ES2694245T3 - Addressable antenna - Google Patents

Addressable antenna Download PDF

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Publication number
ES2694245T3
ES2694245T3 ES14198496.3T ES14198496T ES2694245T3 ES 2694245 T3 ES2694245 T3 ES 2694245T3 ES 14198496 T ES14198496 T ES 14198496T ES 2694245 T3 ES2694245 T3 ES 2694245T3
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Prior art keywords
motor
support arm
pulley
antenna
base
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Spanish (es)
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Massimo Coppola
Giuseppe Luigi Lutricusi
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MBDA Italia SpA
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MBDA Italia SpA
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2213Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2246Active homing systems, i.e. comprising both a transmitter and a receiver
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2286Homing guidance systems characterised by the type of waves using radio waves
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/281Nose antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q21/00Antenna arrays or systems
    • H01Q21/06Arrays of individually energised antenna units similarly polarised and spaced apart
    • H01Q21/061Two dimensional planar arrays

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Details Of Aerials (AREA)
  • Support Of Aerials (AREA)

Abstract

Antena direccionable (1), que comprende: - una carga útil (4, 5) orientable; - un sistema electromecánico (6-10) de movimiento y soporte, conectado operativamente a la carga útil (4, 5) y adaptado para orientar la carga útil de una manera controlada, comprendiendo dicho sistema electromecánico una base (6), un primer motor (7) sujeto a la base (6), una polea de transmisión (8) conectada operativamente al primer motor (7) para hacer que gire en torno a un primer eje de rotación, un segundo motor (9) conectado operativamente a la polea de transmisión (8) y conectado operativamente a la carga útil (4, 5) para hacer que gire la carga útil en torno a un segundo eje de rotación; en donde el sistema electromecánico (6-10) de movimiento y soporte comprende además un brazo de soporte (10) integral con la base (6), al que está abisagrado pivotantemente el segundo motor (9) y la polea de transmisión (8) está conectada operativamente al segundo motor (9) para hacer que gire el segundo motor (9) con relación a la base (6) y con relación al brazo de soporte (10); en donde el sistema electromecánico (6-10) de movimiento y soporte comprende un sistema (18, 19, 48, 49) de transmisión por correa adaptado para acoplar operativamente el primer motor (7) a la polea de transmisión (8), comprendiendo dicho sistema de transmisión una polea motriz (48, 49) acoplada al primer motor (7); caracterizada porque dicho sistema (18, 19, 48, 49) de transmisión por correa comprende dos correas (18, 19) cruzadas que tienen una primera porción de extremo sujeta a dicha polea motriz (48, 49), en donde dichas correas (8, 19) están fabricadas con una aleación metálica y cada una de ellas tiene una segunda porción de extremo sujeta a dicha polea de transmisión (8), en donde la polea motriz (48, 49) comprende dos poleas (48, 49) paralelas, unidas entre sí por medio de un sistema de acoplamiento que permite el ajuste de la orientación recíproca de dichas poleas (48, 49) paralelas.Addressable antenna (1), comprising: - a steerable payload (4, 5); - an electromechanical system (6-10) of movement and support, operatively connected to the payload (4, 5) and adapted to guide the payload in a controlled manner, said electromechanical system comprising a base (6), a first motor (7) attached to the base (6), a transmission pulley (8) operatively connected to the first motor (7) to cause it to rotate about a first axis of rotation, a second motor (9) operatively connected to the pulley of transmission (8) and operatively connected to the payload (4, 5) to cause the payload to rotate about a second axis of rotation; wherein the electromechanical system (6-10) of movement and support further comprises a support arm (10) integral with the base (6), to which the second motor (9) and the transmission pulley (8) are hinged pivotably. is operatively connected to the second motor (9) to cause the second motor (9) to rotate relative to the base (6) and relative to the support arm (10); wherein the electromechanical system (6-10) of movement and support comprises a belt transmission system (18, 19, 48, 49) adapted to operatively couple the first motor (7) to the transmission pulley (8), comprising said drive system a drive pulley (48, 49) coupled to the first motor (7); characterized in that said belt transmission system (18, 19, 48, 49) comprises two crossed belts (18, 19) having a first end portion secured to said drive pulley (48, 49), wherein said belts (8, 19). , 19) are made of a metallic alloy and each of them has a second end portion attached to said drive pulley (8), wherein the drive pulley (48, 49) comprises two parallel pulleys (48, 49), joined together by means of a coupling system that allows the adjustment of the reciprocal orientation of said parallel pulleys (48, 49).

Description

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DESCRIPCIONDESCRIPTION

Antena direccionable.Addressable antenna

La presente descripcion se refiere al sector tecnico de las antenas direccionables.The present description refers to the technical sector of addressable antennas.

Se conoce desde hace mucho tiempo que las antenas direccionables comprenden un dispositivo orientable receptor y/o transmisor de radiacion electromagnetica, cuya direccion de senalamiento puede ser controlada por medio de un sistema electromecanico de movimiento y soporte que hace que sea posible orientar el dispositivo orientable de recepcion y/o transmision en el espacio, por ejemplo para ampliar el angulo de exploracion de la antena. El dispositivo orientable receptor y/o transmisor de radiacion electromagnetica se conoce tambien en general como carga util.It has been known for a long time that the addressable antennas comprise an orientable receiver and / or electromagnetic radiation transmitter whose direction of direction can be controlled by means of an electromechanical system of movement and support which makes it possible to orient the orientable device of the electromagnetic radiation. reception and / or transmission in space, for example to expand the scanning angle of the antenna. The orientable receiver device and / or transmitter of electromagnetic radiation is also known in general as a payload.

En algunos casos, tal como por ejemplo el caso de las antenas direccionables de un buscador de misil, el sistema electromecanico de movimiento y soporte utilizado es comparable a un sistema de altazimut y puede estar controlado electronicamente para permitir que el dispositivo orientable de recepcion y/o transmision gire en torno a dos ejes ortogonales entre si y defina un angulo conico de apertura del haz de antena.In some cases, such as, for example, the case of the addressable antennae of a missile search engine, the electromechanical system of movement and support used is comparable to an altazimut system and can be electronically controlled to allow the orientable receiving device and / or transmission rotate around two axes orthogonal to each other and define a cone angle of aperture of the antenna beam.

Teoricamente y segun una primera aproximacion, el sistema electromecanico de movimiento y soporte, o sistema de direccionamiento, debe garantizar un senalamiento altamente preciso, debe ser capaz de impartir aceleraciones relativamente altas al dispositivo orientable receptor y/o transmisor de radiacion electromagnetica, y debe asegurar un angulo conico de apertura del haz de antena que sea tan amplio como sea posible.Theoretically and according to a first approximation, the electromechanical system of movement and support, or addressing system, must guarantee a highly accurate signaling, it must be capable of imparting relatively high accelerations to the orientable receiver and / or electromagnetic radiation transmitter, and must ensure a conical opening angle of the antenna beam that is as wide as possible.

El sistema de control electronico del sistema electromecanico de movimiento y soporte, esta desarrollado en general sobre la base de un comportamiento mecanico teorico del sistema electromecanico de movimiento y soporte, y de varios sensores a bordo de la antena direccionable, por ejemplo sensores de posicion y/o de velocidad y/o giroscopicos, asociados al sistema electromecanico de movimiento y soporte que se usan para crear un control en bucle cerrado. El resultado de la lectura del sensor es lo que esta ocurriendo localmente; por lo tanto, es importante que corriente abajo de esta lectura no existan deformaciones o comportamientos que sean indetectables por los sensores, que pudieran conducir a un comando incorrecto del sistema electromecanico de movimiento y soporte. Estas desviaciones del estandar son por lo general mencionadas habitualmente mediante el termino aberraciones. En teoria, los sensores podrian estar colocados tan cerca como sea posible del dispositivo orientable receptor y/o transmisor de radiacion electromagnetica, de modo que el sistema de control conozca siempre de manera precisa su posicion real. Una posicion distante de los mismos, con una serie de controles mecanicos intermedios, podra introducir aberraciones mecanicas debido a la imprecision de los emparejamientos, a las deformaciones elasticas del sistema debidas a esfuerzos externos y a la imprecision en la mecanizacion de las piezas mecanicas.The electronic control system of the electromechanical system of movement and support, is developed in general on the basis of a theoretical mechanical behavior of the electromechanical system of movement and support, and of several sensors on board of the addressable antenna, for example position sensors and / o speed and / or gyroscopic, associated with the electromechanical system of movement and support that are used to create a closed loop control. The result of the sensor reading is what is happening locally; therefore, it is important that downstream of this reading there are no deformations or behaviors that are undetectable by the sensors, which could lead to an incorrect command of the electromechanical system of movement and support. These deviations from the standard are usually usually mentioned by the term aberrations. In theory, the sensors could be placed as close as possible to the orientable receiver device and / or transmitter of electromagnetic radiation, so that the control system always knows precisely its real position. A distant position of them, with a series of intermediate mechanical controls, could introduce mechanical aberrations due to the imprecision of the pairings, to the elastic deformations of the system due to external stresses and to the imprecision in the mechanization of the mechanical parts.

La solucion ideal podria consistir en estar en condiciones de acoplar los sensores directamente bajo el dispositivo orientable receptor y/o transmisor de radiacion electromagnetica, acoplados a este ultimo con conexiones rigidas, sin controles mecanicos intermedios. La solucion, sin embargo, tiende a limitar el angulo conico; y cuanto mayor sea este, mas grandes son los sensores (y los motores). Con esta configuracion, al desear favorecer el rendimiento en terminos de aceleracion angular (motores mas grandes), se penalizara el rendimiento en terminos de amplitud del angulo conico; a la inversa, el deseo de favorecer este ultimo, penalizara el rendimiento en terminos de aceleraciones angulares en tanto que hace que sea mas apropiado el uso de motores mas pequenos.The ideal solution could be to be able to couple the sensors directly under the orientable receiver device and / or transmitter of electromagnetic radiation, coupled to the latter with rigid connections, without intermediate mechanical controls. The solution, however, tends to limit the cone angle; and the bigger this is, the bigger the sensors (and the motors) are. With this configuration, when desiring to favor the performance in terms of angular acceleration (larger motors), the performance in terms of amplitude of the conical angle will be penalized; conversely, the desire to favor the latter will penalize performance in terms of angular accelerations while making the use of smaller motors more appropriate.

Un posible compromiso entre el rendimiento en terminos de aceleracion angular y la amplitud del angulo conico, podria lograrse mediante la separacion de los motores hacia fuera de la carga util, aun estando conectados rigidamente al dispositivo orientable receptor y/o transmisor de radiacion electromagnetica; esto podria determinar, sin embargo, un incremento del radio de la esfera de huella de la antena direccionable, lo que resulta problematico debido a que el espacio disponible en el radomo es limitado. Adicionalmente, la solucion anterior requiere, en el caso de antenas de microondas, una conexion de senal con cable apantallado al dispositivo receptor y/o transmisor de radiacion electromagnetica, lo que afecta al rendimiento de radiofrecuencia y reduce la potencia maxima transportable.A possible compromise between the performance in terms of angular acceleration and the amplitude of the conic angle, could be achieved by separating the motors out of the useful load, even though they are rigidly connected to the orientable receiver device and / or electromagnetic radiation transmitter; this could, however, determine an increase in the radius of the addressable antenna fingerprint sphere, which is problematic because the available space in the radome is limited. Additionally, the above solution requires, in the case of microwave antennas, a signal connection with shielded cable to the receiver and / or electromagnetic radiation transmitter, which affects the radiofrequency performance and reduces the maximum transportable power.

Una alternativa diferente, relativamente mas generalizada que la descrita con anterioridad, consiste en posicionar los motores y sensores fuera del dispositivo orientable receptor y/o transmisor de radiacion electromagnetica, y en confiar en los controles mecanicos intermedios, con frecuencia ejes cardanicos rigidos y varillas de conexion, para moverlos. Esto hace que sea posible usar motores relativamente mas grandes con un par torsor elevado, y entonces confiar en la calidad de la construccion y montaje mecanicos para limitar posibles aberraciones. Con esta configuracion, existe una division entre los ejes de rotacion del dispositivo orientable receptor y/o transmisor y los ejes de los motores. La alternativa permite angulos conicos mas amplios y un rendimiento elevado en terminos de aceleracion angular. Sin embargo, las antenas direccionables de la tecnica anterior construidas conforme a esta alternativa, tienen costes elevados, son estructuralmente complejas y requieren ajustes delicados durante el montaje.A different alternative, relatively more generalized than previously described, is to position the motors and sensors outside the orientable receiver and / or electromagnetic radiation transmitter, and to rely on intermediate mechanical controls, often rigid cardan shafts and rods. connection, to move them. This makes it possible to use relatively larger motors with a high torque, and then rely on the quality of mechanical construction and assembly to limit possible aberrations. With this configuration, there is a division between the axes of rotation of the receiver and / or transmitter steerable device and the axes of the motors. The alternative allows wider conic angles and high performance in terms of angular acceleration. However, the addressable antennas of the prior art constructed in accordance with this alternative have high costs, are structurally complex and require delicate adjustments during assembly.

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La tecnica anterior comprende tambien antenas direccionables en las que el sistema electromecanico para mover y soportar la carga util comprende una base, un primer motor (o motor externo) sujeto a la base, una polea de transmision, una transmision por correa que conecta el primer motor y la polea de transmision de modo que esta puede hacerse girar en tono a un primer eje de rotacion (o eje externo), un segundo motor (o motor interno) fijado a la polea de transmision y soportado por la misma y adaptado para hacer que gire la carga util en torno a un segundo eje de rotacion (o eje interno). Los dos ejes estan desacoplados entre si; el movimiento de uno no afecta al otro; algo dificil de conseguir con un sistema de varillas de conexion que en general estan sujetas al mismo elemento de arrastre (antena) a pesar de estar movidas por dos actuadores diferentes. Este tipo de antenas de la tecnica anterior tienen varios inconvenientes, tal como una pobre rigidez transversal, debido esencialmente aunque no exclusivamente, a la presencia de la polea de transmision que tiene una funcion de soporte para la carga util y para el segundo motor. Antenas direccionables de ese tipo con un sistema electromecanico para mover y soportar la carga util, han sido divulgadas en los documentos EP1134839 y US2002/0030631.The prior art also comprises addressable antennas in which the electromechanical system for moving and supporting the useful load comprises a base, a first motor (or external motor) attached to the base, a drive pulley, a belt drive connecting the first the motor and the drive pulley so that it can be rotated in pitch to a first axis of rotation (or external shaft), a second motor (or internal motor) fixed to the drive pulley and supported by it and adapted to do that rotates the useful load around a second axis of rotation (or internal axis). The two axes are decoupled from each other; the movement of one does not affect the other; something difficult to achieve with a system of connection rods that are generally subject to the same drag element (antenna) in spite of being driven by two different actuators. This type of antennas of the prior art have several drawbacks, such as poor transverse stiffness, due essentially, but not exclusively, to the presence of the transmission pulley having a supporting function for the useful load and for the second motor. Such addressable antennas with an electromechanical system for moving and supporting the payload have been disclosed in EP1134839 and US2002 / 0030631.

Un proposito general de la presente descripcion consiste en poner a disposicion una antena direccionable que no tenga los inconvenientes mencionados anteriormente con referencia a la tecnica anterior.A general purpose of the present description is to make available an addressable antenna that does not have the drawbacks mentioned above with reference to the prior art.

Este y otros propositos han sido alcanzados por medio de una antena direccionable segun se define en la primera reivindicacion de una forma mas general, y en las reivindicaciones dependientes en alguna de sus realizaciones particulares.This and other purposes have been achieved by means of an addressable antenna as defined in the first claim in a more general manner, and in the dependent claims in some of its particular embodiments.

La invencion podra ser comprendida de manera mas clara a partir de la descripcion detallada que sigue de sus realizaciones, realizada a titulo de ejemplo no limitativo, con referencia a los dibujos anexos, en los que:The invention may be understood more clearly from the detailed description that follows of its embodiments, carried out by way of non-limiting example, with reference to the attached drawings, in which:

La Figura 1 muestra una seccion transversal parcial y en perspectiva de una porcion de un misil, que comprende un radomo y una antena direccionable;Figure 1 shows a partial and perspective cross section of a portion of a missile, comprising a radome and an addressable antenna;

La Figura 2 muestra una vista en perspectiva de la antena direccionable de la Figura 1;Figure 2 shows a perspective view of the addressable antenna of Figure 1;

La Figura 3 muestra una primera vista, en seccion transversal lateral, de la antena direccionable de la Figura 1;Figure 3 shows a first view, in lateral cross-section, of the addressable antenna of Figure 1;

La Figura 4 muestra una vista en perspectiva de una realizacion de un brazo de soporte de la antena direccionable de la Figura 1;Figure 4 shows a perspective view of an embodiment of an addressable antenna support arm of Figure 1;

La Figura 5 muestra una segunda vista en seccion transversal lateral de la antena direccionable de la Figura 1, en la que el plano de la seccion transversal es perpendicular al plano de la seccion transversal de la vista de la Figura 3, yFigure 5 shows a second side cross-sectional view of the addressable antenna of Figure 1, in which the plane of the cross section is perpendicular to the plane of the cross section of the view of Figure 3, and

La Figura 6 muestra una vista en perspectiva de un detalle a mayor escala de la antena direccionable de la Figura 1.Figure 6 shows a perspective view of an enlarged detail of the addressable antenna of Figure 1.

En los dibujos anexos, los elementos que son iguales o similares van a ser indicados usando los mismos numeros de referencia.In the attached drawings, elements that are the same or similar will be indicated using the same reference numbers.

La Figura 1 muestra una porcion de una realizacion de un misil 1 que comprende un radomo 2 y una antena direccionable 3 montada en el interior del radomo 2. En el ejemplo particular mostrado y sin introducir con ello ninguna limitacion, la antena direccionable 1 es la antena de un radar y mas en particular la antena de un buscador de misil. Se debe apreciar, sin embargo, que las ensenanzas de la presente descripcion son aplicables sin restricciones al tipo particular de antena direccionable dado que la antena direccionable a la que se refiere la presente descripcion podria ser cualquier antena utilizable, por ejemplo, en telecomunicaciones, terrestres o por satelite, y en las industrias de instrumentos de medicion cientificos.Figure 1 shows a portion of an embodiment of a missile 1 comprising a radome 2 and an addressable antenna 3 mounted inside the radome 2. In the particular example shown and without thereby introducing any limitations, the addressable antenna 1 is the antenna of a radar and more in particular the antenna of a missile search engine. It should be appreciated, however, that the teachings of the present disclosure are applicable without restriction to the particular type of addressable antenna since the addressable antenna referred to in the present description could be any antenna usable, for example, in telecommunications, terrestrial or by satellite, and in the industries of scientific measurement instruments.

La antena direccionable 1 comprende una carga util orientable 4, 5. Por ejemplo, la carga util orientable 4, 5 comprende al menos un dispositivo 4 receptor y/o transmisor de radiacion electromagnetica. Por ejemplo, el dispositivo 4 receptor y/o transmisor de radiacion electromagnetica comprende una antena matriz planar, por ejemplo una antena de microondas y de disco que comprende una pluralidad de elementos de antena, tal como elementos de antena de parche o elementos de antena de ranura. Con preferencia, y sin introducir con ello ninguna limitacion, el dispositivo 4 receptor y/o transmisor de radiacion electromagnetica es un dispositivo tanto receptor como transmisor.The addressable antenna 1 comprises a steerable useful load 4, 5. For example, the steerable working load 4, 5 comprises at least one receiver device 4 and / or transmitter of electromagnetic radiation. For example, the electromagnetic radiation receiver and / or transmitting device 4 comprises a planar matrix antenna, for example a microwave and disk antenna comprising a plurality of antenna elements, such as patch antenna elements or antenna elements of groove. Preferably, and without thereby introducing any limitations, the electromagnetic radiation receiver and / or transmitter device 4 is a receiver as well as a transmitter device.

Conforme a una realizacion, la carga util 4,5 comprende ademas una seccion 5 de circuito de procesamiento de las senales transmitidas y/o recibidas por el dispositivo 4 receptor y/o transmisor de radiacion electromagnetica.According to one embodiment, the payload 4,5 further comprises a section 5 of processing circuit of the signals transmitted and / or received by the receiver device 4 and / or transmitter of electromagnetic radiation.

La antena direccionable 1 comprende ademas un sistema electromecanico 6-10 de movimiento y de soporte, conectado operativamente a la carga util 4, 5 y adaptado para orientar la carga util 4,5 de una manera continua.The addressable antenna 1 further comprises an electromechanical system 6-10 of movement and support, operatively connected to the load 4, 5 and adapted to guide the load 4,5 in a continuous manner.

El sistema electromecanico 6-10 de movimiento y soporte comprende una base 6, un primer motor 7 sujeto a la base 6 (o motor externo 6), una polea de transmision 8 conectada operativamente al primer motor 7 para hacerla girar en torno a un primer eje de rotacion (o eje de rotacion externo), un segundo motor 9 (o motor interno) conectado operativamente a la polea de transmision 8 y conectado operativamente a la carga util 4, 5 para hacer que gire la carga util 4, 5 en torno a un segundo eje de rotacion (o eje de rotacion interno). El primer y el segundo ejes deThe electromechanical system 6-10 of movement and support comprises a base 6, a first motor 7 attached to the base 6 (or external motor 6), a transmission pulley 8 operatively connected to the first motor 7 to rotate it around a first rotation shaft (or external rotation shaft), a second motor 9 (or internal motor) operatively connected to the transmission pulley 8 and operatively connected to the load 4, 5 to rotate the useful load 4, 5 around to a second axis of rotation (or axis of internal rotation). The first and second axes of

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rotacion son perpendiculares entre si.rotation are perpendicular to each other.

El sistema electromecanico 6-10 de movimiento y soporte comprende ademas un brazo de soporte 10, por ejemplo segun se muestra en la Figura 3, fijado de forma estable a la base 6, en el que se ha abisagrado pivotantemente el segundo motor 9.The electromechanical system 6-10 of movement and support further comprises a support arm 10, for example as shown in Figure 3, fixed stably to the base 6, in which the second motor 9 has been hinged pivotably.

La polea de transmision 8 esta conectada operativamente al segundo motor 9 para hacer que gire el segundo motor 9 con relacion a la base 6 y con relacion al brazo de soporte 10.The drive pulley 8 is operatively connected to the second motor 9 to cause the second motor 9 to rotate relative to the base 6 and relative to the support arm 10.

Conforme a una realizacion acorde con el ejemplo mostrado en las Figuras, el primer motor 7 esta situado por debajo de la polea de transmision 8 y del brazo de soporte 10, en el lado opuesto a la carga util 4, 5. Entre otras ventajas, esto hace que sea posible, a pesar de la presencia de un potente primer motor y por lo tanto de dimensiones significativas, evitar la obstruccion del movimiento de la carga util 4, 5 y, por ejemplo, optimizar el uso del espacio en el que puede ser movida la carga util en el interior de un radomo.According to an embodiment according to the example shown in the figures, the first motor 7 is located below the transmission pulley 8 and the support arm 10, on the opposite side to the useful load 4, 5. Among other advantages, this makes it possible, in spite of the presence of a powerful first motor and therefore of significant dimensions, to avoid the obstruction of the movement of the useful load 4, 5 and, for example, to optimize the use of the space in which it can be moved the useful load inside a radome.

Con preferencia, el primer motor 7 y el segundo 9 son servomotores.Preferably, the first motor 7 and the second motor 9 are servomotors.

Conforme a una realizacion, la base 6 es un contenedor cilindrico o sustancialmente cilindrico, dotado de una abertura superior 12 y una abertura inferior 13. Con preferencia, la base 6 comprende un alojamiento 14 en cuyo interior se aloja y esta fijado el primer motor 7. Con preferencia, la antena direccionable 1 comprende un circuito 15 de control electronico del primer motor 7, alojado tambien, al menos parcialmente, en el alojamiento 14.According to one embodiment, the base 6 is a cylindrical or substantially cylindrical container, provided with an upper opening 12 and a lower opening 13. Preferably, the base 6 comprises a housing 14 inside which the first motor 7 is housed and fixed. Preferably, the addressable antenna 1 comprises an electronic control circuit 15 of the first motor 7, also housed, at least partially, in the housing 14.

Conforme a una realizacion, la base 6 comprende uno o mas elementos de fijacion 16 adaptados para permitir la sujecion de la base 6 en el interior del radomo 2. Por ejemplo, dichos elementos de fijacion 16 comprenden una pluralidad de rebajes definidos en las paredes laterales externas de la base 6.According to one embodiment, the base 6 comprises one or more fixing elements 16 adapted to allow the base 6 to be held inside the radome 2. For example, said fixing elements 16 comprise a plurality of defined recesses in the side walls external of the base 6.

Conforme a una realizacion, la abertura superior 12 de la base 6 permite el paso de al menos un elemento de transmision del movimiento desde el primer motor 7 hasta la polea de transmision 8.According to one embodiment, the upper opening 12 of the base 6 allows the passage of at least one transmission element of the movement from the first motor 7 to the transmission pulley 8.

Con referencia a la Figura 4, de acuerdo con una realizacion, el brazo de soporte 10 comprende una primera porcion extrema 20, 21 sujeta firmemente a la base 6, y una segunda porcion extrema opuesta 22, 23 a la que esta abisagrado pivotantemente el segundo motor 9. Por ejemplo, la primera porcion extrema 20, 21 esta sujeta a la base por medio de tornillos que cruzan a traves de aberturas proporcionadas en la primera porcion extrema 20, 21 para acoplarse en aberturas correspondientes o en orificios internamente roscados previstos en la pared superior de la base 6.With reference to Figure 4, according to one embodiment, the support arm 10 comprises a first end portion 20, 21 firmly attached to the base 6, and a second opposite end portion 22, 23 to which the second hinged pivotably is 9. For example, the first end portion 20, 21 is fastened to the base by means of screws crossing through openings provided in the first end portion 20, 21 to engage in corresponding openings or in internally threaded holes provided in the upper wall of the base 6.

Con preferencia, el brazo de soporte 10 tiene forma de horquilla, y la citada segunda porcion extrema 22, 23 comprende dos porciones extremas entre las que esta abisagrado pivotantemente dicho segundo motor 9.Preferably, the support arm 10 is fork-shaped, and said second end portion 22, 23 comprises two end portions between which said second motor 9 is hinged pivotably.

De manera mas preferible, la primera porcion extrema 20, 21 mencionada con anterioridad del brazo de soporte 10, comprende al menos un pie de fijacion a la base 6, dotado de una abertura pasante 26 atravesada por la polea de transmision 8 y que no interfiere con la rotacion de la polea de transmision 8. En el ejemplo de la Figura 3, el pie de fijacion 20, 21 anteriormente mencionado comprende dos pies de fijacion 20, 21 que estan separados entre si, y entre los que esta definida la abertura pasante 26 mencionada anteriormente, atravesada por la polea de transmision 8.More preferably, the first end portion 20, 21 mentioned above of the support arm 10, comprises at least one fixing foot to the base 6, provided with a through opening 26 traversed by the transmission pulley 8 and which does not interfere with the rotation of the transmission pulley 8. In the example of Figure 3, the aforementioned fixing foot 20, 21 comprises two fixing feet 20, 21 which are separated from each other, and between which the through opening is defined. 26 mentioned above, traversed by the transmission pulley 8.

Conforme a una realizacion adicional, el brazo de soporte 10 comprende dos brazos de horquilla 24, 25 unidos al pie de fijacion 20, 21 del brazo de soporte 10, y las segundas porciones extremas 22, 23 mencionadas con anterioridad son porciones de extremo libre de dichos brazos de horquilla 24, 25. Con preferencia, cada una de las segundas porciones extremas 22, 23 mencionadas con anterioridad del brazo de soporte 10 comprende una abertura pasante 28, 29 respectiva que tiene una seccion transversal circular. Estas aberturas pasantes 28, 29 definen un eje de bisagra y permiten el abisagramiento pivotante del segundo motor 9 en el brazo de soporte 10.According to a further embodiment, the support arm 10 comprises two fork arms 24, 25 attached to the fixing foot 20, 21 of the support arm 10, and the second end portions 22, 23 mentioned above are free end portions thereof. said fork arms 24, 25. Preferably, each of the second end portions 22, 23 mentioned above of the support arm 10 comprises a respective through-opening 28, 29 having a circular cross-section. These through openings 28, 29 define a hinge axis and allow the pivoting hinge of the second motor 9 on the support arm 10.

Conforme a una realizacion 8, el brazo de soporte 10 comprende un guiaondas 30 integrado en el interior del brazo 10.According to an embodiment 8, the support arm 10 comprises a waveguide 30 integrated inside the arm 10.

Con preferencia, el guiaondas 30 es un canal definido en el espesor del brazo de soporte 10 y dicho brazo 10 esta construido con un material metalico, por ejemplo acero.Preferably, the waveguide 30 is a channel defined in the thickness of the support arm 10 and said arm 10 is constructed of a metal material, for example steel.

Con referencia a la Figura 4, conforme a una realizacion ventajosa, el brazo de soporte 10 comprende dos semi- porciones 26, 27 realizadas en dos piezas separadas y yuxtapuestas y acopladas entre si, por ejemplo mediante tornillos. De esta manera, la realizacion del guiaondas 30 integrado en el brazo de soporte 10 es particularmente facil debido a que el guiaondas 30 puede ser construido mediante la provision de un primer rebaje en una pared de una de las dos semi-porciones 26, 27 previsto de modo que se enfrenta a una pared opuesta de la otra de las dos semi-porciones. De manera clara, se puede proporcionar tambien un segundo rebaje en dicha pared opuesta que se enfrente y se alinee con el primer rebaje cuando las dos semi-porciones 26, 27 estan acopladas entre si.With reference to Figure 4, according to an advantageous embodiment, the support arm 10 comprises two half-portions 26, 27 made in two separate pieces and juxtaposed and coupled together, for example by screws. In this way, the execution of the waveguide 30 integrated in the support arm 10 is particularly easy because the waveguide 30 can be constructed by providing a first recess in a wall of one of the two semi-portions 26, 27 provided so that it faces an opposite wall of the other of the two half-portions. Clearly, a second recess may also be provided in said opposite wall that faces and aligns with the first recess when the two half portions 26, 27 are coupled together.

En caso de que el brazo de soporte 10 tenga forma de horquilla con dos brazos de horquilla 24, 25, el canalIn case the support arm 10 is in the form of a fork with two fork arms 24, 25, the channel

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mencionado con anterioridad tiene preferiblemente una porcion que se extiende por el interior de uno de dichos brazos de horquilla 24, 25. Con preferencia, el canal mencionado con anterioridad se extiende entre dos aberturas del canal desde la primera porcion de extremo 20, 21 del brazo de soporte 10, hasta la segunda porcion de extremo 22, 23 del brazo de soporte 10, con el fin de definir un guiaondas 30 que se extienda desde la base 6 de la antena direccionable 1 hasta la carga util 4, 5. Se puede proporcionar un conector de guiaondas en la base 6 dispuesto en la abertura respectiva del canal.mentioned above preferably has a portion extending inside one of said fork arms 24, 25. Preferably, the aforementioned channel extends between two openings in the channel from the first end portion 20, 21 of the arm of support 10, to the second end portion 22, 23 of the support arm 10, in order to define a waveguide 30 extending from the base 6 of the addressable antenna 1 to the payload 4, 5. It can be provided a waveguide connector in the base 6 disposed in the respective opening of the channel.

Con referencia a la Figura 3, conforme a una realizacion, la antena direccionable 1 comprende una primera junta giratoria en el guiaondas 31 que tiene una porcion de junta sujeta al brazo de soporte 10, en la segunda porcion extrema 22, 23 que esta acoplada operativamente al guiaondas integrado 30 y que esta en comunicacion operativa con el mismo, y una segunda porcion de junta acoplada operativamente a la carga util 4, 5. Con preferencia, el segundo motor 9 esta fijado a la segunda porcion de la junta giratoria en el guiaondas, en el ejemplo mostrado, en la parte exterior del mismo. Con referencia conjunta a las Figuras 3 y 5, en el ejemplo particular representado, la primera junta giratoria en el guiaondas 31esta sujeta al brazo 25 del brazo de soporte 10 y, en particular, encajada en la abertura pasante 29, y por lo tanto permite que el segundo motor 9 este abisagrado pivotantemente al brazo 25 del brazo de soporte 10. En el otro lado del brazo de soporte 10, se ha previsto preferiblemente un perno de bisagra 32 que incluye una porcion con una superficie lisa encajada en el segundo motor 9 y con una porcion roscada atornillada en el interior de la abertura pasante 28 del brazo 24 del brazo de soporte 10.With reference to Figure 3, according to one embodiment, the addressable antenna 1 comprises a first rotary joint in the waveguide 31 having a seal portion attached to the support arm 10, in the second end portion 22, 23 which is operatively coupled to the integrated waveguide 30 and which is in operative communication therewith, and a second gasket portion operatively coupled to the payload 4, 5. Preferably, the second motor 9 is fixed to the second portion of the rotary seal in the waveguide , in the example shown, on the outside of it. With joint reference to Figures 3 and 5, in the particular example shown, the first rotary joint in the waveguide 31 is attached to the arm 25 of the support arm 10 and, in particular, fitted in the through opening 29, and therefore allows that the second motor 9 is pivotally hinged to the arm 25 of the support arm 10. On the other side of the support arm 10, a hinge pin 32 is preferably provided which includes a portion with a smooth surface engaged in the second motor 9. and with a threaded portion screwed into the interior of the through opening 28 of the arm 24 of the support arm 10.

Conforme a una realizacion, el segundo motor 9 comprende un cuerpo contenedor 39, un estator 33 alojado en el interior del cuerpo contenedor 39, un rotor 34 y un eje motriz 35 sujeto, o acoplado, al rotor 33. El cuerpo contenedor 39 esta fijado a la polea de transmision 8 y esta abisagrado pivotantemente al brazo de soporte 10 para que gire en torno al primer eje de rotacion. El eje motriz 35 del segundo motor 9 esta acoplado directa o indirectamente a la carga util 4, 5 por medio de una primera brida de acoplamiento 36. En el ejemplo mostrado en las Figuras, no se ha proporcionado ningun reductor de par torsor, de modo que la brida de acoplamiento 36 esta acoplada directamente al eje motriz 35, por ejemplo enchavetada en el eje motriz 35, y esta acoplada directamente a la carga util 4, 5. En una realizacion alternativa, el acoplamiento mencionado anteriormente puede ser logrado mediante la interposicion de un reductor de par torsor.According to one embodiment, the second motor 9 comprises a container body 39, a stator 33 housed inside the container body 39, a rotor 34 and a drive shaft 35 secured, or coupled, to the rotor 33. The container body 39 is fixed to the drive pulley 8 and hinged pivotably to the support arm 10 to rotate about the first axis of rotation. The drive shaft 35 of the second motor 9 is directly or indirectly coupled to the load 4, 5 by means of a first coupling flange 36. In the example shown in the figures, no torque reducer has been provided, so that the coupling flange 36 is coupled directly to the drive shaft 35, for example keyed to the drive shaft 35, and is directly coupled to the load 4, 5. In an alternative embodiment, the aforementioned coupling can be achieved by interposition of a torque reducer.

Conforme a una realizacion, un transductor 45 de velocidad y/o posicion integral con el eje motriz 35 en su rotacion en torno al segundo eje de rotacion, esta acoplado al eje motriz 35 del segundo motor 9.According to an embodiment, a transducer 45 of speed and / or integral position with the drive shaft 35 in its rotation about the second axis of rotation, is coupled to the drive shaft 35 of the second motor 9.

Conforme a una realizacion, la carga util 4, 5 esta acoplada al contenedor externo 39 del segundo motor 9 por medio de una segunda brida de acoplamiento 37 y de una segunda junta giratoria 41, segun se ha mostrado en la Figura 5. Con preferencia, la segunda junta giratoria 41 y la brida de acoplamiento 37 son dispositivos guiaondas y hacen que sea posible realizar una conexion de guiaondas por medio de un guiaondas de enlace 38, interconectado operativamente entre la primera junta de guiaondas 31 y la segunda junta de guiaondas 41, e integral en cuanto a rotacion con el segundo motor 9.According to one embodiment, the payload 4, 5 is coupled to the external container 39 of the second motor 9 by means of a second coupling flange 37 and a second rotary joint 41, as shown in Figure 5. Preferably, the second rotary joint 41 and the coupling flange 37 are waveguide devices and make it possible to make a waveguide connection by means of a link waveguide 38, operatively interconnected between the first waveguide seal 31 and the second waveguide seal 41, and integral in terms of rotation with the second motor 9.

Con referencia a la Figura 5, conforme a una realizacion, la polea de transmision 8 tiene una porcion central 50 de forma arqueada y dos brazos laterales 41, 42 sujetos al cuerpo contenedor 39 del segundo motor 9. La rotacion de la polea de transmision 8 determina de ese modo una rotacion del cuerpo contenedor 39 del segundo motor 9 en torno al primer eje de rotacion.With reference to Figure 5, according to one embodiment, the transmission pulley 8 has a central portion 50 of arcuate shape and two lateral arms 41, 42 attached to the container body 39 of the second motor 9. The rotation of the transmission pulley 8 In this way, it determines a rotation of the container body 39 of the second motor 9 around the first axis of rotation.

Conforme a una realizacion, el primer motor 7 comprende un cuerpo contenedor 70, un estator 71 alojado en el interior del cuerpo contenedor 70, un rotor 72 y un eje motriz 73 sujeto o acoplado al rotor 72. El cuerpo contenedor 70 esta fijado a la base 6. De acuerdo con una realizacion, un transductor 74 de velocidad y/o posicion esta acoplado al eje motriz 73 del primer motor 7.According to an embodiment, the first motor 7 comprises a container body 70, a stator 71 housed inside the container body 70, a rotor 72 and a drive shaft 73 attached or coupled to the rotor 72. The container body 70 is fixed to the base 6. According to one embodiment, a speed and / or position transducer 74 is coupled to the drive shaft 73 of the first motor 7.

El eje motriz 73 del primer motor 7 esta acoplado con preferencia de forma directa, es decir, sin reductor de par torsor, a la polea de transmision 8.The drive shaft 73 of the first motor 7 is preferably directly coupled, that is, without torque reducer, to the drive pulley 8.

Conforme a la invencion, el sistema electromecanico 6-10 de soporte y movimiento comprende un sistema 18, 19, 48, 49 de transmision por correa, adaptado para acoplar operativamente el primer motor 7 a la polea de transmision 8, que comprende dos correas 18, 19 que se cruzan entre si, que tienen una primera porcion de extremo sujeta a la polea motriz 48, 49, en donde dicho sistema de transmision 18, 19, 48, 49 comprende una polea motriz 48, 49 acoplada al primer motor 7, y en particular a su eje motriz 73. Las correas 18, 19 mencionadas con anterioridad tienen, cada una de ellas, una segunda porcion extrema sujeta a la polea de transmision 8. Con preferencia, las segundas porciones extremas de las correas 18, 19 estan fijadas a porciones extremas opuestas 53, 54 de la porcion central 53, 58 redondeada de la polea de transmision 8.According to the invention, the electromechanical system 6-10 of support and movement comprises a belt transmission system 18, 19, 48, 49, adapted to operatively couple the first motor 7 to the transmission pulley 8, which comprises two belts 18. 19, which intersect each other, having a first end portion subject to the drive pulley 48, 49, wherein said transmission system 18, 19, 48, 49 comprises a drive pulley 48, 49 coupled to the first motor 7, and in particular to its drive shaft 73. The belts 18, 19 mentioned above each have a second end portion attached to the drive pulley 8. Preferably, the second end portions of the belts 18, 19 are fixed to opposite end portions 53, 54 of the rounded central portion 53, 58 of the drive pulley 8.

Conforme a la invencion, las correas 18, 19 mencionadas con anterioridad estan hechas de una aleacion metalica, por ejemplo de una super aleacion, a base de niquel-cromo, de estructura austenitica. Con preferencia, tales correas tienen un espesor reducido, por ejemplo del orden de decimas de milimetro, por ejemplo igual a una decima de milimetro.According to the invention, the belts 18, 19 mentioned above are made of a metal alloy, for example of a super alloy, based on nickel-chromium, of austenitic structure. Preferably, such belts have a reduced thickness, for example in the order of tenths of a millimeter, for example equal to one tenth of a millimeter.

Conforme a la invencion, la polea motriz 48, 49 comprende dos poleas 48, 49 paralelas, unidas entre si por medio deAccording to the invention, the drive pulley 48, 49 comprises two parallel pulleys 48, 49, joined together by means of

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un sistema de acoplamiento que hace que sea posible ajustar la orientacion mutua de dichas poleas 48, 49 para asegurar el correcto pretensado de las correas 18, 19.a coupling system which makes it possible to adjust the mutual orientation of said pulleys 48, 49 to ensure the correct prestressing of the belts 18, 19.

A partir de la descripcion que antecede, resulta evidente la manera en que una antena direccionable 1 del tipo descrito con anterioridad, hace posible conseguir los propositos antes mencionados con referencia al estado de la tecnica anterior.From the foregoing description, it is evident how an addressable antenna 1 of the type described above, makes it possible to achieve the aforementioned purposes with reference to the state of the prior art.

La antena direccionable descrita con anterioridad tiene de hecho una estructura muy compacta y una elevada rigidez transversal. El sistema en su totalidad, de hecho, se desarrolla en torno a un cuerpo central rigido que consiste en el brazo de soporte 10 y la base 6. La realizacion en la que se proporciona un guiaondas integrado en el brazo de soporte 10, parece ser tambien particularmente ventajosa dado que hace que sea posible evitar la provision de un cable de radiofrecuencia que se mueva durante las maniobras de la antena direccionable.The addressable antenna described above has in fact a very compact structure and a high transverse rigidity. The entire system, in fact, is developed around a rigid central body consisting of the support arm 10 and the base 6. The embodiment in which an integrated waveguide is provided on the support arm 10, appears to be also particularly advantageous since it makes it possible to avoid the provision of a radiofrequency cable that moves during maneuvers of the addressable antenna.

Sin perjuicio de los principios de la invencion, las realizaciones y los detalles de construccion pueden ser ampliamente variados con respecto a lo que se ha descrito e ilustrado unicamente a titulo de ejemplo no limitativo, sin apartarse por ello del alcance de la invencion segun se define en las reivindicaciones anexas.Notwithstanding the principles of the invention, the embodiments and construction details may be widely varied with respect to what has been described and illustrated solely by way of non-limiting example, without thereby departing from the scope of the invention as defined. in the appended claims.

Claims (13)

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Five 50fifty REIVINDICACIONES 1. - Antena direccionable (1), que comprende:1. - Addressable antenna (1), comprising: - una carga util (4, 5) orientable;- an adjustable load (4, 5); - un sistema electromecanico (6-10) de movimiento y soporte, conectado operativamente a la carga util (4, 5) y adaptado para orientar la carga util de una manera controlada, comprendiendo dicho sistema electromecanico una base (6), un primer motor (7) sujeto a la base (6), una polea de transmision (8) conectada operativamente al primer motor (7) para hacer que gire en torno a un primer eje de rotacion, un segundo motor (9) conectado operativamente a la polea de transmision (8) y conectado operativamente a la carga util (4, 5) para hacer que gire la carga util en torno a un segundo eje de rotacion;- an electromechanical system (6-10) of movement and support, operatively connected to the useful load (4, 5) and adapted to guide the useful load in a controlled manner, said electromechanical system comprising a base (6), a first motor (7) attached to the base (6), a transmission pulley (8) operatively connected to the first motor (7) to cause it to rotate about a first axis of rotation, a second motor (9) operatively connected to the pulley of transmission (8) and operatively connected to the useful load (4, 5) to cause the useful load to rotate about a second axis of rotation; en donde el sistema electromecanico (6-10) de movimiento y soporte comprende ademas un brazo de soporte (10) integral con la base (6), al que esta abisagrado pivotantemente el segundo motor (9) y la polea de transmision (8) esta conectada operativamente al segundo motor (9) para hacer que gire el segundo motor (9) con relacion a la base (6) y con relacion al brazo de soporte (10);wherein the electromechanical system (6-10) of movement and support further comprises a support arm (10) integral with the base (6), to which the second motor (9) and the drive pulley (8) are hinged pivotably is operatively connected to the second motor (9) to cause the second motor (9) to rotate relative to the base (6) and relative to the support arm (10); en donde el sistema electromecanico (6-10) de movimiento y soporte comprende un sistema (18, 19, 48, 49) de transmision por correa adaptado para acoplar operativamente el primer motor (7) a la polea de transmision (8), comprendiendo dicho sistema de transmision una polea motriz (48, 49) acoplada al primer motor (7);wherein the electromechanical system (6-10) of movement and support comprises a belt transmission system (18, 19, 48, 49) adapted to operatively couple the first motor (7) to the transmission pulley (8), comprising said transmission system a drive pulley (48, 49) coupled to the first motor (7); caracterizada porque dicho sistema (18, 19, 48, 49) de transmision por correa comprende dos correas (18, 19) cruzadas que tienen una primera porcion de extremo sujeta a dicha polea motriz (48, 49), en donde dichas correas (8, 19) estan fabricadas con una aleacion metalica y cada una de ellas tiene una segunda porcion de extremo sujeta a dicha polea de transmision (8), en donde la polea motriz (48, 49) comprende dos poleas (48, 49) paralelas, unidas entre si por medio de un sistema de acoplamiento que permite el ajuste de la orientacion reciproca de dichas poleas (48, 49) paralelas.characterized in that said belt transmission system (18, 19, 48, 49) comprises two crossed belts (18, 19) having a first end portion secured to said drive pulley (48, 49), wherein said belts (8, 19). , 19) are made with a metal alloy and each of them has a second end portion attached to said drive pulley (8), wherein the drive pulley (48, 49) comprises two parallel pulleys (48, 49), joined together by means of a coupling system that allows the adjustment of the reciprocal orientation of said parallel pulleys (48, 49). 2. - Antena direccionable (1) segun la reivindicacion 1, en donde dicho brazo de soporte (10) comprende una primera porcion de extremo (20, 21) fijada a la base (6), y una segunda porcion de extremo (22, 23) a la que esta abisagrado pivotantemente el segundo motor (9).2. - Addressable antenna (1) according to claim 1, wherein said support arm (10) comprises a first end portion (20, 21) fixed to the base (6), and a second end portion (22, 23) to which the second motor (9) is hinged pivotably. 3. - Antena direccionable (1) segun la reivindicacion 2, en donde dicho brazo de soporte (10) tiene forma de horquilla, y en donde dicha segunda porcion de extremo (22, 23) comprende dos porciones extremas entre las que esta abisagrado pivotantemente dicho segundo motor (9).3. - Addressable antenna (1) according to claim 2, wherein said support arm (10) is fork-shaped, and wherein said second end portion (22, 23) comprises two end portions between which hinged pivotingly said second motor (9). 4. - Antena direccionable (1) segun la reivindicacion 3, en donde dicha primera porcion de extremo (20, 21) del brazo de soporte (10) comprende un pie de fijacion a la base (6), dotado de una abertura pasante (26) atravesada por la polea de transmision (8).4. - Addressable antenna (1) according to claim 3, wherein said first end portion (20, 21) of the support arm (10) comprises a base fixing foot (6), provided with a through opening ( 26) traversed by the transmission pulley (8). 5. - Antena direccionable (1) segun la reivindicacion 4, en donde dicho pie de fijacion (20, 21) comprende dos pies de fijacion separados, entre los que esta definida la citada abertura pasante (26).5. - Addressable antenna (1) according to claim 4, wherein said fixing foot (20, 21) comprises two separate fixing feet, between which said through-opening (26) is defined. 6. - Antena direccionable (1) segun la reivindicacion 4 o 5, que comprende dos brazos de horquilla (24, 25) sujetos al pie de fijacion (20, 21), y en donde dichas dos porciones de extremo (22, 23) son porciones extremas libres de dichos brazos de horquilla (24, 25).6. - Addressable antenna (1) according to claim 4 or 5, comprising two fork arms (24, 25) attached to the fixing foot (20, 21), and wherein said two end portions (22, 23) they are free end portions of said fork arms (24, 25). 7. - Antena direccionable (1) segun cualquiera de las reivindicaciones anteriores, en donde la carga util (4, 5) comprende un dispositivo (4) de transmision y/o recepcion de radiacion electromagnetica.7. - Addressable antenna (1) according to any of the preceding claims, wherein the payload (4, 5) comprises a device (4) for transmission and / or reception of electromagnetic radiation. 8. - Antena direccionable segun la reivindicacion 1, en donde el primer motor (7) esta posicionado por debajo de la polea de transmision (8) y del brazo de soporte (10) en el lado opuesto a la carga util (4, 5).8. - Addressable antenna according to claim 1, wherein the first motor (7) is positioned below the drive pulley (8) and the support arm (10) on the side opposite the load (4, 5). ). 9. - Antena direccionable (1) segun la reivindicacion 1, en donde el brazo de soporte (10) comprende un guiaondas integrado (30).9. - Addressable antenna (1) according to claim 1, wherein the support arm (10) comprises an integrated waveguide (30). 10. - Antena direccionable (1) segun la reivindicacion 9, en donde dicho guiaondas integrado (30) es un canal definido en el espesor del brazo de soporte (10), y en donde dicho canal tiene una porcion que se extiende por el interior de uno de dichos brazos de horquilla (24, 25).10. - Addressable antenna (1) according to claim 9, wherein said integrated waveguide (30) is a channel defined in the thickness of the support arm (10), and wherein said channel has a portion extending in the interior of one of said fork arms (24, 25). 11. - Antena direccionable (1) segun cualquiera de las reivindicaciones anteriores, en donde el segundo motor (9) comprende un cuerpo contenedor (39), un estator (33) alojado en el interior de dicho cuerpo contenedor (39), un rotor (34) y un eje motriz (35) sujeto o acoplado al rotor (34), y en donde el cuerpo contenedor (39) esta sujeto a la polea de transmision (8) y esta abisagrado pivotantemente al brazo de soporte (10) de modo que esta capacitado para girar en torno a dicho primer eje de rotacion.11. - Addressable antenna (1) according to any of the preceding claims, wherein the second motor (9) comprises a container body (39), a stator (33) housed inside said container body (39), a rotor (34) and a drive shaft (35) attached or coupled to the rotor (34), and wherein the container body (39) is attached to the drive pulley (8) and hinged pivotally to the support arm (10) of so that it is capable of rotating around said first axis of rotation. 55 1010 15fifteen 20twenty 2525 3030 12. - Antena direccionable (1) segun la reivindicacion 11, en donde la polea de transmision (8) tiene una porcion central (50) de forma arqueada, y dos brazos laterales (51, 52) fijados al cuerpo contenedor (39) del segundo motor (9).12. - Addressable antenna (1) according to claim 11, wherein the transmission pulley (8) has a central portion (50) of arched shape, and two side arms (51, 52) fixed to the container body (39) of the second motor (9). 13. - Buscador que comprende una antena direccionable (1) segun cualquiera de las reivindicaciones anteriores.13. - Search engine comprising an addressable antenna (1) according to any of the preceding claims.
ES14198496.3T 2013-12-18 2014-12-17 Addressable antenna Active ES2694245T3 (en)

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FR3055050B1 (en) * 2016-08-11 2019-11-22 Thales SELF-CONTROLLED RADAR FOR SELF-ADHESIVE GUIDANCE OF A PLATFORM AND AUTOGUID MISSILE COMPRISING SUCH RADAR
CN108682955B (en) * 2018-05-11 2020-12-29 山东天元信息技术集团有限公司 Integrated terminal antenna based on Beidou navigation technology
IT202100013952A1 (en) 2021-05-28 2022-11-28 Mbda italia spa Method and system for electronically controlling the movement of a power-assisted device for receiving and/or transmitting and/or reflecting electromagnetic radiation
IT202100032696A1 (en) 2021-12-27 2023-06-27 Mbda italia spa Electronic control unit of a servo-assisted device for receiving and/or transmitting and/or reflecting electromagnetic radiation

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