Patent Application
20240136716
The invention relates to an antenna array being attachable to a surface, an antenna system being attachable to a surface, and an antenna kit being attachable to a surface.
Generally, in times of an increasing number of communication applications providing wireless connectivity possibilities, there is a growing need of an antenna array, antenna system and antenna kit, each being attachable to a surface, for performing measurements with respect to such applications in order to verify their correct functioning in an efficient and accurate manner, whereby a high flexibility is ensured with special respect to different measurement purposes.
In this context of performing measurements, it is exemplarily noted that with special respect to antennas or antenna arrays, respectively, mounted to a vehicle, such as a car or an aircraft, which are employed for network and/or spectrum monitoring, the corresponding capabilities cannot be extended, and thus, disadvantageously, said antennas cannot flexibly be used in different measurement scenarios. There are no antennas or antenna arrays, respectively, known, which allow for different configurations depending on the corresponding measurement scenario, and thus would ensure a high accuracy, efficiency, and flexibility.
Accordingly, there is the object to provide an antenna array, antenna system and antenna kit, each being attachable to a surface, in order to allow for performing measurements, especially measurements regarding wireless connectivity capabilities, in a flexible manner, thereby ensuring a high accuracy and efficiency of the measurement.
According to a first aspect of the invention, an antenna array being attachable to a surface is provided. Said antenna array comprises at least two antennas, and a magnetic material and/or an alloy with ferro-magnetic properties for magnetically attaching at least one further antenna. Advantageously, this allows for different configurations depending on the corresponding measurement scenario, thereby ensuring a particularly high flexibility, efficiency, and accuracy. Further advantageously, a lower profile directional capability can be achieved in an efficient manner.
According to a first preferred implementation form of the first aspect of the invention, the at least one further antenna comprises or is at least one further antenna array, especially at least one further directional antenna array.
Advantageously, for instance, by stacking at least two antenna arrays, capabilities of car or aircraft mounted antennas for network and/or spectrum monitoring can be extended in an efficient and flexible manner.
According to a second preferred implementation form of the first aspect of the invention, the at least one further antenna comprises a further magnetic material and/or a further alloy with ferro-magnetic properties.
Advantageously, for example, a secure but also easily detachable attachment of the at least one further antenna can be achieved.
According to a further preferred implementation form of the first aspect of the invention, the surface is at least part of, especially at least part of the corresponding skin of, a car, a tank, a helicopter, an airplane, or a streetlamp. Advantageously, for instance, the antenna array can efficiently be mounted to a vehicle in the context of network and/or spectrum monitoring.
According to a further preferred implementation form of the first aspect of the invention, the antenna array further comprises a centering unit, especially a centering peg and/or a centering indentation, for axially arranging the at least one further antenna with respect to the antenna array. Advantageously, for example, with respect to the antenna array and the at least one further antenna, the same center can efficiently be achieved especially for the purpose of similar time of arrival.
According to a further preferred implementation form of the first aspect of the invention, the at least one further antenna comprises a further centering unit, especially a further centering peg and/or a further centering indentation, for axially arranging the at least one further antenna with respect to the antenna array. Advantageously, for instance, such an axial arrangement allows for a similar time of arrival.
According to a further preferred implementation form of the first aspect of the invention, the magnetic material and/or the alloy with ferro-magnetic properties is fixed to the antenna array such that the at least one further antenna is located opposite to the surface in the case that the at least one further antenna is magnetically attached. Advantageously, for example, the antenna array has not be detached from the surface when the at least one further antenna is to be attached or exchanged.
According to a further preferred implementation form of the first aspect of the invention, an operational frequency range of the antenna array is lower than a further operational frequency range of the at least one further antenna. Advantageously, for instance, a lower frequency directional antenna array can be mounted directly on a vehicle.
According to a further preferred implementation form of the first aspect of the invention, the antenna array comprises or is a directional antenna array especially with an operational frequency range of 0.6 GHz to 8 GHz. Advantageously, for example, it is noted that an operational frequency range of 0.6 GHz to 18 GHz is also possible.
According to a further preferred implementation form of the first aspect of the invention, the magnetic material and/or the alloy with ferro-magnetic properties is of circular or annular shape. Advantageously, for instance, a symmetrical, and thus secure and efficient, attachment of the at least one further antenna can be achieved.
According to a further preferred implementation form of the first aspect of the invention, the alloy with ferro-magnetic properties comprises or is an iron ring or a steel ring. Advantageously, for example, cost-efficiency can be increased.
According to a further preferred implementation form of the first aspect of the invention, the at least one further antenna comprises or is an omnidirectional antenna or a Global Positioning System (GPS) antenna. Advantageously, for instance, flexibility can be increased.
According to a further preferred implementation form of the first aspect of the invention, the at least one further antenna comprises or is a directional antenna array with a further operational frequency range of 17 GHz to 44 GHz. Advantageously, for example, a further operational frequency range of 4.5 GHz to 53 GHz can also be possible.
According to a further preferred implementation form of the first aspect of the invention, the antenna array comprises a hole for cable routing from the at least one further antenna. Advantageously, for instance, cable routing can be achieved in a cost-efficient manner.
According to a further preferred implementation form of the first aspect of the invention, the hole is located in the center of the antenna array. Advantageously, for example, a low interference cable routing can efficiently be achieved.
According to a further preferred implementation form of the first aspect of the invention, at least one cable from the at least one further antenna is routed in such a manner as to not interfere with the antenna array. Advantageously, for instance, the antenna array can comprise a cost-efficient cable inset.
According to a further preferred implementation form of the first aspect of the invention, the magnetic material comprises or is an embedded magnet. In addition to this or as an alternative, the alloy with ferro-magnetic properties comprises or is an embedded ferro-metal. Advantageously, for example, complexity can be reduced, thereby further increasing efficiency.
According to a further preferred implementation form of the first aspect of the invention, the magnetic material and/or the alloy with ferro-magnetic properties is fixed to the antenna array by glue. Advantageously, for instance, a simple, and thus cost-efficient, fixing can be achieved.
According to a second aspect of the invention, an antenna system being attachable to a surface is provided. Said antenna system comprises an antenna array according to the first aspect of the invention or any of its preferred implementation forms, respectively, and at least one further antenna being magnetically attached to the antenna array. Advantageously, this allows for different configurations depending on the corresponding measurement scenario, thereby ensuring a particularly high flexibility, efficiency, and accuracy. Further advantageously, a lower profile directional capability can be achieved in an efficient manner.
According to a third aspect of the invention, an antenna kit being attachable to a surface is provided. Said antenna kit comprises an antenna array according to the first aspect of the invention or any of its preferred implementation forms, respectively, and at least one further antenna being magnetically attachable to the antenna array.
Advantageously, this allows for different configurations depending on the corresponding measurement scenario, thereby ensuring a particularly high flexibility, efficiency, and accuracy. Further advantageously, a lower profile directional capability can be achieved in an efficient manner.
Exemplary embodiments of the invention are now further explained with respect to the drawings by way of example only, and not for limitation. In the drawings:
Firstly,
In accordance with
It is noted that said at least one further antenna can be further antenna array, especially at least one further directional antenna array.
It is further noted that the antenna array 10 can also be a directional antenna array.
It might be particularly advantageous if the at least one further antenna or the further antenna array, respectively, comprises a further magnetic material and/or a further alloy with ferro-magnetic properties.
With respect to the surface, to which the antenna array 10 is attachable, it is note that said surface can be at least part of, especially at least part of the corresponding skin of, a car, a tank, a helicopter, an airplane, or a street lamp.
In this context, it is mentioned that the antenna array 10 exemplarily comprises a first surface 16a for attaching the antenna array 10 to the above-mentioned surface which is not explicitly shown. Said first surface 16a can be attached to the surface, for instance, in a magnetic manner or by gluing, screwing, nailing, or the like.
As it can further be seen from
In this context, it might be particularly advantageous if the at least one further antenna or the further antenna array, respectively, comprises a further centering unit, exemplarily a further centering peg, for axially arranging the at least one further antenna or the further antenna array, respectively, with respect to the antenna array 10.
Furthermore, the magnetic material and/or the alloy with ferro-magnetic properties, exemplarily equipped with reference sign 15, is fixed to the antenna array 10 such that the at least one further antenna or the further antenna array, respectively, is located opposite to the surface in the case that the at least one further antenna or the further antenna array, respectively, is magnetically attached.
In this context, it is mentioned that the antenna array 10 exemplarily comprises a second surface 16b opposite to the above-mentioned first surface 16a. Moreover, said second surface 16b comprises the magnetic material and/or the alloy with ferro-magnetic properties, exemplarily equipped with reference sign 15, or said magnetic material and/or the alloy with ferro-magnetic properties is fixed to the second surface 16b, respectively.
It is additionally noted that the term “opposite” can especially be understood in a manner that each of at least one pair out of respective normals to the surface, the first surface 16a, and the second surface 16b, deviate not more than 10 degrees, preferably 5 degrees, more preferably 2 degrees, most preferably 0.5 degrees, from a certain direction.
Furthermore, an operational frequency range of the antenna array 10 is lower than a further operational frequency range of the at least one further antenna or the further antenna array, respectively.
Moreover, the antenna array 10 can comprise or be a directional antenna array exemplarily with an operational frequency range of 0.6 GHz to 18 GHz.
As it can further be seen from
It is noted that it might be particularly advantageous if the antenna array 10 comprises a hole for cable routing from the at least one further antenna. Further advantageously, said hole can be located in the center of the antenna array 10.
In this exemplary case according to
Said cable inset 18, especially in the sense of the length thereof, is substantially perpendicular to at least one of the surface, the first surface 16a, and the second surface 16b. Furthermore, said cable inset 18 may preferably be arranged in the vicinity of the housing of the antenna array. More preferably, the cable inset 18 may be arranged such that said cable inset 18 is located as far as possible from the center of the antenna array 10.
It is noted that the term “substantially perpendicular” is especially to be understood as an angle between 80 degrees and 100 degrees, preferably between 85 degrees and 95 degrees, more preferably between 88 degrees and 92 degrees, most preferably between 89.5 degrees and 90.5 degrees.
It is further noted that the antenna array 10 comprises at least one cable, especially at least one radio frequency cable, exemplarily four radio frequency cables.
Furthermore, the antenna array 10, especially each of the first surface 16a and the second surface 16b, is of a circular shape.
It is noted that a diameter of said circular shape can be between 18 cm and 26 cm, preferably between 20 cm and 24 cm, more preferably between 21 cm and 23 cm, most preferably between 21.5 cm and 22.5 cm.
Moreover, a height of the antenna array 10, especially in the sense of a distance between the first surface 16a and the second surface 16b, can be between 6 cm and 14 cm, preferably between 8 cm and 12 cm, more preferably between 9 cm and 11 cm, most preferably between 9.5 cm and 10.5 cm.
Now, with respect to
Said antenna system comprises the antenna array 10 according to
It is noted that the explanations above regarding the at least one further antenna or the further antenna array, respectively, can analogously apply for the omnidirectional antenna 21.
As it can further be seen from
It is noted that the omnidirectional antenna 21 can alternatively be a Global Positioning System (GPS) antenna.
In accordance with
Said antenna system comprises the antenna array 10 according to
It is noted that the explanations above regarding the at least one further antenna or the further antenna array, respectively, can analogously apply for the omnidirectional antenna 22.
As it can further be seen from
It is noted that the omnidirectional antenna 22 can alternatively be a GPS antenna.
Furthermore,
Said antenna system comprises the antenna array 10 according to
It is noted that the explanations above regarding the at least one further antenna or the further antenna array, respectively, can analogously apply for the omnidirectional antenna 23.
As it can further be seen from
It is noted that the omnidirectional antenna 23 can alternatively be a GPS antenna.
Now, with respect to
Said antenna system comprises the antenna array 10 according to
It is noted that the explanations above regarding the at least one further antenna or the further antenna array, respectively, can analogously apply for the directional antenna array 24.
As it can further be seen from
It is noted that it might be particularly advantageous if the antenna array 24 is of the same type as the antenna array 10.
It is further noted that a diameter of the antenna array 24 may be at least 20 percent, preferably at least 30 percent, more preferably at least 45 percent, most preferably at least 50 percent, smaller than the diameter of the antenna array 10.
Moreover, with respect to the antenna array 10, the above-mentioned omnidirectional antennas 21, 22, 23, and the above-mentioned directional antenna array 24, it is noted that the antenna array 10 and at least a part of said omnidirectional antennas 21, 22, 23, and said directional antenna array 24 can form an antenna kit according to the third aspect of the invention.
Furthermore,
Said antenna array 10a comprises a monocone feed 11a for inputting an input signal and/or outputting an output signal, and a reflecting surface 12a comprising a parabolic shape for transmitting the input signal as an electromagnetic output wave and/or receiving an electromagnetic input wave as the output signal.
As it can further be seen from
It is noted that the reflecting surface 12 and said two planar surfaces 16a′, 16b′ especially form a cavity. Preferably, the above-mentioned monocone feed 11a is located inside said cavity.
Moreover, the antenna array 10a further comprises at least one further monocone feed, exemplarily three further monocone feeds 11b, 11c, 11d for inputting the input signal and/or outputting the output signal and/or for inputting a further input signal and/or outputting a further output signal, and at least one further reflecting surface, exemplarily three further reflecting surfaces 12b, 12c, 12d, each comprising a further parabolic shape for transmitting the input signal as the electromagnetic output wave and/or receiving the electromagnetic input wave as the output signal and/or for transmitting the further input signal as a further electromagnetic output wave and/or receiving a further electromagnetic input wave as the further output signal.
It is noted that the explanations above, especially regarding the monocone feed 11a and the reflecting surface 12a, can analogously be applied for at least one, preferably each, of said further monocone feeds 11b, 11c, 11d and said further reflecting surfaces 12b, 12c, 12d.
It is further noted that it might be particularly advantageous if the monocone feed 11a, the reflecting surface 12a, the at least one further monocone feed, exemplarily the three further monocone feeds 11b, 11c, 11d, and the at least one further reflecting surface, exemplarily the three further reflecting surfaces 12b, 12c, 12d, are arranged to form a directional array, especially a switched directional array.
As it can further be seen from
In addition to this, the planar surfaces 16a′, 16b′, to which the above-mentioned corresponding explanations especially apply in an analogous manner, are of circular shape and/or of the same size.
It is further noted that the monocone feed 11a and the three further monocone feeds 11b, 11c, 11d substantially form the corners of an imaginary square. In other words, an angle between two neighboring ones of said monocone feeds 11a, 11b, 11c, 11d is between 80 degrees and 100 degrees, preferably between 85 degrees and 95 degrees, more preferably between 88 degrees and 92 degrees, most preferably between 89.5 degrees and 90.5 degrees.
With respect the antenna array 10a of
With respect to the above-mentioned vicinity, it is noted that said vicinity may preferably refer to the corresponding volume of the above-mentioned cavity.
Finally, it is noted that the number of monocone feeds, such as the above-mentioned monocone feeds 11a, 11b, 11c, 11d of
For instance, in accordance with
While various embodiments of the present invention have been described above, it should be understood that they have been presented by way of example only, and not limitation. Numerous changes to the disclosed embodiments can be made in accordance with the disclosure herein without departing from the spirit or scope of the invention. Thus, the breadth and scope of the present invention should not be limited by any of the above described embodiments. Rather, the scope of the invention should be defined in accordance with the following claims and their equivalents.
Although the invention has been illustrated and described with respect to one or more implementations, equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification and the annexed drawings. In addition, while a particular feature of the invention may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular application.
