• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a device (10) for a transmitting and receiving unit (110) of a communication system. The device (10) has a first passage (120A) for electromagnetic waves and a second passage (120B) for electromagnetic waves, a partially transparent surface (130) that is transparent for electromagnetic waves of a first range of lengths of electromagnetic waves. wave (180A, 180B) and reflective for electromagnetic waves of a second wavelength range (190) different from the first range (180A, 180B), and a first retroreflective surface (140A) which retroreflects the electromagnetic waves of the first range (180A, 180B). A wave reflection direction of the first range (180A, 180B) is different than a second wave reflection direction (190) when the first range (180A, 180B) electromagnetic waves as well as the electromagnetic waves from the second range (190) enter through the same passage.
    公开号:FR3058394A1
    申请号:FR1760517
    申请日:2017-11-09
    公开日:2018-05-11
    发明作者:Konrad Panzlaff；Andrej Brzoska；Wolfgang Holota；Martin Schwab；Gerd Muhlnikel；Carsten Fechtmann
    申请人:Tesat Spacecom GmbH and Co KG；
    IPC主号:
    专利说明:

    (54) SOLAR FILTER FOR SPACE VEHICLES.
    The present invention relates to a device (10) for a transmission and reception unit (110) of a communication system. The device (10) has a first passage (120A) for electromagnetic waves and a second passage (120B) for electromagnetic waves, a partially transparent surface (130) which is transparent for electromagnetic waves of a first range of lengths d wave (180A, 180B) and reflecting for electromagnetic waves of a second wavelength range (190) different from the first range (180A, 180B), and a first retroreflective surface (140A) which retroreflects the electromagnetic waves of the first range (180A, 180B). A direction of reflection of the waves of the first range (180A, 180B) is different from a direction of reflection of the waves of the second range (190) when the electromagnetic waves of the first range (180A, 180B) as well as the electromagnetic waves of the second range (190) enter through the same passage.
    Γ 17θ
    The present invention relates to a device for a transmission and reception unit of a communication system, as well as a spacecraft equipped with such a device. The present invention relates in particular to the improvement of the thermal stresses of the heat fluxes concerning the components of such a device as well as a spacecraft equipped with such a device.
    The magnitude of thermal stresses can be a major challenge, especially for spacecraft that are used and operate outside of the Earth's atmosphere. This is due to the fact that, given the absence of atmosphere, the heat exchange takes place without convection only by thermal conduction and radiation.
    In principle, heat can pass from a place at a higher temperature to a place at a lower temperature by the phenomenon of thermal conduction (also called thermal diffusion) or by thermal radiation. In addition, heat transport is also possible by convection and a flow of macroscopic material is necessary for this purpose. Outside the Earth's atmosphere, that is to say in a vacuum, a transport of heat by convection is impossible due to the absence of atmosphere. The actual or variable exposure, or non-exposure, of an object to sources of radiation, especially also to the sun, can lead to very high temperature variations inside the object. This poses a major challenge for man-made spacecraft, particularly since the components used must be designed to operate in a limited temperature range.
    US Pat. No. 6,073,888 describes a satellite which orbits around the Earth and which includes a thermal radiator. The heat radiator is designed to dissipate heat from a heat source and to diffuse it into space. A heat conductor extends between the heat sink and the heat source, and thermal switches are provided to connect the heat source to the heat sink and reduce the temperature of the heat source when the temperature exceeds a predetermined threshold.
    It can be considered that the aim of the present invention is to reduce a temperature gradient, in particular a spatial temperature gradient, that is to say a temperature difference between two points of an object at the same time t, in a communication system, and in particular to reduce or eliminate an unwanted loss or unwanted entry of thermal radiation into a communication system.
    This object is achieved by the subject of the independent claim. Other embodiments arise from the dependent claims as well as from the description which follows.
    According to a first aspect of the present invention, a device is provided for a transmission and reception unit of a communication system. This device can be a part of a communication device, but it can also be an extension or a subsequent installation which is in particular arranged on a signal transmission path.
    According to an embodiment of the present invention, the device comprises a first passage for electromagnetic waves and a second passage for electromagnetic waves. The first and second passes can be called signal input or signal output. For optical signals, these passages can be recesses or openings which allow the passage of optical signals. The device can be configured for unidirectional or bidirectional transmission of signals in half-duplex or duplex mode. Both the first pass and the second pass can be thought of as signal input or signal output, or both.
    In this embodiment, the device further comprises a partially transparent surface which is transparent for electromagnetic waves of a first range of wavelengths, and which is produced so as to reflect electromagnetic waves of a second range of wavelengths which is different from the first range of wavelengths. The partially transparent surface can also be qualified as a partially reflective surface.
    In the context of the present description, the term partially transparent means that the partially transparent surface is transparent for a first range of electromagnetic wavelengths, and is substantially impermeable for a second range of wavelengths d electromagnetic waves and reflects the electromagnetic waves of the second wavelength range.
    More particularly, the electromagnetic waves of the second wavelength range are reflected by the partially transparent surface so that they are directed or reflected from the first pass to the second pass, and / or vice versa, while the electromagnetic waves of the first range of wavelengths are little, or are not, reflected by the partially transparent surface.
    In this embodiment, the device further comprises a first retroreflective surface, which is produced so as to retroreflect the electromagnetic waves of the first range of wavelengths. Here, a direction of reflection of the electromagnetic waves of the first wavelength range is different from a direction of reflection of the electromagnetic waves of the second wavelength range, when the electromagnetic waves of the first wavelength range d wave just like the electromagnetic waves of the second range of wavelengths enter by the same passage.
    In the context of the present description, the term retroreflective means that the retroreflective surface reflects an incident electromagnetic wave at the same angle as that into which it enters. In other words, an incident electromagnetic source is reflected back to its source and is not otherwise deflected or reversed in terms of direction. The retroreflective surface can be produced so that it has retro-reflecting properties in a given angular range, this angular range being for example between 80 ° and 100 °, in particular between 85 ° and 95 °, in particular 90 ° of the incident electromagnetic wave with respect to the retroreflective surface.
    The electromagnetic waves of the second wavelength range can be a signal carrier of a wireless optical communication path. It can in particular be laser radiation. The electromagnetic waves of the first wavelength range can be thermal radiation.
    The configuration described here has the advantage that the signal carrier, that is to say the electromagnetic waves of the second wavelength range, are guided from one passage to the other, while the electromagnetic waves of the first range of wavelengths are prevented from following the same path because they are reflected by the partially transparent surface. In particular, it is thus possible to obtain thermal radiation for example following a path other than the signal carrier. It is thus possible to reduce, or even eliminate, the extent of thermal radiation which leaves the device through the first and second passages and / or enters the device through these passages. We can therefore succeed in reducing a temperature fluctuation and a possible temperature difference in the device (i.e. the difference between the maximum temperature of the device when the energy input from the outside is the highest and the minimum temperature of the device when the energy loss to the outside is greatest).
    If the signal carrier and thermal radiation enter through the first pass, that is, through the same passage, the signal carrier reflects towards the second pass and the thermal radiation is returned towards the first pass. This means that the direction of reflection of the electromagnetic waves of the first wavelength range is different from the direction of reflection of the electromagnetic waves of the second wavelength range.
    For the purposes of this direction, the partially transparent surface associated with the first retroreflective surface as well as with the two passages can be called a reflective unit.
    The direction of reflection of the electromagnetic waves of the first wavelength range is different from the direction of reflection of the electromagnetic waves of the second wavelength range. This means for example that the electromagnetic waves of the first range of wavelengths (thermal radiation) are returned by the retroreflective surface towards their source or origin. If the electromagnetic waves of the second wavelength range enter the reflective unit through the first pass, they are reflected so that they leave the reflective unit again through the same pass. The electromagnetic waves of the second wavelength range (the signal carrier) enter the reflecting unit through one passage, are reflected and leave the reflecting unit through the other passage. The signal carrier corresponds to the communication signal and must naturally leave the device in the direction of a remote station so that a communication link can be established.
    According to an embodiment of the present invention, the electromagnetic waves of the first wavelength range are radiation having a wavelength up to 1000 nm (inclusive) and between 1600 nm and 1 mm ( respectively included). The wavelength range between 1600 nm and 1 mm can also be called long wave thermal radiation. In other words, the partially transparent surface is produced so as to allow the radiation to pass through this range of wavelengths, that is to say in order to be transparent to it, and the retroreflective surface is produced so as to reflect electromagnetic radiation in this wavelength range. This makes it possible to reflect the radiation, in particular the thermal radiation, from the retroreflective surface towards its source, so that it is blocked or at least reduced, said radiation leaves the reflective unit or penetrates by it in the components. of the device located behind.
    It should be noted that the partially transparent surface can be made so as to be transparent for one or more ranges of predefined wavelengths from the indicated range of 1600 nm to 1 mm. Thus, within the meaning of the present application, the term range of wavelengths need not necessarily be understood as a single range of continuous values (but it can be), but it can also include a plurality of ranges spaced apart each other on the wavelength scale. The partially transparent surface can therefore be transparent for electromagnetic waves at a wavelength of 1000 nm (inclusive) and from 1600 nm (inclusive) to 1 mm (inclusive), while the partially transparent surface is made so to be reflective for the excluded range between 1000 nm and 1600 nm (respectively excluded). Of course, segmentation into narrower wavelength ranges is also possible. The partially transparent surface can be called a notch filter, which reflects electronic waves in a narrow wavelength range over a wider wavelength range, and which is transparent to magnetic waves in the remaining range of the wider wavelength range.
    According to another embodiment of the present invention, the electromagnetic waves of the second range of wavelengths are laser radiation.
    The laser wavelength used can be, for example, 1,064 nm or 1,550 nm. For these wavelengths or for a range of wavelengths containing these indicated wavelengths, that is to say for example between 1,060 nm and 1,070 nm or between 1,545 nm and 1,555 nm, or even higher ranges, the partially transparent surface is produced in a reflective manner.
    The laser radiation is used as a signal carrier on a wireless optical data transmission path and is reflected or deflected by the partially transparent surface.
    According to another embodiment of the present invention, the partially transparent surface is produced in the form of a dichroic filter.
    A dichroic filter can also be called an interference filter and is made so as to mirror or reflect magnetic waves as a function of frequency. An interference filter can generally be used to split incident light into frequency ranges.
    Here, the dichroic filter is made so as to reflect waves at the wavelength of the signal carrier and to absorb or substantially reflect electromagnetic waves whose wavelength deviates therefrom, in particular the thermal radiation, or otherwise allow them to pass so that thermal radiation arrives on the retroreflective surface.
    The partially transparent surface may have a dichroic coating which provides or has the dichroic property. This coating may in particular not be metallic.
    The properties of the dichroic coating can be adapted according to the wavelength of the signal carrier used. This adaptation can for example take place during the development or during the manufacture of the device, and it may be necessary because the dichroic coating must be designed differently depending on the wavelength to be reflected. In the analog to the band filter indicated above, it may be a question of adapting the range of wavelengths in which the partially transparent surface reflects, namely the wavelength of the signal carrier used. This can be a wavelength or a range of wavelengths, but it can also be several wavelengths or several ranges of wavelengths.
    According to another embodiment of the present invention, the partially transparent surface comprises germanium.
    The partially transparent surface can be produced in the form of a germanium mirror. For this purpose, the dichroic coating can be deposited on the germanium. The germanium allows thermal radiation to pass through or is transparent to it.
    The partially transparent surface is arranged between the first retroreflective surface and the two passages. Regardless of the passages through which electromagnetic waves enter the direction change device, these electromagnetic waves first meet and are not reflected by the partially transparent surface and then the first retroreflective surface.
    According to another embodiment of the present invention, the device further comprises a first thermal insulator, the first thermal insulator being arranged behind the first retroreflective surface from the point of view of the first passage. The first thermal insulator allows in particular that the thermal energy introduced into the retroreflective surface by means of thermal radiation has the lowest thermal impact on the surrounding components of the direction change device, that is to say that practically no energy thermal, or even no thermal energy, is supplied by or received by the reflecting unit.
    The first thermal insulator can be produced in the form of a black body. A black body (also called black radiator, Planck radiator or source of thermal radiation) absorbs incident electromagnetic radiation at each wavelength or in a predetermined wavelength range in an ideal case up to 100% and emits thermal radiation in the form of electromagnetic radiation, which depends only on its temperature and is independent of the subsequent nature of the body and its surface.
    According to another embodiment of the present invention, the device further comprises a first heating element which is produced so as to supply thermal energy and to direct it towards the first retroreflective surface.
    Thus, the temperature of the first retroreflective surface can be increased in order to compensate for the losses and the diffusions of the thermal radiation resulting from the partially transparent surface, so that the magnitude of the thermal radiation supplied by the retroreflective surface (i.e. - say the sum of the reflected radiation and the thermal energy supplied) corresponds to the thermal radiation initially introduced into the reflecting unit.
    The first heating element is produced in such a way as to generate and transfer thermal energy. The first heating element can for example be supplied with electrical energy. The heating element can also be produced so as to be coupled to a receiver, in particular an electric receiver, and to receive the heat lost by this receiver and then to transfer it in the form of thermal energy towards the first retroreflective surface .
    According to another embodiment of the present invention, the first retroreflective surface comprises a metallic coating.
    The metallic coating may for example be gold, silver or copper, or a combination thereof. This coating can be applied to a plastic body, the thermal radiation being thus reflected.
    According to another embodiment of the present invention, the first retroreflective surface comprises at least one triple mirror element, which is produced so as to return incident electromagnetic radiation towards its source.
    A triple mirror element can reflect incident radiation over a determined angular range, so that it is returned to its source. The retroreflective surface may include a plurality of such triple mirror elements, these being arranged flat next to each other. Such a configuration can be called triple mirror or retroreflector.
    According to another embodiment of the present invention, the at least one triple mirror element has an opening through which additional thermal radiation can penetrate, which radiation is supplied in the same direction as the electromagnetic waves of the first range of lengths. wave. The additional thermal radiation can in particular be provided by the heating element, such as that which has been described more above.
    According to another embodiment of the present invention, the device further comprises a second retroreflective surface, in which the first retroreflective surface is arranged opposite the first passage, in which the second retroreflective surface is arranged opposite the second passage, and wherein the partially transparent surface is arranged between the first passage and the first retroreflective surface and between the second passage and the second retroreflective surface, so that the electromagnetic waves of the second wavelength range which are incident on the surface partially transparent through the first passage, are reflected towards the second passage.
    The retro-reflective surfaces can be in the form of a single structural component associated with the partially transparent surface. For example, the retroreflective surfaces can be applied to the rear face of the partially transparent surface, that is to say to the face of the partially transparent surface which is opposite the passages. It is possible to arrange several triple mirror elements, a part of these triple mirror elements being arranged so as to reflect the thermal radiation in the direction of the first passage and another part of the triple mirror elements being arranged so as to reflect the thermal radiation towards the second pass.
    Alternatively, the retroreflective surface can be structurally separated from the partially transparent surface.
    The second retroreflective surface can be constructed similarly to the first retroreflective surface, so that reference is made here to the embodiments of the first retroreflective surface.
    It should however be noted that the second retroreflective surface can also be different from the first retroreflective surface. The shape and size of the openings in the second retroreflective surface can thus be different from those of the openings in the first retroreflective surface. The configuration of the retro-reflective surfaces and the partially transparent surface can be adapted to the wavelength of the signal carrier used, during the development and / or manufacturing phase.
    According to another embodiment of the present invention, the first retroreflective surface just like the second retroreflective surface are produced in a planar manner and the first and second retroreflective surfaces have an angle with respect to each other not equal to 0 ° and not equal to 180 °.
    The first retroreflective surface can be arranged at an angle of 90 ° relative to the second retroreflective surface. Other angles are possible. Preferably, the first passage extends parallel to the first retroreflective surface (opposite the latter), and the second passage extends parallel to the second retroreflective surface.
    According to another embodiment of the present invention, the device further comprises a transmitting and / or receiving unit which is produced so as to emit electromagnetic waves of the second range of wavelengths towards the surface partially transparent, and / or to receive electromagnetic waves of the second wavelength range which are reflected by the partially transparent surface.
    The transmission and / or reception unit is in particular a component intended for the optical transmission of data and is designed so as to be able for example to transmit and / or receive a laser beam, in order to transmit or thus receive data. . The transmitting and / or receiving unit can for example be arranged in a satellite. In order to avoid that, in addition to the laser beam, thermal energy is also emitted from the transmitting and / or receiving unit and is supplied by the satellite, the device described above is provided a partially transparent surface and a retroreflective surface. The laser beam is deflected and emitted by the partially transparent surface, while the thermal radiation crosses the partially transparent surface and is reflected by the retroreflective surface towards the emitting and / or receiving unit. A loss of thermal energy is thus reduced, or even entirely prevented.
    The transmitting and / or receiving unit is arranged in such a way that the first passage is between the transmitting and / or receiving unit and the partially transparent surface.
    According to another embodiment of the present invention, the device further comprises a solar filter and a focusing device, in which the solar filter is arranged between the focusing device and the second passage, in which the solar filter is made of so as to filter an incident radiation in the second passage and to be transparent for electromagnetic waves of the second wavelength, and in which the focusing device is made so as to focus the electromagnetic waves of the second wavelength and direct them to a remote station.
    The device may include a second thermal insulator and a second heating element which are associated with the second retroreflective surface in the same manner as that which has already been described with respect to the first thermal insulator, the first heating element and the first retroreflective surface. The solar filter can be heated by incident solar radiation or by other radiation, and deliver thermal radiation towards the reflective unit. The second retroreflective surface is intended to prevent this thermal radiation from heating the device and / or the reflecting unit, which second surface reflects (returns) this radiation towards the second passage and the solar filter, the laser signals received, this that is to say the useful signals or the signal carrier, being reflected by the partially transparent surface in the direction of the transmitting and / or receiving unit.
    In the event that the sun filter is not exposed to direct sunlight, significant cooling may occur, particularly when used in space outside of the Earth's atmosphere, and the temperature range over which the sun filter must work, so can be very high. In order to reduce temperature variations at the solar filter, the second heating element can provide thermal radiation which is delivered from the second retro-reflective surface towards the solar filter.
    According to another aspect of the present invention, a spacecraft is provided comprising a device as described here, in which the device is intended to establish a communication link.
    The spacecraft may be a satellite intended to be used outside of the Earth's atmosphere. Such a spacecraft can establish a communication link, in particular link a wireless optical communication link, with another aircraft or spacecraft or with a remote station on Earth.
    The communication system necessarily involves the transmission and / or reception of signals. The corresponding openings allow (essentially unwanted) exchange of thermal radiation in both directions. In other words, the spacecraft and / or the components of the communication device can thus cool when the openings are directed towards space, that is to say by moving away from the direct constraint of a radiation source such as, for example, the sun. Otherwise, that is to say when the openings are directed towards a source of radiation such as, for example, the sun, this can lead to a significant heating of the spacecraft and / or the components of the device. Communication. The configuration of the device described here allows the smallest possible amount of thermal radiation to exit or enter the spacecraft through the device. The maximum temperature variation of the solar filter is also reduced.
    Embodiments of the present invention are explained below in more detail by means of the accompanying drawings. The figures are schematic and are not to scale. Identical references relate to identical or analogous elements. Other characteristics and advantages of the invention will emerge more clearly on reading the description below, made with reference to the accompanying drawings, in which:
    FIG. 1 is a schematic representation of a device for a transmission and reception unit of a communication system according to an exemplary embodiment of the present invention,
    FIG. 2 is a schematic representation of a retroreflective surface for a device for a transmission and reception unit of a communication device according to another exemplary embodiment of the present invention,
    - Figure 3 is a schematic representation of a retroreflector.
    FIG. 1 represents a device 10 for a transmission and reception unit of a communication system. The device comprises: a first passage 120A for electromagnetic waves and a second passage 120B for electromagnetic waves, a partially transparent surface 130 which is transparent for electromagnetic waves of a first wavelength range 180A, 180B and which is produced so as to reflect electromagnetic waves of a second wavelength range 190, which is different from the first wavelength range, and a first retroreflective surface 140A which is produced so as to retroreflect the electromagnetic waves of the first wavelength range 180A, 180B, in which a direction of reflection of the electromagnetic waves of the first wavelength range 180A, 180B is different from a direction of reflection of the electromagnetic waves of the second range of lengths wave 190.
    The device 10 further comprises: a first thermal insulator 150A, which is arranged behind the first retroreflective surface 140A from the point of view of the first passage 120A, and a first heating element 155A which is produced so as to yield thermal energy and to direct it towards the first retroreflective surface 140A.
    The device 10 further comprises: a second retroreflective surface 140B, in which the first retroreflective surface 140A is arranged opposite the first passage 120A, in which the second retroreflective surface 140B is arranged opposite the second passage 120B, and in which the surface partially transparent 130 is arranged between the first passage 120A and the first retroreflective surface 140A and between the second passage 120B and the second retroreflective surface 140B, so that the electromagnetic waves of the second wavelength range, which arrive on the surface partially transparent 130 by the first passage 120B, are reflected towards the second passage 120B.
    From the point of view of the second passage 120B, a second thermal insulator 150B and a second heating element 155B are arranged behind the second retroreflective surface 140B.
    The device 10 further comprises: a transmitting and / or receiving unit 110 which is produced so as to emit electromagnetic waves of the second wavelength range 190 towards the partially transparent surface 130 and / or at receiving electromagnetic waves of the second range of wavelengths 190 which are reflected by the partially transparent surface 130. In addition, the device 10 comprises a solar filter and a focusing device which are arranged in front of the second passage 120B.
    In other words, the device 10 is configured so that it consists of two partly similar functional branches. A first functional branch is composed of the transmitting and / or receiving unit 110, the first passage 120A, the partially transparent surface 130, the first retroreflective surface
    140A, the first thermal insulator 150A and the first heating element 155A. This first functional branch is represented horizontal in FIG. 1. The second functional branch is configured in a similar manner to the first functional branch and is represented vertical in FIG. 1. In addition to the first functional branch, the second functional branch comprises a filter. solar 160 and a focusing device 170, no transmitting and / or receiving unit 110 being provided in the second functional branch. In a satellite, the device 10 is installed so that the first functional branch points towards the inside of the satellite and the second functional branch points towards the outside of the satellite towards a remote communication station.
    The first functional branch is intended not to allow thermal radiation from the communication system or a satellite to escape, or to reduce the extent of escaping thermal radiation. As can be seen in FIG. 1, the transmitting and / or receiving unit 110 emits an electromagnetic wave 190, for example a laser beam. This laser beam is reflected by the partially transparent surface 130 in the direction of the second passage 120B and of the focusing device. Simultaneously, thermal radiation 180A which emanates from the interior space of a satellite is deflected towards the retroreflective surface 140A by the surface 130 transparent for this radiation 180A and returned by the latter towards the emission unit and / or reception or inside the satellite, so that as a result, practically no thermal radiation, or even no thermal radiation, leaves the satellite. In order to compensate for losses by diffusion, the magnitude of the thermal radiation reflected by the retroreflective surface 140A can be increased by additional thermal energy by means of the heating element 155A.
    The second functional branch (vertical) is in principle similar to the first functional branch (horizontal). The second functional branch is mainly designed to prevent the entry of thermal radiation into the satellite or the communication system. The solar filter is transparent to the signal carrier 190. The solar radiation however makes it possible to heat the solar filter 160 and to deliver the thermal radiation 180B inside the device for changing direction. In order that this thermal radiation 180B does not contribute to heating the communication system or to reduce its magnitude, the second retroreflective surface 140B is arranged so as to reflect the thermal radiation 180B again in the direction of the solar filter. The second heating element 3058394 fant 155B can thus contribute to emitting thermal radiation towards the solar filter 160, so that the solar filter can be heated when it is located on a side of the satellite opposite to the sun and thus prevent the solar filter does not cool very strongly.
    In the exemplary embodiment of FIG. 1, the first retroreflective surface 140A as well as the second retroreflective surface 140B are produced in a planar manner. The two surfaces 140A, 140B are provided as structurally distinct components separate from the partially transparent surface 130. The surfaces 140A, 140B may consist of a main body of plastic material which is coated with a metallic coating. In this exemplary embodiment, the surfaces 140A, 140B are arranged at an angle of 90 ° relative to one another.
    The transmitting and / or receiving unit 110 may for example be a transmitting / receiving unit of a laser communication device. The arrangement shown according to the device 10 is on the one hand adapted to store the thermal radiation inside the unit 110 or not to let it escape, and in the case where the focusing device 170 is opposite in the sun or another source of radiation, to heat the solar filter 160. On the other hand, in the event of direct exposure of the focusing device 170 and the solar filter 160 to the sun, heating of the emission unit / reception 110 is minimized. In addition, this arrangement is suitable for keeping the thermal gradient in the transmitting / receiving unit to a minimum since the partially transparent surface 130 allows thermal radiation to pass through and reflects the laser wavelength 190 used by means of a special coating (reflection coating, dichroic, non-metallic). The partially transparent surface 130 can also be produced in the form of a germanium mirror.
    The wavelength of the laser radiation 190 can be changed and it may therefore be necessary to adapt the reflection coating. The operating principle remains, however, maintained.
    The function of the solar filter 160 is to reflect the solar radiation as much as possible (from UV up to about 1800 nm) or to absorb it. For longer wavelengths, the germanium mirror is transparent. For the laser wavelength used, for example 1,064 nm or 1,550 nm, the solar filter must be transparent or practically transparent.
    In the case of direct solar radiation (when the sun is in the field of vision of the instrument), a large part of the wavelength range> 400 nm (more than 50%) is reflected by the filter solar. For wavelengths <400 nm, a large part is absorbed. This absorption leads to a rise in temperature of the solar filter and therefore to a variation of the radiation in particular in the wavelength range from 7 pm to 12 pm. In order for this variation to have the smallest possible effect on the instrument (device 10), this thermal radiation passes through the germanium mirror and is absorbed by the second insulator 150B.
    In the case where the solar filter 160 and the focusing device 170 are facing the sun, that is to say in the direction of the empty space, it is necessary to prevent the internal temperature of the device 10 from decreasing too strongly by thermal rays. If the thermal radiation 180A of the device 10 now passes through the germanium mirror, it arrives on the retroreflective surface 140A and is reflected in the same direction as the direction of incidence. The thermal radiation thus returns again to the instrument or to the satellite (possibly with low losses). These losses can and must be compensated in order to avoid cooling of the device 10 and of the satellite and to minimize the thermal gradient which appears. This compensation is carried out with the heating element 155B. Too much cooling of the focusing device 170 is prevented by means of the heating element 155B which is arranged opposite the focusing device 170. The two insulators 150A, 150B and heating elements 155A, 155B can be constructed differently as regards , for example, the size of the openings in the retro-reflective surfaces. In addition, it is possible to influence the amount of additional thermal radiation that can be supplied. The main functions of these two units 150A, 155A and 150B, 155B are identical, namely: reflecting the thermal radiation and / or emitting additional thermal radiation by means of the heating elements.
    The operation of the units, and in particular the amount of additional thermal radiation, is regulated by the shape and size of the holes in the triple mirrors.
    The openings of the surface 140B, which receives direct solar radiation as well as the inflow of space from the side opposite the sun, are preferably larger than the openings of the surface 140A. The size of the openings can depend directly on the possible temperature variation of the thermal source (the emission / reception unit 110 or the sun or the empty space).
    The arrows in FIG. 1 make it easy to see that the signal carrier 190, when it enters through the first passage 120A, is reflected towards the second passage 120B, while the thermal radiation 180A which enters through the first passage 120A, is again reflected in the direction of the first pass 120A.
    FIG. 2 represents a retroreflective surface 140A, 140B which comprises a plurality of elements with triple mirror 142. This arrangement can also be called a network of triple mirrors. The surface of the network of triple mirrors can for example be golden. Behind the triple mirror array is arranged a regulated thermal black body, thermal insulation 150A, 150B and a heating element 155A, 155B, which radiates through the openings 147.
    The network of triple mirrors can be circular in shape and have a diameter of 80 mm. It may be a compression molded plastic component, having a metallic coating, for example gold, silver or copper, or a combination thereof.
    FIG. 3 shows a single triple mirror element 142. The triple mirror element 142 has three reflective side faces 144, 145, 146 arranged so that incident radiation is returned to the source.
    The triple mirror element 142 has an opening 147. In this opening, it is possible to arrange an infrared capacitor acting as a source of thermal radiation.
    It should also be clarified that the terms including or including do not exclude any other element or stage and articles one or one do not exclude any plurality. In addition, it should be noted that the characteristics or steps which have been described with reference to one of the exemplary embodiments described above, can also be used in combination with other characteristics or stages of other exemplary embodiments. described above. The references contained in the claims should not be considered as limiting.
    10 Device 110 Transmitting and / or receiving unit 120A First passage 120B Second pass 130 Partially transparent surface 140A First retroreflective surface 140B Second retroreflective surface 142 Retroreflector 144 First side face 145 Second side face 146 Third side face 147 Opening 150A First insulator 150B Second insulator 155A First heating element 155B Second heating element 160 Sun filter 170 Focusing device 180A Electromagnetic waves of the first wavelength range 180B Electromagnetic waves of the first wavelength range 190 Electromagnetic waves of the second wavelength range
    权利要求:
    Claims (15)
    [1" id="c-fr-0001]
    1. Device (10) for a transmission and reception unit (110) of a communication system, comprising:
    a first passage (120A) for electromagnetic waves and a second passage (120B) for electromagnetic waves, a partially transparent surface (130) which is transparent for electromagnetic waves of a first wavelength range (180A, 180B ) and which is made so as to reflect electromagnetic waves of a second range of wavelengths (190) different from the first range of wavelengths (180A, 180B), a first retroreflective surface (140) which is produced so as to retroreflect the electromagnetic waves of the first wavelength range (180A, 180B), characterized in that a direction of reflection of the electromagnetic waves of the first wavelength range (180A, 180B) is different from a direction of reflection of the electromagnetic waves of the second wavelength range (190) when not only the electromagnetic waves of the first wavelength range (180A, 180B) but also the electromagnetic waves of the second wavelength range (190) enter through the same passage (120A; 120B).
    [2" id="c-fr-0002]
    2. Device (10) according to claim 1, characterized in that the electromagnetic waves of the first range of wavelengths (180A, 180B) are radiation having a wavelength up to 1000 nm inclusive and between 1600 nm and 1 mm.
    [3" id="c-fr-0003]
    3. Device (10) according to claim 1 or 2, characterized in that the electromagnetic waves of the second range of wavelengths (180A, 180B) are laser radiation.
    [4" id="c-fr-0004]
    4. Device (10) according to one of the preceding claims, characterized in that the partially transparent surface (130) is produced in the form of a dichroic filter.
    [5" id="c-fr-0005]
    5. Device (10) according to one of the preceding claims, characterized in that the partially transparent surface (130) comprises germanium.
    [6" id="c-fr-0006]
    6. Device (10) according to one of the preceding claims, further comprising a first thermal insulator (150A), characterized in that from the point of view of the first passage (120A), the first thermal insulator (150A) is arranged behind the first retroreflective surface (140).
    [7" id="c-fr-0007]
    7. Device (10) according to one of the preceding claims, characterized in that it further comprises a first heating element (155A) which is produced so as to yield thermal energy and to supply it to the first surface retroreflective (140A).
    [8" id="c-fr-0008]
    8. Device (10) according to one of the preceding claims, characterized in that the first retroreflective surface (140A) comprises a metallic coating.
    [9" id="c-fr-0009]
    9. Device (10) according to one of the preceding claims, characterized in that the first retroreflective surface (140A) comprises at least one triple mirror element (142) which is produced so as to return incident electromagnetic radiation towards its source .
    [10" id="c-fr-0010]
    10. Device (10) according to claim 8, characterized in that the at least one triple mirror element (142) has an opening (147) through which additional thermal radiation can penetrate, which additional thermal radiation is provided in the same direction as the electromagnetic waves of the first wavelength range (180A, 180B).
    [11" id="c-fr-0011]
    11. Device (10) according to one of the preceding claims, further comprising a second retroreflective surface (140B), characterized in that the first retroreflective surface (140A) is arranged opposite the first passage (120A), the second surface retroreflective (140B) is arranged opposite the second passage (120B), the partially transparent surface (130) is arranged between the first passage (120A) and the first retroreflective surface (140A) and between the second passage (120B) and the second retroreflective surface (140B), so that the electromagnetic waves of the second wavelength range (190) which are incident on the partially transparent surface (130) through the first passage (120A) are returned towards the second passage (120B).
    [12" id="c-fr-0012]
    12. Device (10) according to claim 11, characterized in that not only the first retroreflective surface (140A) but also the second retroreflective surface (140B) are made planar and have, with respect to each other, a angle not equal to 0 ° and not equal to 180 °.
    [13" id="c-fr-0013]
    13. Device (10) according to claim 11 or 12, characterized in that it further comprises a transmitting and / or receiving unit (110) which is produced so as to emit electromagnetic waves of the second range of wavelengths (190) towards the partially transparent surface (130) and / or receiving electromagnetic waves of the second range of wavelengths (190) which are reflected by the partially transparent surface (130).
    [14" id="c-fr-0014]
    14. Device (10) according to one of claims 11 to 13, further comprising a solar filter (160) and a focusing device (170), characterized in that the solar filter (160) is arranged between the device focusing (170) and the second passage (120B), the solar filter (160) is produced so as to filter an incident radiation in the second passage (120B) and to be transparent for electromagnetic waves of the second range of lengths wave (190), the focusing device (170) is designed so as to focus the electromagnetic waves of the second wavelength range (190) and to direct them to a remote station.
    [15" id="c-fr-0015]
    15. spacecraft comprising:
    a device (10) according to one of the preceding claims, characterized in that the device (10) is intended to establish a communication link.
    1/2 ^ 170
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    同族专利:
    公开号 | 公开日
    DE102016121484B3|2017-12-28|
    US20180128951A1|2018-05-10|
    FR3058394B1|2021-05-28|
    US10948639B2|2021-03-16|
    JP2018106146A|2018-07-05|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US5367399A|1992-02-13|1994-11-22|Holotek Ltd.|Rotationally symmetric dual reflection optical beam scanner and system using same|
    CA2140618C|1994-11-30|2002-01-15|Nelson L. Rowell|Silicon coated mylar beamsplitter|
    US6073888A|1998-12-02|2000-06-13|Loral Space & Communications, Ltd.|Sequenced heat rejection for body stabilized geosynchronous satellites|
    DE10123050A1|2001-05-11|2002-11-14|Bodenseewerk Geraetetech|Optical arrangement for a dual-mode seeker head|
    US20030081293A1|2001-10-26|2003-05-01|Optical Datastreams, Llc.|Optical communications system and method|
    US7982960B2|2004-03-08|2011-07-19|Optoplex Corporation|Co-package DQPSK demodulator by Michelson interferometer|
    US7121671B2|2003-12-11|2006-10-17|Agilent Technologies, Inc.|Phase-compensated cube corner in laser interferometry|
    DE102016121484B3|2016-11-09|2017-12-28|Tesat-Spacecom Gmbh & Co. Kg|Device for a transmitting and receiving unit of a communication device and spacecraft, comprising such a device|DE102016121484B3|2016-11-09|2017-12-28|Tesat-Spacecom Gmbh & Co. Kg|Device for a transmitting and receiving unit of a communication device and spacecraft, comprising such a device|
    WO2018225754A1|2017-06-05|2018-12-13|積水化学工業株式会社|Sealant for liquid crystal display element, vertical conduction material, and liquid crystal display element|
    US10601367B2|2018-05-11|2020-03-24|The Boeing Company|System for redirecting sunlight to a mobile platform|
    法律状态:
    2019-11-20| PLFP| Fee payment|Year of fee payment: 3 |
    2020-11-20| PLFP| Fee payment|Year of fee payment: 4 |
    2020-12-11| PLSC| Publication of the preliminary search report|Effective date: 20201211 |
    2021-11-22| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    DE102016121484.1A|DE102016121484B3|2016-11-09|2016-11-09|Device for a transmitting and receiving unit of a communication device and spacecraft, comprising such a device|
    DE102016121484.1|2016-11-09|
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