• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention describes a device for reducing aerodynamic resistance in vehicles, comprising at least one panel (2) intended to be fixed to at least one edge (a) of the rear side (lt) of said vehicle, and where at least the profile of the outer surface (2e) of said panel (2) has a curved shape optimized to reduce the aerodynamic drag of the vehicle (100). For example, the curved shape can be obtained by applying a parametric study accompanied by numerical simulations that use the turbulent iddes model. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2651902A1
    申请号:ES201631052
    申请日:2016-07-29
    公开日:2018-01-30
    发明作者:Cándido GUTIÉRREZ MONTES；Javier RUIZ RUS；Rocío BOLAÑOS JIMÉNEZ；Carlos MARTÍNEZ BAZÁN；José Ignacio JIMÉNEZ GONZÁLEZ；Manuel LORITE DÍEZ；José Carlos CANO LOZANO
    申请人:Universidad de Jaen；
    IPC主号:
    专利说明:

    Device to reduce aerodynamic drag on land vehicles OBJECT OF THE INVENTION
    The present invention belongs in a general way to the automotive field, and more specifically to the devices used to reduce aerodynamic drag in land vehicles.
    The object of the present invention is a novel device designed to be installed on the rear side of a land vehicle, such as a truck or a bus, for the purpose of significantly reducing aerodynamic drag. BACKGROUND OF THE INVENTION
    The opposition to the advance of a vehicle is mainly due, among other factors, to rolling resistance (friction) and aerodynamic (air) or drag resistance, the latter being the most important quantitatively. On the resistance to the rolling the efforts for its reduction center in the tires, as much in its composition as in its design. However, the possibilities of action on aerodynamic drag are greater, being more effective in the rear and front of the vehicle. To quantify the aerodynamic drag, the axial force exerted by the air on the vehicle is calculated and is usually expressed in the scientific literature in a dimensionless manner by means of the drag coefficient or "drag":
    Fx
    Cx
    VA
    where: ρ is the density of the air, V is the speed of the vehicle and A is the frontal area of the same.
    The high interest in reducing aerodynamic drag is the close relationship between it and the fuel consumption of the vehicle and, consequently, with the carbon dioxide emissions generated by the vehicle. Current estimates of fuel consumption in heavy vehicles establish that about 20% of total fuel consumption is invested in overcoming such aerodynamic drag. Thus, the lower the aerodynamic drag, the lower the fuel consumption and greenhouse gas emissions.
    Actions to reduce this resistance may involve modifications throughout the vehicle: in the front, in the rear, in the lower part of the vehicle, between the traction car and the semi-trailer, etc. The front modifications fundamentally affect the cabin, so they are usually more restricted by technical and constructive needs. Therefore, the area with the greatest potential is the rear of the vehicle, since in addition to achieving reductions in the drag coefficient, it influences the control of the wake behind the vehicle, minimizing fluctuations and vibrations in the vehicle.
    The strategies and actions dedicated to this purpose are grouped according to the type of control that they carry out: passive, active in open loop, or active in closed loop, being understood as active control that which requires an external contribution of energy for its operation. Active control can be carried out in many different ways, for example, by introducing a blow in the rear of the truck, while passive control is usually related to an alteration of the exterior surface of the vehicle. The first two types of control, passive control and active control in open loop, operate in the same way regardless of the conditions of the flow around the vehicle, that is, they do not require feedback or outside information. On the contrary, the active closed loop control acts according to the flow conditions, therefore depending on its operation of the speed and pressure around the vehicle at all times. Although effective, active control in closed loop is usually more complex, requiring sensors and actuators to carry out flow control.
    Therefore, passive control stands out as the most viable and least cost solution. Passive control can be carried out in different ways, such as modifying the surface roughness, adding elements such as vortex-inducing stems
    or secondary control cylinders, or by modifying the geometry of the rear of the vehicle through the arrangement of ailerons or panels. This document focuses on the geometric modification of the rear of the vehicle. Next, some patent documents describing solutions of this type are briefly described.
    Document WO / 2015/007942 describes a system of straight panels configured to be installed on the rear surface of a vehicle so that they form a multicavity of at least four cavities preferably square or rectangular, as can be seen in Fig. 1a of this request.
    US 4,682,808 describes a drag reduction device consisting of panels that are fixed to the rear of the vehicle so that they capture at least two vortices that in turn orient the flow inwards at the rear of the vehicle body, so that for practical purposes a reduction of the rear area of the vehicle is achieved. An example of this device is shown in Fig. 1b of this application.
    US 5,498,059 proposes different cavity-based systems and different panel configurations in the rear. For example, Fig. 1c of the present application shows an example of the device formed by four straight panels that essentially constitute an extension of the four lateral surfaces of the vehicle. DESCRIPTION OF THE INVENTION
    The present invention describes a new type of perimeter device formed by several folding panels or ailerons configured for fixing to the edges of the rear side of a land vehicle and which are provided with a curved profile obtained according to the results of a parametric study to minimize the aerodynamic drag of the vehicle. That is, this strategy allows to obtain the optimum shape for the profile of the panels that make up the device, so that the reduction of aerodynamic drag is analytically maximized. The numerical simulations performed verify that the device achieves a significant additional improvement of the effect generated by flat-shaped devices used in the prior art.
    In this document, the term “land vehicle,” or simply “vehicle,” refers to any type of vehicle intended to move over the land surface, such as a car, a truck, a train, or others. In general, a vehicle will be assumed to have a main body essentially in the form of a parallelepiped, such as a truck with a parallelepiped box, in a train formed by wagons of a parallelepipedic shape, or others.
    In this document, the term "rear side" of the vehicle refers to a flat rear surface, taking as reference the natural direction of travel of said vehicle, of the essentially parallelepipedic main body of the vehicle.
    In this document, the term "lateral side" of the vehicle refers to any of the four flat surfaces located on the right, left, upper, and lower sides, taking as reference the natural direction of movement of said vehicle, of the main body essentially parallelepiped of the vehicle.
    In this document, the term "width" referring to a panel refers to the dimension of the panel according to the z axis according to the reference system described below. In other words, the width of the panel corresponds to the dimension of the panel according to a direction perpendicular to the direction of travel of the vehicle.
    In this document, the term "length" referring to a panel refers to the dimension of the panel according to a direction perpendicular to the surface of the rear side of the vehicle. That is, it is the distance between the base of the panel, which is fixed to the rear side of the vehicle, and the free end of the panel, according to a direction parallel to the direction of travel of the vehicle.
    In this document, the term "panel" refers to a spoiler configured for attachment to an edge on the rear side of the vehicle. The width of the panel can match the length of the corresponding edge so that the panel encompasses the entire edge from one end to the other. Alternatively, the panel may have a smaller width than the entire edge, for example for legal reasons, to facilitate the opening of the vehicle case, or for other reasons. It is also possible to use several panels substantially less wide than the corresponding edge which together cover all or a substantial part of the length of the edge. On the other hand, it is not necessary that each panel corresponds to a single physical piece. For example, the four panels corresponding to the four edges of the rear side of a vehicle can be connected to each other forming a single piece with essentially rectangular shape, or two complementary pieces with essentially U shape.
    In this document, the term "inner surface" of a panel refers to the surface of said panel which, when the panel is fixed to the corresponding edge of the vehicle, is oriented towards the center of the rear side of the vehicle. In other words, the inner surface of the panel fixed to a first edge faces the inner surface of the panel fixed to a second edge opposite the first. Similarly, the term "outer surface" of a panel refers to the surface of said panel which, when the panel is fixed to the corresponding edge of the vehicle, is oriented in the opposite direction to the center position of the rear side of the vehicle. That is, the outer surface
    The panel fixed to an edge is oriented in a direction away from the vehicle.
    The present invention describes a device for reducing aerodynamic drag in vehicles comprising at least one panel intended to be fixed to at least one edge of the rear side of said vehicle, and where at least the profile of the outer surface of said panel has a shape Optimized curve to reduce the aerodynamic drag of the vehicle. Specifically, the curved form of the present application is obtained by applying a parametric study accompanied by numerical simulations that employ a turbulent IDDES (Improved Delayed Detached Eddy Simulation) model, although it is conceivable to use other models to obtain curved shapes optimized of this type.
    In principle, the optimal configuration of the device is formed by four panels intended to be fixed respectively on the four edges of the rear side of a vehicle. However, for various practical reasons, other configurations are possible. For example, the lower edge panel can be removed because its influence on the aerodynamic coefficient of the vehicle is limited. Another possibility is that the device is formed by a single panel arranged, for example, on the upper edge. The main difference between the panels of the invention and the panels known so far, such as, for example, some of the panels described in the documents mentioned in the previous section, is that straight panels are replaced by panels that have, at least in their outer surface, a curved shape specially calculated to minimize the aerodynamic drag of the vehicle. This makes it possible to significantly improve the performance of the device, as will be shown in greater detail later in this document.
    The shape of the profile of the outer surface of a panel according to a preferred embodiment of the invention is defined qualitatively below. To do this, a reference system is formed consisting of an x axis perpendicular to the rear side of the vehicle, and an axis and contained in the rear side of the vehicle in a direction perpendicular to the edge of said rear side to which the panel is fixed. With this reference system, the preferred shape of the profile of the outer surface of each panel describes an initial decrease in the negative direction of the y-axis, reaches a minimum value in said y-axis, and ends with ascent in the positive direction of the y-axis, or well with a section essentially parallel to the x axis, to the tip.
    In principle, curves of this type can be defined mathematically using different expressions, although in another preferred embodiment of the present invention it is used
    specifically a polynomial expression of type:
    (yext / L) = aext (x / L) 4 + bext (x / L) 3 + cext (x / L) 2 + dext (x / L) + hext / L,
    where L is the total length of the panel and where the hext coefficient is the distance between the origin of coordinates and the edge at which the panel is fixed.
    A family of curves is thus defined which, for each given length L, allows the aerodynamic resistance to be significantly reduced relative to the known flat panels. The inventors of the present application have discovered that this expression adapts perfectly to the needs of the model used, allowing aerodynamic drag to be reduced without excessive complexity. To obtain the specific expression of the curve in each particular case, it is only necessary to select the desired total length L, and the hext coefficient (which, by properly locating the origin of the coordinate system, can be matched with the height of the rear side of the vehicle , for example).
    According to an even more preferred embodiment, the coefficients aext, bext, cext, and dext adopt a value that falls within the following ranges:
    - 0.768 <aext <-0.512
    1,648 <bext <2,472
    - 1,776 <cext <-1,184
    - 0.240 <dext <-0.160
    Even more preferably, the optimum values of the coefficients aext, bext, cext, and dext that allow obtaining the maximum possible aerodynamic drag reduction for each given length L are approximately the following:
    aext ≈ -0.64bext ≈ 2.06cext ≈ -1.48dext ≈ -0.20
    Therefore, the optimal expression of the curve defining the outer surface of the device according to the present invention takes the following form:
    (yext / L) = -0.64 (x / L) 4 + 2.06 (x / L) 3 - 1.48 (x / L) 2 - 0.20 (x / L) + hext / L,
    Until now, the outer surface of the panel has been described, since it has the greatest impact on the aerodynamic drag of the vehicle. Therefore, if necessary for practical reasons, such as improving mechanical strength, simplicity of manufacture, ease of fixing to the edges, etc., it would be possible that the interior surface did not have an optimized shape. For example, the inner surface could be essentially flat or in any other way that allowed the panel to be folded while ensuring sufficient mechanical strength.
    However, in an especially preferred embodiment of the invention also the profile of the inner surface has a curved shape optimized to reduce the aerodynamic drag of the vehicle. In this case, the shape of the interior surface profile can also be obtained through the application of a parametric study accompanied by numerical simulations using a turbulent IDDES model.
    To qualitatively describe the shape of the profile of the inner surface of the panel according to a preferred embodiment of the invention, the same coordinate system described above is taken. Thus, the preferred shape of the profile of the inner surface of the panel also describes an initial decrease in the negative direction of the y-axis, reaches a minimum value in said y-axis, and ends with ascent in the positive direction of the y-axis, or with a section essentially parallel to the x axis, to a point. In general, this means that the interior and exterior surfaces are essentially parallel.
    More preferably, the profile curve of the inner surface of the panel is defined by means of the polynomial expression:
    (yint / L) = aint (x / L) 4 + bint (x / L) 3 + belt (x / L) 2 + dint (x / L) + hint / L,
    where L is the total length of the panel and where the hint coefficient coincides with the hext value minus the thickness of the panel.
    Similar to that described above, to obtain the specific expression of the curve in each particular case it is only necessary to select the desired total length L, and the hint coefficient (for example, through the selection of the desired thickness for the whole panel ).
    According to an even more preferred embodiment, the corresponding aint, bint, cint, and dint coefficients the formula that defines the shape of the profile of the inner surface of the panel adopt a value that falls within the following ranges:
    -0,588 <aint <-0,3921,328 <bint <1,992-1,644 <belt <-1,096-0.084 <dint <-0.056
    Even more preferably, the optimal values of the coefficients aint, bint, cint, and dint that allow obtaining the maximum possible aerodynamic drag reduction for each given length L are approximately the following:
    aint ≈ -0.49bint ≈ 1.66belt ≈ -1.37dint ≈ -0.07
    Therefore, the optimal expression of the curve defining the inner surface of the device according to the present invention takes the following form:
    (yint / L) = -0.49 (x / L) 4 + 1.66 (x / L) 3 - 1.37 (x / L) 2 - 0.07 (x / L) + hint / L,
    With regard to the length of the panels of the present invention, it is chosen according to the needs of each case. Ideally, longer panels allow for greater reductions in aerodynamic drag, although obviously the maximum length of the panels may be limited for practical reasons such as applicable legislation, ease of assembly / disassembly, ease of opening the rear side of the vehicle, mechanical resistance of the panels, etc. In any case, according to a preferred embodiment of the present invention, the optimum panel length is between 0.2 1.2 meters. As regards the thickness, it should preferably be less than 20 cm. In general, the thickness will be the minimum possible as long as the panels are rigid enough to prevent breakage and deflection, although preventing them from being too large so that they can hinder their implementation and handling.
    Finally, the panels can be made of any material provided that it has sufficient mechanical strength to withstand the forces to which it will be subjected during its useful life, and that its installation does not significantly increase the weight of the vehicle or cause vibrations that may affect its stability and manageability. For example, preferably the panels are made of a material selected from: composite fiber, carbon fiber, rigid plastic, and aluminum. BRIEF DESCRIPTION OF THE FIGURES
    Figs. 1 a-c show three examples of devices for reducing aerodynamic drag according to the prior art.
    Fig. 2 shows a perspective view of the rear portion of a vehicle with the reference system used to define the shape of the panels of the present invention.
    Fig. 3 shows a detailed side view of the form of an example panel according to the present invention.
    Fig. 4 shows a detailed side view of the range of possible shapes that the panel of the present invention can take for the example shown in Fig. 3 as a function of the variation of the polynomial coefficients.
    Fig. 5 shows a perspective view of the rear portion of a vehicle to which four panels have been fixed in accordance with the present invention.
    Fig. 6 shows a rear view of the vehicle of Fig. 6.
    Fig. 7 shows a top view of the vehicle of Fig. 6.
    Fig. 8 shows a side view of the vehicle of Fig. 6.
    Fig. 9 shows a perspective view of an example of a device according to the invention formed by a single piece.
    Fig. 10 shows a perspective view of another example of a device according to the invention formed by a folding set of pieces like slats. PREFERRED EMBODIMENT OF THE INVENTION
    Next, the process of calculating the shape of the inner (2i) and outer (2e) surfaces of an example panel (2) according to the present invention is described in greater detail with reference to the attached figures.
    The optimization of the shape of both surfaces begins with a straight profile to, from there, modify the polynomials that define the geometry of the profiles according to an optimization process according to the influence observed in the fluid layer around the body . This study gives as a final result a smoothed curved shape that constitutes the optimal solution for the flow conditions existing around the model studied.
    The parametric optimization study has been carried out under adequate simplified conditions that make it possible to obtain an optimal form of the panels and guarantee the convergence of the method, being:
    VH
    Re  2000
    ,
    where H is the height of the vehicle model (100) used, V is the vehicle speed,  is the density of the air, and μ the viscosity of the air. The Reynolds number chosen for the parametric study corresponds to a small speed for a vehicle model
    (100) of real dimensions, but it provides stability and robustness to the technique used to obtain the curved perfies.
    In order to verify its applicability, numerical simulations have been carried out under realistic conditions of the flow that exist around this type of vehicles (100) at a higher Reynolds number:
    5VH 5
    Re 210


    These last simulations only serve to evaluate the effectiveness of the present invention, obtained in the simplified study, under more realistic conditions using an IDDES turbulent model that is the most realistic when it comes to reproducing the turbulent flow in this type of blunt bodies. The turbulent IDDES model is mainly defined in the following two articles:
    M. L. Shur, P. R. Spalart, M. K. Strelets, and A. K. Travin. "A Hybrid RANS-LES Approach With Delayed-DES and Wall-Modelled LES Capabilities". International Journal of Heat and Fluid Flow. 29: 6 December 2008. 1638-1649
    M. S. Gritskevich, A. V. Garbaruk, J. Schutze, F. R. Menter. "Development of DDES and IDDES Formulations for the k-ω Shear Stress Transport Model." Flow, Turbulence and Combustion. 88 (3). 431–449. 2012
    The possible variation between the conditions at a high simulated Reynolds number and the real ones is predictably negligible, since the drag coefficient tends towards a constant value as the Re number increases, which corresponds to an increase in vehicle speed (100). The models used in the numerical study are representative of large cargo vehicles and similar to those proposed by Ahmed, SR, Ramm, G., & Faitin, G. (1984) in “Some salient features of the time-averaged ground vehicle wake” , SAE-TP840300.
    In this example, the general expressions described above in this document are particularized in the case of panels (2) whose length (L) is 30 cm. 30 cm in length is chosen because, although ideally greater reductions in aerodynamic drag are obtained for longer lengths, there are legal and practical restrictions that limit the maximum allowed length. On the other hand, a reference system formed by an x axis perpendicular to the rear side (LT) of the vehicle (100), and an axle and content on the rear side (LT) of the vehicle (100) in the direction perpendicular to the edge (A) of said rear side (LT) to which the panel is fixed. The arrangement of the reference system can be seen in greater detail in Fig. 2, which shows a vehicle (100) comprising four lateral sides (LL) and a rear side (LT). The rear side (LT) comprises four edges (A) that constitute the cutting lines between said rear side (LT) and the lateral sides (LL). In this specific example, a vehicle (100) is considered to have a parallelepiped shaped body with a height of 2 meters with respect to the origin of coordinates.
    As a result, two dimensional polynomials are obtained that express the curvature of the inner (2i) and outer (2e) surfaces of the panels (2), taking into account L = 0.3 m, hext = 2.00 m and hint = 1 , 96. The resulting expressions are as follows:
    4 32
    yext 23.70 x 22.89 x 4.93 x 0.202 x 2
    4 32
    yint 18.15x 18.44 x 4.57 x 0.07 x 1.96
    where yext defines the shape of the profile of the outer surface (2e) of the panel (2) and yint defines the shape of the profile of the inner surface (2i) of the panel (2), and where the magnitudes are expressed in units of the International System . A view of the profile of the panel (2) is shown in Fig. 3. In a broken line the shape of a straight panel of a type similar to those used in the prior art has been drawn.
    In addition, as described earlier in this document, it is possible to make minor modifications to the shape of the panel profile (2) while maintaining a significant reduction in drag coefficient compared to known flat designs. For example, Fig. 4 shows the family of curves generated allowing a variation of 20% for each of the polynomial coefficients of the expression that defines the shape of the inner surface (2i) and the outer surface (2e). This 20% variation of the coefficients results in the allowable ranges for each coefficient described above in this document. While the curves in Fig. 4 slightly deviate from the optimum curve described above, any panel (2) defined in this way also allows a vehicle's aerodynamic drag to be significantly reduced
    (100) compared to the flat designs of the prior art.
    In the evaluation study of the efficacy of the present invention, the percentage reduction in aerodynamic drag obtained with respect to a vehicle lacking a rear device using a four panel device (2) according to the present invention has been compared with the percentage reduction obtained with straight panels. Specifically, this table shows the percentage of reduction obtained using four straight panels of 1.2 meters and 0.3 meters in length respectively and the percentage of reduction obtained using the device of the invention of 0.3 meters in length. As can be seen, the reduction achieved using straight panels of 1.2 meters in length is approximately 30%, while using straight panels of 0.3 meters in length is approximately 28%. Therefore, the percentage of reduction is hardly affected by the length, within the ranges studied. On the other hand, using the device of the present invention with panels (2) of 0.3 meters in length a reduction of approximately 42% is achieved, which constitutes a considerable improvement.
    Device used Straight panels (L = 1.2 m)Straight panels (L = 0.3 m)Panels of the invention (L = 0.3 m)
    Aerodynamic drag reduction (%) 302842
    Fig. 5 shows an isometric view of the rear part of a vehicle (100) having four panels (2) according to the invention fixed to the respective four edges of its rear side (LT). In this example, the length of the panels (2) is about 0.3 meters, which prevents them from interfering with signaling elements or vehicle identification plates (100).
    To allow the deployment of the panels (2), the device further comprises hinges (3) arranged in the joint between the edges (A) of the rear side (LT) and the panels (2). Thus, it is possible to use any type of drive, for example pneumatic, hydraulic, electronic or manual, to move the plates (2) from their use position essentially perpendicular to the rear side (LT) to a retracted position essentially parallel to said rear side (LT).
    The device further comprises squares (4) that rest on the inner surface (2i) of the panels (2), for example located in its central part, to provide sufficient rigidity against deflection so that the shape is maintained of the panels
    (2) and the possible vibrations are reduced.
    In addition, to ensure the tightness and cross stiffness of the formed rear region, the device of the invention may further comprise magnetized connecting elements (5) to facilitate the coupling of the ends of the panels (2). Indeed, the ends of the panels (2) must be joined together through a relatively complex curved shape, which can be complicated if the aforementioned magnetized joining elements (5) are not used.
    Figs. 9 and 10 show two additional examples of the device according to the present invention formed by a single panel (2) fixed to the upper edge of the rear side (LT) of the vehicle (100). Specifically, the panel (2) of Fig. 9 is composed of a single piece, while the panel of Fig. 10 is composed of a plurality of sheets configured to alternate between a retracted position and an extended position according to the direction of the length (L). Fig. 10 shows the extended position, which is the position of use where the panel (2) adopts the curved shape defined above in this document. When the device is not going to be used, the sheets that constitute this panel
    (2) fold back until they are piled in parallel to each other next to the edge of the vehicle (100). The sheets may have some flexibility to improve folding.
    权利要求:
    Claims (17)
    [1]
    one. Device for reducing aerodynamic drag in vehicles, comprising at least one panel (2) intended to be fixed to at least one edge (A) of the rear side (LT) of said vehicle (100), characterized in that at least the profile of The outer surface (2e) of said panel (2) has a curved shape optimized to reduce the aerodynamic drag of the vehicle (100), said curved shape being obtained by applying a parametric study accompanied by numerical simulations using a turbulent IDDES model .
    [2]
    2. Device according to claim 1, wherein the shape of the profile of the outer surface (2e) of the panel (2), defined by reference to an x axis perpendicular to the rear side (LT) of the vehicle (100), and a y axis content on the rear side (LT) of the vehicle
    (100) in the direction perpendicular to the edge (A) of said rear side (LT) to which the panel (2) is fixed, presents an initial decrease in the negative direction of the y-axis, reaches a minimum value on said axis and, and ends with an ascent in the positive direction of the y-axis, or with a section essentially parallel to the x-axis, to a point (2p).
    [3]
    3. Device according to claim 2, wherein the shape of the profile of the outer surface (2e) of the panel (2) is defined by a polynomial expression of type:
    (yext / L) = aext (x / L) 4 + bext (x / L) 3 + cext (x / L) 2 + dext (x / L) + hext / L, where L is the total length of the device and the hext coefficient is the distance between the origin of coordinates and the edge (A) at which the panel (2) is fixed.
    [4]
    Four. Device according to claim 3, wherein the coefficients aext, bext, cext, and dext adopt a value that is within the following ranges: -0.768 <aext <-0.512
    1,648 <bext <2,472 -1,776 <cext <-1,184 -0,240 <dext <-0,160
    [5]
    5. Device according to claim 4, wherein the coefficients aext, bext, cext, and dext
    have an optimal value of: aext ≈ -0.64 bext ≈ 2.06
    16 cext ≈ -1.48 dext ≈ -0.20
    [6]
    6. Device (1) according to any of the preceding claims, wherein also the profile of the inner surface (2i) of said at least one panel (2) has a curved shape optimized to reduce the aerodynamic drag of the vehicle (100), being able to Obtain this curved form by applying a parametric study accompanied by numerical simulations using the turbulent IDDES model.
    [7]
    7. Device according to claim 6, wherein the shape of the profile of the inner surface (2i) of the panel (2), defined by reference to an x axis perpendicular to the rear side (LT) of the vehicle (100), and a y axis content on the rear side (LT) of the vehicle
    (100) in the direction perpendicular to the edge (A) of said rear side (LT) to which the panel (2) is fixed, presents an initial decrease in the negative direction of the y-axis, reaches a minimum value on said axis and, and ends with ascent in the positive direction of the y-axis, or with a section essentially parallel to the x-axis, to the tip (2p).
    [8]
    8. Device according to claim 7, wherein the shape of the profile of the inner surface (2i) of the panel (2) is defined by a polynomial expression of type:
    (yint / L) = aint (x / L) 4 + bint (x / L) 3 + belt (x / L) 2 + dint (x / L) + hint / L, where L is the total length of the device and where the hint coefficient coincides with the hext value minus the thickness of the device.
    [9]
    9. Device according to claim 8, wherein the coefficients aint, bint, cint, and dint
    they adopt a value that falls within the following ranges: -0,588 <aint <-0,392 1,328 <bint <1,992 -1,644 <belt <-1,096 -0,084 <dint <-0,056
    [10]
    10. Device according to claim 9, wherein the coefficients aint, bint, cint, and
    dint have an optimal value of: aint ≈ -0.49 bint ≈ 1.66 belt ≈ -1.37 dint ≈ -0.07
    [11]
    eleven. Device according to any of the preceding claims, wherein the optimum total length (L) of the panel (2) is between 0.2-1.2 meters.
    [12]
    12. Device according to any of the preceding claims, wherein the thickness of the panel (2) is less than 20 cm.
    [13]
    13. Device according to any of the preceding claims, wherein the panel (2) is made of a material selected from: composite fiber, carbon fiber, rigid plastic, and aluminum.
    [14]
    14. Device according to any of the preceding claims, further comprising hinges (3) arranged at the junction between the edge (A) of the rear side (LT) and the panel (2).
    [15]
    fifteen. Device according to any of the preceding claims, which further comprises brackets (4) that rest on the inner surface (2i) of the panel (2) to provide sufficient rigidity against deflection.
    [16]
    16. Device according to any of the preceding claims, which also magnetized connecting elements (5) to facilitate the coupling of the ends of the panels (2).
    [17]
    17. Device according to any of the preceding claims, wherein the panel (2) is formed by a plurality of sheets configured to alternate between a retracted position and an extended position according to the direction of the length (L) of the panel (2).
    22
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    同族专利:
    公开号 | 公开日
    WO2018020068A1|2018-02-01|
    ES2651902B2|2018-05-08|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    WO2012051174A1|2010-10-13|2012-04-19|Advanced Transit Dynamics, Inc.|Rear-mounted aerodynamic structure for truck cargo bodies|
    US20140292023A1|2013-02-01|2014-10-02|Clarkson University|Drag Reduction of a Tractor Trailer Using Guide Vanes|
    US20160137234A1|2014-11-14|2016-05-19|Embry-Riddle Aeronautical University, Inc.|Optimizing jets for wake control of ground vehicles|
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    PCT/ES2017/070521| WO2018020068A1|2016-07-29|2017-07-19|Device for reducing the aerodynamic resistance of land vehicles|
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