Patent Grant
10426021
This application claims priority to German patent application DE 10 2016 008 945.8 filed Jul. 26, 2016, the entire disclosure of which is incorporated by reference herein.
Various embodiments generally relate to a microelectronic module for altering the electromagnetic signature of a surface, and a module array and a method for altering the electromagnetic signature of a surface.
The development of modern vehicles, for example modern aircraft, is tending more and more toward reducing discoverability by enemy radar, for example. By way of example, this is achieved by so-called stealth technology. In this case, inter alia, the geometric shape of a vehicle, such as, for example, a ship, a land vehicle or an aircraft, is optimized to the effect that the vehicle for example on an enemy radar screen appears significantly smaller or is represented at a different position or in a delayed manner. However, such geometric optimizations have the disadvantage, for example, that often they only act passively and are not adaptable to the respective situation.
Taking this as a departure point, it is an object of the disclosure herein to specify a device which avoids the disadvantages mentioned above.
This object is achieved by a device having the features herein and by a method having the features herein. Exemplary embodiments are presented in the dependent claims. It should be pointed out that the features of the exemplary embodiments of the devices also apply to embodiments of the method, and vice versa.
A microelectronic module for altering the electromagnetic signature of a surface is specified. The microelectronic module comprises at least one voltage converter for converting a first voltage provided into a higher, lower or identical second voltage. Furthermore, the microelectronic module comprises at least one actuator. The actuator comprises at least one generator for generating an electrical plasma from the second voltage provided by the voltage converter. At least the voltage converter and the actuator are arranged on a thin-layered planar substrate. The electrical plasma generated by the actuator interacts with an electromagnetic radiation impinging on the surface, as a result of which the electromagnetic signature is altered.
The disclosure herein is based on the concept of altering the electromagnetic signature of a surface by generating an electrical plasma that interacts with an electromagnetic radiation impinging on the surface. In this case, the electrical plasma can be generated depending on the electromagnetic radiation impinging on the surface and the electromagnetic signature of a surface can thereby be altered. The electromagnetic signature emitted by the surface, as a result of the interaction with the electrical plasma, is preferably altered relative to an electromagnetic signature reflected back without being influenced, i.e. for example the radar cross section of a vehicle appears altered, preferably reduced, on a radar screen, for example, as a result. Consequently, by way of example, the electromagnetic signature can adapt actively to the respective situation.
The designation “actuator” can be understood as any type of device which is suitable for converting an electrical signal into some other physical variable.
The designation “voltage converter” can be understood as any electrical element which is able to convert an input voltage into a higher, lower or identical output voltage. For the case where the input voltage corresponds to the output voltage, the electrical element can also consist just of an electrical connection element.
In accordance with one preferred embodiment, the microelectronic module furthermore comprises at least one detection unit. The detection unit comprises at least one sensor for detecting an electromagnetic radiation impinging on the surface. The sensor can be suitable, for example, for detecting electromagnetic interactions of photons impinging on the sensor with the electrons or atomic nuclei of a detector material of the sensor.
In accordance with one preferred embodiment, the microelectronic module furthermore comprises a control unit. The control unit is configured for controlling the generation of the electrical plasma depending on a signal from the detection unit, a receiver, control commands of a superordinate transmitting and/or control element, and/or information from at least one further conventional sensor, an antenna and/or a control or regulating system. The receiver is configured for receiving external data, containing information about the detection of the electromagnetic radiation impinging on the surface. The microelectronic module can thus be controlled in a targeted manner in accordance with the detected electromagnetic radiation in order to alter the electromagnetic signature of a surface.
In accordance with one preferred embodiment, the actuator is furthermore configured to detect the electromagnetic radiation impinging on the surface. As an alternative to external sensors, the actuator itself can also be able to detect the electromagnetic radiation impinging on the surface. This has the advantage that no further detectors or sensors are required, or the detection can be improved by combination with further detectors or sensors.
In accordance with one preferred embodiment, the electrical plasma is generated depending on the detected electromagnetic radiation and/or the received data about the electromagnetic radiation impinging on the surface. In a manner dependent on the detected electromagnetic radiation and/or the received data about the electromagnetic radiation impinging on the surface, the electrical plasma is generated. This has the advantage that the generation of the electrical plasma can be adapted to the requirements.
In accordance with one preferred embodiment, the electromagnetic signature of the surface is altered by absorbing and/or reflecting an outer wave of the electromagnetic radiation. By reducing the backscattering of the electromagnetic radiation and/or by damping the surface wave of the electromagnetic radiation, it is possible to alter for example the absorption and/or reflection of the electromagnetic radiation. Alternatively, the electromagnetic signature of the surface can also be altered for example by a combination of the above-described absorption and/or reflection with, for example, a conventional RAM (radar-absorbing material) coating or other radar-absorbing materials or else an infrared camouflage. This has the advantage that, for example, the radar-absorbing properties of a RAM coating can be improved.
In accordance with one preferred embodiment, a frequency-selective surface is generated with the aid of the at least one actuator. By the driving of the at least one actuator, distributed or periodically conductive plasma structures are generatable preferably on, in or below the surface. The generated plasma preferably has a specific frequency band. The width of the frequency band and/or the center frequency are/is preferably controllable by an applied magnetic field. Preferably, an active metamaterial is formed by the influencing of the generated plasma. The active metamaterial is usable for example as band-pass filter, band-stop filter, high-pass filter, low-pass filter or a combination thereof, for altering the electromagnetic waves. This has the advantage that the electromagnetic radiation can be altered in a targeted manner in order thereby to falsify the radar image, for example.
In accordance with one preferred embodiment, the thin-layered planar substrate is a flexible and/or multidimensionally deformable film or lattice. By way of example, the lattice can have a flexible and/or multidimensionally deformable lattice structure. The thin-layered planar substrate can alternatively also consist of a comparable material which is suited to enabling the components of the module to be applied, introduced or fitted thereon and which is as thin as possible and stable enough. By way of example, the substrate can also comprise a fabric, a lattice structure or a composite material. This has the advantage that the module can be kept small in terms of its geometric dimensions, a sufficient stability being provided to apply, for example to adhesively bond, the module permanently or reversibly on a surface, for example.
In accordance with one preferred embodiment, the module comprises a plurality of actuators. The plurality of actuators preferably have a different and/or identical orientation. This has the advantage that the electromagnetic radiation impinging on the module from different directions, for example, can be altered in a targeted manner.
In accordance with one preferred embodiment, the module comprises at least one switching element for activating and/or deactivating the module and/or at least one of the plurality of actuators. This has the advantage that the one individual module itself, or one module or two or more modules from a plurality of modules can be activated and/or deactivated in a targeted manner.
The designation “switching element” can be understood as any type of device which is suitable for altering a connection from an interrupted state to a connected state. This can also be understood to mean a connection which is open at one end and which can be closed permanently or reversibly for example by connecting the module to, for example, an electronic unit for control.
In accordance with one preferred embodiment, an antenna that is freely definable on the surface or an antenna array for adapting antenna gain, polarization and receiving direction can be formed by the actuators.
In accordance with one preferred embodiment, the antenna or the antenna array is usable as transmitting and/or receiving antenna for electromagnetic radiation. This has the advantage that the antenna or the antenna array, if necessary, can be used for sending and/or receiving data. This has the advantage that the module is also usable as receiving and/or transmitting antenna.
In accordance with one preferred embodiment, the transmitting and/or receiving antenna can be coupled to an external transmitter and/or receiver via a coupling-in and/or coupling-out device. This has the advantage that the antenna or the antenna array, which can be embodied as transmitting and/or receiving antenna, for example, is connectable to an external transmitter and/or receiver. As a result, for example, data can be sent by the external transmitter via the antenna, embodied as transmitting antenna, or the antenna array and/or data can be received by the external receiver via the antenna, embodied as receiving antenna, or the antenna array.
In accordance with one preferred embodiment, the voltage converter, the switching element, the actuator, the detection unit, the sensor, the receiver, the transmitter and/or the control element are/is embodied as MEMS (MicroElectroMechanical System) structure. Alternatively, the voltage converter, the switching element, the actuator, the detection unit, the sensor, the receiver, the transmitter and/or the control element can also be embodied as a nanoelectromechanical system. Further advantageous components of the module, insofar as is advantageous and applicable, can also be embodied for example as MEMS structure or as a nanoelectromechanical system. This has the advantage that the module and the components thereof can be kept very small in terms of dimensions. The space required for the module can thus be reduced to a minimum, for example.
Furthermore, a module array, comprising a plurality of microelectronic modules described above, is specified. By virtue of the arrangement of a plurality of the modules in an array, the alteration of the electromagnetic signature of a surface can be intensified and/or be used with targeted orientation.
In accordance with one preferred embodiment, it is also possible to arrange a plurality of microelectronic modules on a common thin-layered planar substrate. This has the advantage that, for example, the application of the module on a surface can be facilitated, or accelerated, as a result of which the costs for mounting can be reduced.
In accordance with one preferred embodiment, the actuators of the plurality of modules are drivable in a time-staggered and/or phase-shifted manner. The intensity can be influenced for example by utilization of interference phenomena. A time-staggered and/or phase-shifted driving of the actuators makes it possible to utilize interference phenomena in the generation of the electrical plasma in a targeted manner.
In accordance with one preferred embodiment, the module array comprises one or a plurality of switching elements configured to activate and/or to deactivate one or a plurality of actuators of the module array. This has the advantage that the module array can be controlled individually and the geometric dimensions can be kept small depending on the application.
Furthermore, an arrangement of at least one above-described microelectronic module or of at least one above-described module array on and/or in a surface of a vehicle is specified.
In accordance with one preferred embodiment, the surface has a coating that at least partly absorbs an electromagnetic radiation impinging on the surface. The coating can consist of a RAM material, for example.
In accordance with one preferred embodiment, the vehicle is an aircraft, a watercraft, or a land vehicle. By virtue of the arrangement of at least one module or of at least one module array, the electromagnetic signature can be altered, such that, for example, the electromagnetic signature can be reduced and the radar image of the vehicle can be falsified as a result.
Furthermore, a method for altering the electromagnetic signature of a surface using at least one above-described microelectronic module or at least one above-described module array is specified. The method comprises the step of converting a first voltage provided into a higher, lower or identical second voltage. Furthermore, the method comprises the step of detecting an electromagnetic radiation. The method furthermore comprises the step of generating an electrical plasma from the second voltage. Furthermore, the method comprises the step of altering the electromagnetic signature of the surface by interaction of the electrical plasma generated with an electromagnetic radiation impinging on the surface.
In the example drawings, in general, identical reference signs refer to the same parts across the various views. The drawings are not necessarily true to scale; instead, importance is generally attached to elucidating the principles of the disclosure herein. In the following description, various embodiments of the disclosure herein are described with reference to the following drawings, in which:
The following detailed description refers to the accompanying drawings, which show for explanation purposes specific details and embodiments in which the disclosure herein can be practiced.
The word “exemplary” is used herein with the meaning “serving as an example, case or illustration”. Any embodiment or configuration described herein as “exemplary” should not necessarily be interpreted as preferred or advantageous vis-à-vis other embodiments or configurations.
In the following detailed description, reference is made to the accompanying drawings, which form part of this description and show for illustration purposes specific embodiments in which the disclosure herein can be implemented. In this regard, direction terminology such as, for instance, “at the top”, “at the bottom”, “at the front”, “at the back”, “front”, “rear”, etc. is used with respect to the orientation of the figure(s) described. Since components of embodiments can be positioned in a number of different orientations, the direction terminology serves for illustration and is not restrictive in any way whatsoever. It goes without saying that other embodiments can be used and structural or logical changes can be made, without departing from the scope of protection of the present disclosure. It goes without saying that the features of the various exemplary embodiments described herein can be combined with one another, unless specifically indicated otherwise. Therefore, the following detailed description should not be interpreted in a restrictive sense, and the scope of protection of the present disclosure is defined by the appended claims.
In the context of this description, the terms “connecting”, and “coupled” are used to describe both a direct and an indirect connection and a direct or indirect coupling. In the figures, identical or similar elements are provided with identical reference signs, insofar as this is expedient.
In the methods described here, the steps can be performed in virtually any arbitrary order, without departing from the principles of the disclosure herein, unless a temporal or functional sequence is expressly presented. If it is set out in a patent claim that firstly one step is performed and then a plurality of other steps are performed successively, then this should be understood to mean that the first step is carried out before all other steps, but the other steps can be carried out in any arbitrary suitable order, unless a sequence is set out within the other steps. Parts of claims in which for example “step A, step B, step C, step D and step E” are presented should be understood to mean that step A is performed first, step E is performed last and steps B, C and D can be performed in any arbitrary order between steps A and E, and that the sequence falls within the formulated scope of protection of the claimed method. Furthermore, specified steps can be performed simultaneously, unless express wording in the claim sets out that the steps are to be performed separately. By way of example, a step for performing X in the claim and a step for performing Y in the claim can be carried out simultaneously within a single procedure, and the resultant process falls within the worded scope of protection of the claimed method.
In accordance with a further embodiment (not illustrated), the microelectronic module 100 can also comprise more than one voltage converter 101, wherein the plurality of voltage converters can also be electrically interconnected with one another and can for example interact as a result. The microelectronic module 100 can also comprise a plurality of actuators 102, wherein each actuator 102 can comprise for example one or a plurality of generators 103 for generating an electrical plasma. Furthermore, the microelectronic module 100 in accordance with one embodiment that is not illustrated can comprise a detection unit for detecting the electromagnetic radiation impinging on the surface, and/or a control unit, configured for controlling the generation of the electrical plasma depending on a signal from the detection unit, a receiver, configured for receiving external data, containing information about the detection of the electromagnetic radiation impinging on the surface, control commands of a superordinate transmitting and/or control element, and/or information from at least one further conventional sensor, an antenna and/or a control or regulating system.
The subject matter disclosed herein, such as the controller and/or other components herein, can be implemented with software in combination with hardware and/or firmware. For example, the subject matter described herein, such as the controller, can be implemented or used in association with software executed by a processor or processing unit. In one exemplary implementation, the subject matter described herein can be implemented using a computer readable medium having stored thereon computer executable instructions that when executed by a processor of a computer control the computer to perform steps. Exemplary computer readable mediums suitable for implementing the subject matter described herein include non-transitory devices, such as disk memory devices, chip memory devices, programmable logic devices, and application specific integrated circuits. In addition, a computer readable medium that implements the subject matter described herein can be located on a single device or computing platform or can be distributed across multiple devices or computing platforms.
In a further embodiment (not illustrated), microelectronic modules 301 can also be provided on the entire aircraft surface, both on the underside and on the top side.
Although the disclosure herein has been shown and described primarily with reference to specific embodiments, it should be understood by those familiar with the technical field that numerous modifications can be made thereto with regard to configuration and details, without departing from the essence and scope of the disclosure herein, as defined by the appended claims. The scope of the disclosure herein is thus determined by the appended claims, and the intention is therefore to encompass all modifications which come under the literal sense or the range of equivalence of the claims.
While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a”, “an” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.
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