and aircraft using this method
A method for preventing vibration of a rudder of an aircraft may have, on a lateral aerodynamic surface of the aircraft's rudder, a protruding aerodynamic element capable of generating an...
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7322547 |
Aerospace vehicle leading edge slat devices and corresponding methods
Aerospace vehicle leading edge slat devices and corresponding methods are generally disclosed herein. One aspect of the invention is directed toward an aerospace vehicle system that includes an...
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7309043 |
Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
Actuation device positioning systems and associated methods, including aircraft spoiler droop systems are generally disclosed herein. One aspect of the invention is directed toward a positioning...
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7300021 |
Aerospace vehicle fairing systems and associated methods
Aerospace vehicle fairing systems and associated methods, including fairings that house flap surface drive mechanisms on aircraft, are disclosed herein. One aspect of the invention is directed...
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7270305 |
Aircraft leading edge apparatuses and corresponding methods
Aircraft and leading edge apparatuses and corresponding methods are disclosed. In one embodiment, an aircraft system includes an airfoil with a leading edge device that is movable among a retracted...
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7264206 |
Leading edge flap apparatuses and associated methods
The present invention is directed generally toward leading edge flap apparatuses and corresponding methods. One aspect of the invention is directed toward an aircraft system having an airfoil, an...
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EP1314885B1 |
Flexible serrated trailing edge for wind turbine rotor blade
Abstract of EP1314885 A method for the improvement of wind turbine rotor efficiency blades of a wind turbine rotor with serrated trailing edges each having a plurality of span-wise, periodic...
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7243881 |
Multi-function trailing edge devices and associated methods
Trailing edge devices configured to carry out multiple functions, and associated methods of use and manufacture are disclosed. An external fluid flow body (e.g., an airfoil) configured in...
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7185859 |
***WITHDRAWN PATENT AS PER THE LATEST USPTO WITHDRAWN LIST*** Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle...
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7114685 |
Wing for an aircraft or spacecraft
The invention relates to a wing, a wing, a tail unit or grid fins for a flying object moving with supersonic speeds. The wing comprises leading edges and tailing edges. According to the invention,...
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7065957 |
Segmented mixing device for jet engines and aircraft
Disclosed is a means for reducing jet engine exhaust noise wherein mixing is enhanced between adjacent exhaust flows and between exhaust flow and free-stream flow. Also disclosed is a means for...
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7059833 |
Method for improvement of the efficiency of a wind turbine rotor
A method for the improvement of wind turbine rotor efficiency blades of a wind turbine rotor with serrated trailing edges each having a plurality of span-wise, periodic indentations, in the form of...
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7059563 |
Systems, apparatuses, and methods for moving aircraft control surfaces
Aircraft control surface operating systems and apparatuses, and associated methods of use. In one embodiment, an aircraft system includes an actuator operably coupled to a control surface in...
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6978971 |
Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
Methods and apparatuses for controlling airflow proximate to engine/airfoil systems are disclosed. In one embodiment, an aircraft system includes an airfoil and an engine unit at least proximate to...
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6939108 |
Cooling fan with reinforced blade
A circulatory device comprising a large diameter fan having reinforced fan blades with a tapered airfoil shape is disclosed. The fan blades may be formed using an extrusion method of fabrication,...
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6869050 |
Profiled wing unit of an aircraft
The deformation characteristic of a profiled aerodynamic aircraft component is improved by forming ridges ( 6, 7 ) in the top and bottom skin ( 4, 5 ) of the component. Two ridges ( 6, 7 ) form a...
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6830436 |
Wind turbine provided with nacelle
The blade structure of a wind turbine which has enough strength for sporadic large load and increased durability. The blade can be formed into a thinner blade profile, with which blade performance...
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6684802 |
Serrated leech flaps for sails
In an improved sail for a sailboat, the trailing edges of a pair of serrated flaps of sailcloth are attached to the trailing edge of the sail, one on each side; the leading portions of...
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6634309 |
Device for reducing the resistance to the advancement of a motorboat on water
A device for reducing the resistance to the advancement on water of a motorboat ( 1 ), including a keel ( 2 ), on the underside of which at least one step ( 3 ) is provided; projecting element ( 6...
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6592072 |
Spanwise tailoring of divergent trailing edge wings
A method for forming a transonic wing that segregates a baseline transonic wing into a plurality of airfoil segments that are collectively modified an optimized so as to tailor a spanwise variation...
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EP1314885A1 |
Flexible serrated trailing edge for wind turbine rotor blade
A method for the improvement of wind turbine rotor efficiency blades of a wind turbine rotor with serrated trailing edges each having a plurality of span-wise, periodic indentations, in the form a...
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6471157 |
Device and method for reducing aircraft noise
A noise abatement device that is positioned adjacent to a body. The noise abatement device generally includes tabs or cavities which thicken the shear layer created by fluid flow over, around, or...
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EP1112928A2 |
Airfoil with performance enhancing trailing edge
The aerofoil section has a suction side and a compression side when a flow passes round it. The trailing edge (2) diverges or is angled away from the rest of the section. The trailing edge has...
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6173924 |
Low density flexible edge transition
In accordance with the present invention, there is provided a structural transition system for use between an aerodynamic lifting member and an aerodynamic control device attached thereto. The...
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5901925 |
Serrated-planform lifting-surfaces
A novel set of serrated-planform lifting surfaces produce unexpectedly high lift coefficients at moderate to high angles-of-attack. Each serration, or tooth, is designed to shed a vortex. The...
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5533865 |
Wind turbine
In order to reduce the noise nuisance caused during operation by rotor blades of a rotor of a wind turbine the rear edge of each blade is irregularly formed. In particular the saw-tooth form with a...
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5492448 |
Rotary blades
A rotary blade includes a fixed boundary layer control device extending spanwise on a lower surface adjacent the trailing edge to improve the lift/thrust characteristics of the blade especially at...
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