| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 281 | AERODYNAMIC FEATURES OF PLASTIC GLAZING OF TAILGATES | PCT/IB2016/055332 | 2016-09-07 | WO2017042697A1 | 2017-03-16 | SCHELLEKENS, Geert Jan; TERRAGNI, Matteo |
A plastic glazing of a tailgate of a vehicle is provided, the plastic glazing comprising: a first translucent component comprising a full panel of the plastic glazing; a second translucent component molded onto the first translucent component, wherein the second translucent component is a colored thermoplastic polymer, wherein the plastic glazing is of one-piece molded plastic construction, wherein at least one of the first translucent component and the second translucent component comprises one or more aerodynamic features, wherein the one or more aerodynamic features are each configured to reduce one or more of: a turbulence, a drag force, and a lift force. |
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| 282 | A WIND TURBINE GENERATOR WITH EXTENDED BLADE SUPPORT | PCT/DK2009/050280 | 2009-10-27 | WO2010048959A2 | 2010-05-06 | SLOTH, Erik |
The present invention relates to a wind turbine generator with a hub that has a plurality of radially extending support structures, one radially extending support structure for each rotor blade, and a plurality of inclined support beams, one inclined support beam for each rotor blade, and/or a first peripheral support rod positioned in an exterior position on the hub, said first peripheral support rod connecting two of said radially extending support structures. The inclined support beams, and/or the first peripheral support rod have an airfoil shape providing aerodynamic lift upon wind engagement. This is advantageous for obtaining a wind turbine where the rotor blades resonances are controlled by designing and dimensioning the plurality of inclined support beams and the first peripheral support rod accordingly. At the same time the volume of the hub is utilized for increasing the aerodynamic lift while still facilitating a relatively strong structure of the hub. |
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| 283 | AN AIRWING STRUCTURE | PCT/US2002/000568 | 2002-01-09 | WO2003068596A2 | 2003-08-21 | YIM, James, H. |
The airwing structure according to the present invention comprises of an airfoil structure, a main frame, and a means for providing a downward and a forward tension on the airfoil structure. The airfoil structure further comprises of a leading edge, a trailing edge, a left edge, a right edge, a central wing root, and a plurality of chord lines. Moreover, the airfoil structure comprises of a substantially flexible surface skin and the airfoil structure also has a downward arc for producing lift by aerodynamic forces exerted thereon. The main frame attached to the airfoil structure comprises of a leading bar and a supporting bar. The leading bar is fixedly attached to the leading edge supporting and maintaining the leading edge from collapsing. The supporting bar is attached to the leading bar and attached to the trailing edge supporting and maintaining the airfoil structure from collapsing. |
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| 284 | WING ABLE TO ENHANCE LIFT BY INTERNAL AIR FLOW | PCT/HR2002/000049 | 2002-10-17 | WO2003039949A2 | 2003-05-15 | BOSATLIC, Dragutin |
Wing able to enhance lift power by inner air flow, is solution of wing that results in increased and changeable lift power, with lesser increase of aerodynamic resistance than with conventional wings. In the invention basic embodiment, the wing is provided with free aerodynamic air-flow through a specially designed tunnel (4) running from the opening below the wing front edge (5) to the wing exit edge (6). Turning of the blades (11) enables adjusting of angle of the air flow (13) exiting from the tunnel (4), and their synchronous turning with the gate (15) enables partial or complete closing of the tunnel (4) and turning of the wing into a l conventional wing with closed profile contour. The principle of this technical solution is applicable, with adequate adjustments, to glider-paraglider and kite wings, made of fabrics, and to wind-generator rotor wings. |
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| 285 | MAIN ROTOR SYSTEM FOR HELICOPTERS | PCT/US9504929 | 1995-04-24 | WO9529842A2 | 1995-11-09 | ARLTON PAUL E; ARLTON DAVID J |
| A high-lift main rotor system (1) is provided for a full-size or model helicopter (15). Main rotor system (1) includes rotor blades (100) and subrotor blades (84) for producing aerodynamic lift. The subrotor blades (84) act to augment control and stability of main rotor (1). Main rotor blades (100) are configured to include airfoiled cross sections (103-107) of varying shape and are mounted to a rotor hub (77) to fold within limits about a horizontal flapping axis (10). A linkage including swashplate (140) is provided for transmitting pilot control commands to the rotating rotor blades (100). | ||||||
| 286 | WIND TURBINE | PCT/AU1990000600 | 1990-12-19 | WO1991009225A1 | 1991-06-27 | THE UNIVERSITY OF MELBOURNE |
| A cross-flow wind turbine comprising a rotor mounted for rotation about a vertical axis and a plurality of blade assemblies mounted on the rotor. Each blade assembly comprises a blade (16) of aerofoil section mounted vertically for pivotal movement about a vertical shaft (12). The turbine also includes a device (18) for measuring the direction of the apparent fluid velocity, a shaft encoder for measuring the blade angle and a control system (22) to set the blade angle such that the lift component of the aerodynamic forces on the blade (16) contributes positively to the driving torque on the rotor. | ||||||
| 287 | Device and method for increasing the aerodynamic lift of an aircraft | US13855234 | 2013-04-02 | US09193444B2 | 2015-11-24 | Carsten Weber; Markus Fischer; Arne Grote; Rolf Radespiel; Martin Dreyer |
| A lift arrangement for an aircraft includes an aircraft fuselage section with an outside, an aerodynamic lift body attached to the aircraft fuselage section and extending from the aircraft fuselage section outwardly, and a pair of movably held add-on bodies arranged upstream of a leading edge of the aerodynamic lift body. The add-on bodies include an aerodynamically effective surface and are equipped with incoming airflow to generate vortices that impinge on the aerodynamic lift body, thus leading to an increase in lift on the aerodynamic lift body. Thus the lift generation on a lift body is effectively influenced, in particular to compensate for loss of lift as a result of icing. The add-on bodies are moveable, and, can be moved to a neutral position in which they do not project into the flow around the aircraft, and are thus not effective from the point of view of fluid dynamics. | ||||||
| 288 | Wind turbine with auxiliary fins | US13094237 | 2011-04-26 | US08308437B2 | 2012-11-13 | Bharat Bagepalli; Aniruddha D. Gadre; Nitin Narayan Bhate |
| A wind turbine includes a nacelle mounted atop a tower. Power generating components are housed within the nacelle. A rotor hub is rotationally coupled to the power generating components. A plurality of blades are fixed to the rotor hub. The blades include a root section extending radially outward from the rotor hub and an aerodynamic section extending radially outward from the root section, wherein lift is generated by the blades primarily along the aerodynamic section. Aerodynamic fins extend radially outward from the rotor hub alongside the root sections of the blades and have an aerodynamic shape so as to capture wind and impart rotational torque to the hub from a central impinging wind zone that is coaxial to the rotor hub and the blade root sections. | ||||||
| 289 | WIND TURBINE WITH AUXILIARY FINS | US13094237 | 2011-04-26 | US20120051916A1 | 2012-03-01 | Bharat Bagepalli; Aniruddha D. Gadre; Nitin Narayan Bhate |
| A wind turbine includes a nacelle mounted atop a tower. Power generating components are housed within the nacelle. A rotor hub is rotationally coupled to the power generating components. A plurality of blades are fixed to the rotor hub. The blades include a root section extending radially outward from the rotor hub and an aerodynamic section extending radially outward from the root section, wherein lift is generated by the blades primarily along the aerodynamic section. Aerodynamic fins extend radially outward from the rotor hub alongside the root sections of the blades and have an aerodynamic shape so as to capture wind and impart rotational torque to the hub from a central impinging wind zone that is coaxial to the rotor hub and the blade root sections. | ||||||
| 290 | Delta-wing aircraft | US3738595D | 1970-10-12 | US3738595A | 1973-06-12 | BOUCHNIK J |
| A delta-wing aircraft comprises a pair of auxiliary wings pivotably mounted forwardly of the leading edge of the delta-wing from a deployed position at lower speeds wherein they increase lift and also act as horizontal stabilizers, to a retracted dragdecreasing position at cruising speeds. In one described embodiment, the auxiliary wings are pivotable about a vertical axis of the aircraft from a deployed position wherein their leading edges are about 90* to the longitudinal axis of the aircraft, to a retracted position wherein they form the apex of the delta-wing; in both positions, the mean aerodynamic chord of the auxiliary wings is aligned with that of the delta-wing. In a second described embodiment, the pair of auxiliary wings are pivoted about a horizontal axis of the aircraft, from a deployed position substantially perpendicular to the longitudinal axis of the aircraft, to a retracted position substantially flush with the aircraft fuselage.
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| 291 | Method for altitude control and/or pitch angle control of airships, and an airship having a device for altitude control and/or pitch angle trimming | US09790792 | 2001-02-22 | US20020014555A1 | 2002-02-07 | Tim Smith |
| A method for altitude control of airships in all the speed ranges which occur during operation has the following features: a) above a predetermined upper speed threshold value, the altitude of the airship is essentially controlled by at least one elevator (5); b) in the range between the upper speed threshold value and a predetermined lower speed threshold value, the altitude of the airship is controlled by aerodynamic lift or downward force which can be varied independently of the airspeed and incidence angle and is produced by aerodynamic lifting bodies; and c) below the lower speed threshold value, the altitude of the airship is controlled by means of devices which produce vertically acting thrust. An airship which is suitable for carrying out the method has a fuselage, forward propulsion means and aerodynamic lifting bodies for producing aerodynamic lift bodies for producing aerodynamic lift which, above a lower threshold value of the airspeed, can be varied independently of said airspeed and independently of the incidence angle, and can be influenced by means of a control device. | ||||||
| 292 | Wind turbine blade with base part having inherent non-ideal twist | US13320977 | 2010-05-18 | US08899922B2 | 2014-12-02 | Peter Fuglsang; Stefano Bove; Lars Fuglsang |
| A blade for a rotor of a wind turbine is divided into a root region closest to the hub and an airfoil region with a lift generating profile furthest away from the hub. A transition region has a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region, and includes at least a first longitudinal segment extending along at least 20% of a longitudinal extent of the airfoil region. A base part has an inherent non-ideal twist, such as no twist, or a reduced twist compared to a target blade twist, so that an axial induction factor of the first base part at a design point deviates from a target axial induction factor. A number of flow altering devices are arranged so as to adjust the aerodynamic properties of the first longitudinal segment. | ||||||
| 293 | Hybrid hull for high speed water transport | US177328 | 1998-10-22 | US6058872A | 2000-05-09 | Robert G. Latorre |
| A catamaran-type boat having two or more demi-hulls that are connected by a wing-shaped superstructure is disclosed. The demi-hulls are further connected by two or more transverse hydrofoils. A tunnel is created between the demi-hulls and the superstructure. The shape of the superstructure takes advantage of the airflow through the tunnel to provide aerodynamic lift. The hydrofoils serve two purposes. The first is to provide hydrodynamic lift, and the second is to cancel wave build up between the hulls. The wave cancellation assists the stability of the craft by providing a relatively flat surface for the wing, to provide stable additional lift through the "wing in ground" effect. The combination of hydrodynamic lift, wave cancellation, and aerodynamic lift decreases the ship's drag and increases its speed. | ||||||
| 294 | Hybrid Flow Control Method for Simple Hinged Flap High-Lift System | US14955913 | 2015-12-01 | US20160280358A1 | 2016-09-29 | John C. Lin; Mehti Koklu |
| Systems, methods, and devices are provided that provide hybrid flow control for a simple hinged flap high-lift system using sweeping jet (SWJ) actuators for active flow control (AFC) and adaptive vortex generators (AVGs) that may be actuated by flap deflection for passive flow control (PFC). The various embodiments may significantly reduce mass flow, differential pressure, and power requirements for equivalent flow control performance when compared to using AFC only. The various embodiments may reduce the power requirement of AFC, while still maintaining the aerodynamic performance enhancement necessary for high-lift applications using a simple hinged flap. The various embodiments may provide the necessary lift enhancement for a simple hinged flap high-lift system, while keeping the pneumatic power requirement (mass flow and pressure) for the AFC within an aircraft's capability for system integration. | ||||||
| 295 | Methods and apparatus for aerodynamic and hydrodynamic drag reduction and attitude control for high speed boats | US11899543 | 2007-09-05 | US07543544B2 | 2009-06-09 | Loo T. Yap |
| The present invention provides methods and apparatus for reducing sinkage and wetted surface, and thus hydrodynamic drag of a high-speed boat through the generation of aerodynamic lift while decreasing overall aerodynamic drag. At least one lift-generating front wing proximate a bow section of the boat with at least one corresponding front air channel may be provided. At least one lift-generating rear wing proximate a transom section of the boat with at least one corresponding rear air channel may also be provided. At least one of the wings may be adjustable to generate aerodynamic lift with one of: (1) a neutral; (2) a transom-lifting; and (3) a bow-lifting pitching moment about a center of inertia of the boat. At least one wing proximate the leading edge of the tunnel of a multi-hull boat may be provided to increase the operational envelope. | ||||||
| 296 | WIND TURBINE BLADE WITH BASE PART HAVING INHERENT NON-IDEAL TWIST | US13320977 | 2010-05-18 | US20120063910A1 | 2012-03-15 | Peter Fuglsang; Stefano Bove; Lars Fuglsang |
| A blade for a rotor of a wind turbine is divided into a root region closest to the hub and an airfoil region with a lift generating profile furthest away from the hub. A transition region has a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region, and includes at least a first longitudinal segment extending along at least 20% of a longitudinal extent of the airfoil region. A base part has an inherent non-ideal twist, such as no twist, or a reduced twist compared to a target blade twist, so that an axial induction factor of the first base part at a design point deviates from a target axial induction factor. A number of flow altering devices are arranged so as to adjust the aerodynamic properties of the first longitudinal segment. | ||||||
| 297 | Airfoil | US39458173 | 1973-09-05 | US3860200A | 1975-01-14 | PETRUSHKA EDWARD M |
| An airfoil for an aircraft system is provided with a pair of airfoil-like primary fluid flow injectors that are rotatable relative to airfoil structure and to positions that develop aerodynamic lift in conventional flight and fluid-reaction lift in vertical/hovering/transitional flight. An actuator connected to the aft airfoil-like injector functions to selectively rotate such injector to positions whereat the injector trailing edge comprises a part of the airfoil cross-sectional profile associated with aircraft system attitude-stabilized flight, is positioned above such profile to reduce airfoil camber and associated aerodynamic lift, or is projected below such profile to define, in combination with the other airfoil-like injector, a lift ejector diffuser section.
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| 298 | Vehicle control device | JP2012063835 | 2012-03-21 | JP2013193596A | 2013-09-30 | ODAJIMA KENJI |
| PROBLEM TO BE SOLVED: To improve fuel consumption while securing travelling safety of a vehicle.SOLUTION: In a vehicle control device which is mounted in a vehicle and controls a movable aerodynamic member capable of vertically changing force transmitted to a vehicle by receiving traveling wind, when the occurrence of idle is not estimated (S2), a driving wheel is not actually idled (S3), a vehicle is not turned (S4) and a vehicle is not in a braking state (S5), since running safety of the vehicle is secured, ground contact pressure of a wheel is reduced to reduce rolling resistance by setting a movable aerodynamic member to cause lift in which force transmitted to the vehicle is directed upward. When a road surface condition is estimated not to be bad even though a driving wheel is actually idled (S7), when a side slip is prevented even during turning of the vehicle (S8), or when no slip by a wheel rock occurs during vehicle breaking (S9), running safety of the vehicle is secured, but slip or the like may be caused, so that the movable aerodynamic member is set to a neutral position in which force transmitted to the vehicle approaches to zero. | ||||||
| 299 | Aerodynamic noise suppressing structure of current collector, lift adjuster of current collector, and karman vortex reducing structure | JP2011259072 | 2011-11-28 | JP2013115897A | 2013-06-10 | KOYO TAKESHI; IKEDA MITSURU |
| PROBLEM TO BE SOLVED: To provide an aerodynamic noise suppressing structure of a current collector, a lift adjuster of the current collector, and a Karman vortex reducing structure, which lessen the strength of a Karman vortex to reduce aerodynamic sounds from a collector shoe, using a readily attachable and simple structure, and easily adjust a lift acting on the collector shoe.SOLUTION: When a collector shoe 7 moves in an Adirection, ribbons 9a and 9b of a disturbance giving portion 9 are exposed to an airflow F, thus they flutter in the airflow F. As a result, a separation shearing layer on a lower side, from which a Karman vortex Fis generated, interferes with the ribbons 9a. This consequently prevents the growth of the Karman vortex Fgenerated from the separation shearing layer on the lower side to lessen the strength of the Karman vortex F, thereby aerodynamic sounds are suppressed. At the same time, the Karman vortex Fgenerated in a wake of the collector shoe 7 interferes with the ribbons 9b to collapse the Karman vortex F. This reduces the strength of the Karman vortex Fgenerated from the separation shearing layer on the lower side, thereby the aerodynamic sounds are suppressed. | ||||||
| 300 | FLOW CONTROL ARRANGEMENT FOR A WIND TURBINE ROTOR BLADE | PCT/EP2017/058492 | 2017-04-10 | WO2018041420A1 | 2018-03-08 | AKAY, Busra; ENEVOLDSEN, Peder Bay; GONZALEZ, Alejandro Gomez; LAURSEN, Jesper Monrad; LOEVEN, Alex; SCHEURICH, Frank |
The invention relates to a rotor blade (20) for a wind turbine (10). The rotor blade (20) comprises an aerodynamic device (30) for influencing the airflow (61) flowing from the leading edge section (24) of the rotor blade (20) to the trailing edge section (23) of the rotor blade (20). The aerodynamic device (30) is mounted at a surface (28) of the rotor blade (20) and comprises a pneumatic or hydraulic actuator, such as a hose (31) or a cavity (32), of which the volume depends on the pressure of a fluid (62) being present inside the pneumatic or hydraulic actuator. The rotor blade (20) further comprises a control unit (51) for controlling the pressure of the fluid (62) in the hose (31) or the cavity (32) of the aerodynamic device (30). The aerodynamic device (30) is in a first configuration when no pressure application to the fluid (62) in the pneumatic or hydraulic actuator is induced by the control unit (51), and is in a second configuration when the control unit (51) induces the application of a positive or negative pressure to the fluid (62) in the pneumatic or hydraulic actuator. The rotor blade (20) is furthermore characterized in that its lift (71) in the first configuration is smaller than the lift (71) of the rotor blade (20) in the second configuration. Additionally, the invention relates to a wind turbine (10) for generating electricity comprising at least one such rotor blade (20). |
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