ES1299306U

ES1299306U - Aerodynamic device (Machine-translation by Google Translate, not legally binding)

Info

Publication number: ES1299306U
Application number: ES202231936U
Authority: ES
Inventors: Cases Gaspar Rodes
Original assignee: Individual
Current assignee: Individual
Priority date: 2022-11-21
Filing date: 2022-11-21
Publication date: 2023-04-26
Anticipated expiration: 2032-11-21
Also published as: ES1299306Y; ES1299306U8

Abstract

Dispositivo aerodinámico caracterizado porque comprende al menos dos alerones laterales (2) en la parte trasera de los laterales de un vehículo de carga (1) situados de forma simétrica, así como al menos dos alerones superiores (3) situados en la parte trasera de la parte superior de un vehículo de carga (1), que son desplegables y plegables.Aerodynamic device characterized in that it comprises at least two lateral wings (2) at the rear of the sides of a cargo vehicle (1) located symmetrically, as well as at least two upper wings (3) located at the rear of the upper part of a cargo vehicle (1), which are deployable and collapsible.

Description

DESCRIPCIÓNDESCRIPTION

Dispositivo aerodinámicoaerodynamic device

OBJETO DE LA INVENCIÓNOBJECT OF THE INVENTION

Es objeto de la presente invención, tal y como el título de la invención establece, un dispositivo aerodinámico que se instala en vehículos de carga. Se trata de una innovación que dentro de las técnicas actuales aporta ventajas desconocidas hasta ahora.The object of the present invention, as the title of the invention establishes, is an aerodynamic device that is installed in cargo vehicles. It is an innovation that within the current techniques provides advantages unknown until now.

SECTOR DE LA TÉCNICATECHNIQUE SECTOR

La presente invención pertenece al sector de la automoción.The present invention belongs to the automotive sector.

ANTECEDENTES DE LA INVENCIÓNBACKGROUND OF THE INVENTION

Como referencia al estado actual de la técnica, cabe señalar que, si bien se conocen diseños elementos para mejorar la aerodinámica de los vehículos de carga, se desconoce la existencia de ningún otro que presente características técnicas estructurales y constitutivas iguales o semejantes a las que presenta la invención que aquí se reivindica.As a reference to the current state of the art, it should be noted that, although element designs to improve the aerodynamics of cargo vehicles are known, the existence of any other that presents structural and constituent technical characteristics equal or similar to those presented is unknown. the invention claimed herein.

EXPLICACIÓN DE LA INVENCIÓNEXPLANATION OF THE INVENTION

Actualmente los vehículos de transporte de mercancías en su parte trasera no suelen ser aerodinámicos, esto provoca que el vehículo tenga una mayor resistencia al rozamiento con el aire y provoque un mayor consumo de combustible al contrarrestar estas fuerzas.Currently, goods transport vehicles at the rear are not usually aerodynamic, this causes the vehicle to have a greater resistance to friction with the air and causes greater fuel consumption by counteracting these forces.

Es objeto de la presente invención un dispositivo aerodinámico que permite a los vehículos de carga ser aerodinámicos en su parte trasera sin alterar la propia estructura del vehículo mediante el añadido de alerones en los laterales de la parte trasera, así como en la parte superior e inferior de la parte trasera del vehículo, dotando de una forma más aerodinámica a la parte trasera del vehículo. The object of the present invention is an aerodynamic device that allows cargo vehicles to be aerodynamic at the rear without altering the structure of the vehicle itself by adding spoilers on the sides of the rear, as well as on the top and bottom. from the rear of the vehicle, giving a more aerodynamic shape to the rear of the vehicle.

Estos alerones son plegables y desplegables, estando plegados cuando no se están utilizando y desplegándose cuando se requiere que funcionen, siendo este proceso manual, o bien de una forma automática estando los medios de accionamiento en este caso en la cabina del vehículo.These flaps are foldable and deployable, being folded when they are not being used and unfolding when they are required to work, this process being manual, or else automatically, the actuation means being in this case in the vehicle cabin.

El dispositivo aerodinámico permite que el vehículo de carga sea más aerodinámico reduciendo su resistencia al aire, permitiendo un mayor ahorro de combustible y una reducción significativa de la contaminación. Así mismo el dispositivo aerodinámico también sirve como amortiguador en caso de un posible choque con otro vehículo por la parte trasera, absorbiendo la energía del impacto y evitando un daño mayor al vehículo de carga y al vehículo siniestrado.The aerodynamic device allows the cargo vehicle to be more aerodynamic by reducing its air resistance, allowing greater fuel savings and a significant reduction in pollution. Likewise, the aerodynamic device also serves as a shock absorber in the event of a possible collision with another vehicle from the rear, absorbing the energy of the impact and avoiding further damage to the cargo vehicle and the damaged vehicle.

BREVE DESCRIPCIÓN DE LOS DIBUJOSBRIEF DESCRIPTION OF THE DRAWINGS

Para completar la descripción que se está realizando y con objeto de ayudar a la mejor comprensión de las características de la invención, se acompaña a la presente memoria descriptiva, como parte integrante de la misma, de unas figuras en las que, con carácter ilustrativo y no limitativo, se ha representado lo siguiente:To complete the description that is being made and in order to help a better understanding of the characteristics of the invention, this specification is accompanied, as an integral part thereof, by some figures in which, for illustrative and not limiting, the following has been represented:

La Figura 1 es una representación en perspectiva del dispositivo aerodinámico desplegado en un vehículo de carga (1).Figure 1 is a perspective representation of the aerodynamic device deployed in a cargo vehicle (1).

La Figura 2 es una representación del dispositivo aerodinámico desplegado en un vehículo de carga (1) en detalleFigure 2 is a representation of the aerodynamic device deployed in a cargo vehicle (1) in detail.

La Figura 3 es una representación en perspectiva del dispositivo aerodinámico plegado en un vehículo de carga (1).Figure 3 is a perspective representation of the aerodynamic device folded in a cargo vehicle (1).

REALIZACIÓN PREFERENTE DE LA INVENCIÓNPREFERRED EMBODIMENT OF THE INVENTION

A la vista de las figuras se describe seguidamente un modo de realización preferente, aunque no limitativa de la invención propuesta, la cual consiste en un dispositivo aerodinámico. Tal y como se aprecia en las figuras, el dispositivo aerodinámico, comprende al menos dos alerones laterales (2) en la parte trasera de los laterales de un vehículo de carga (1) situados de forma simétrica, así como al menos dos alerones superiores (3) situados en la parte trasera de la parte superior de un vehículo de carga (1), que son desplegables y a su vez plegables.In view of the figures, a preferred, though not limiting, embodiment of the proposed invention is described below, which consists of an aerodynamic device. As can be seen in the figures, the aerodynamic device comprises at least two lateral flaps (2) at the rear of the sides of the a cargo vehicle (1) located symmetrically, as well as at least two upper wings (3) located at the rear of the upper part of a cargo vehicle (1), which are deployable and foldable in turn.

Los alerones laterales (2) comprenden en uno de sus extremos una superficie auxiliar lateral (2.1) que está configurada para extenderse y fijarse a su homólogo del lado opuesto formando una estructura firme.The lateral wings (2) comprise at one of their ends a lateral auxiliary surface (2.1) that is configured to extend and be fixed to its counterpart on the opposite side, forming a firm structure.

Los alerones superiores (3) comprenden en uno de sus extremos una superficie auxiliar superior (3.1) que está configurada para extenderse y fijarse a su homólogo del lado opuesto y los laterales (2) formando un cerramiento y una estructura firme.The upper wings (3) include at one of their ends an upper auxiliary surface (3.1) that is configured to extend and be fixed to its counterpart on the opposite side and the sides (2) forming an enclosure and a firm structure.

Dependiendo del modo de realización el dispositivo aerodinámico comprende al menos dos alerones inferiores (4) situados en la parte trasera de la parte inferior de un vehículo de carga (1) plegables y desplegables, comprendiendo en uno de sus extremos una superficie auxiliar inferior (4.1) que está configurada para extenderse y fijarse a su homólogo del lado opuesto y a los laterales (2) formando un cerramiento y una estructura firme.Depending on the embodiment, the aerodynamic device comprises at least two lower flaps (4) located at the rear of the lower part of a cargo vehicle (1) that are foldable and deployable, comprising a lower auxiliary surface (4.1) at one of its ends. ) which is configured to extend and be fixed to its counterpart on the opposite side and to the sides (2) forming an enclosure and a firm structure.

El dispositivo aerodinámico comprende unos medios de accionamiento que podrán ser de carácter manual, o ser de carácter automático. The aerodynamic device comprises drive means that may be manual or automatic.

Claims

1. Aerodynamic device characterized in that it comprises at least two lateral wings (2) at the rear of the sides of a cargo vehicle (1) located symmetrically, as well as at least two upper wings (3) located at the rear from the upper part of a cargo vehicle (1), which are deployable and collapsible.

2. Aerodynamic device according to the preceding claim, characterized in that the lateral wings (2) comprise at one of their ends a lateral auxiliary surface (2.1) that is configured to extend and be fixed to its counterpart on the opposite side.

3. Aerodynamic device according to any of the preceding claims, characterized in that the upper wings (3) comprise at one of their ends an upper auxiliary surface (3.1) that is configured to extend and be fixed to its counterpart on the opposite side and to the sides (2 ) forming an enclosure and a firm structure.

4. Aerodynamic device according to any of the preceding claims, characterized in that it comprises at least two lower wings (4) located at the rear of the lower part of a cargo vehicle (1) that are deployable and collapsible.

5. Aerodynamic device according to the preceding claim, characterized in that the lower wings (4) comprise at one of their ends a lower auxiliary surface (4.1) that is configured to extend and be fixed to its counterpart on the opposite side and to the sides (2).

6. Aerodynamic device according to any of the preceding claims, characterized in that it comprises drive means.

7. Aerodynamic device according to the previous claim, characterized in that the actuation means are manual.

8. Aerodynamic device according to claim 6, characterized in that the drive means are automatic.