CN201160279Y - Transceiver for high-frequency satellite communication - Google Patents
Transceiver for high-frequency satellite communication Download PDFInfo
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- CN201160279Y CN201160279Y CNU2008200037608U CN200820003760U CN201160279Y CN 201160279 Y CN201160279 Y CN 201160279Y CN U2008200037608 U CNU2008200037608 U CN U2008200037608U CN 200820003760 U CN200820003760 U CN 200820003760U CN 201160279 Y CN201160279 Y CN 201160279Y
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- 238000004891 communication Methods 0.000 title claims abstract description 14
- 238000001914 filtration Methods 0.000 claims abstract description 5
- 230000010287 polarization Effects 0.000 claims abstract description 5
- 239000011358 absorbing material Substances 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000012545 processing Methods 0.000 description 5
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
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Abstract
Description
技术领域 technical field
本实用新型涉及一种应用于高频卫星通信的收发装置,且尤其涉及一种具有接收端终端元件的应用于高频卫星通信的收发装置。The utility model relates to a transceiver device applied to high-frequency satellite communication, and in particular to a transceiver device applied to high-frequency satellite communication with a receiving end terminal element.
背景技术 Background technique
高频卫星通信系统的接收路径由一波导(waveguide)接收一卫星信号,经由一模拟处理元件,例如一模拟芯片处理之后,将该卫星信号再转至一数字处理元件,例如一数字芯片作后续的信号处理。The receiving path of the high-frequency satellite communication system receives a satellite signal through a waveguide, and after being processed by an analog processing element, such as an analog chip, the satellite signal is then transferred to a digital processing element, such as a digital chip for follow-up signal processing.
在公知的高频卫星通信收发装置内,其波导自一波导出入端接收该接收卫星信号之后,经由该波导传导至一接收端,再将其传送至一模拟处理元件。在发射路径方面,该波导自一发射端的模拟处理元件接收想要发射的信号,经由该波导传导至该波导出入端发射该卫星信号。In the known high-frequency satellite communication transceiver, the waveguide receives the received satellite signal from a waveguide input terminal, and conducts it to a receiving terminal through the waveguide, and then transmits it to an analog processing element. In terms of the transmission path, the waveguide receives signals to be transmitted from an analog processing element at a transmission end, and transmits the satellite signal through the waveguide to the waveguide input end.
然而该高频卫星通信收发装置在接收卫星信号时,需要将该想要接收卫星信号垂直极化方向的信号消除,以避免该高频卫星通信收发装置无法正常运作。因此,在公知的高频卫星通信收发装置内,还具有一接收端终端元件(receiver load termination),其用以消除该接收卫星信号于该接收端终端元件的反射信号。此装置即可消除该想要接收卫星信号垂直极化方向的信号。However, when the high-frequency satellite communication transceiver device receives satellite signals, it needs to eliminate the signal in the vertical polarization direction of the desired satellite signal to avoid the normal operation of the high-frequency satellite communication transceiver device. Therefore, in the known high-frequency satellite communication transceiver, there is also a receiver load termination, which is used to eliminate the reflected signal of the received satellite signal on the receiver load termination. This device can eliminate the signal in the vertical polarization direction of the desired received satellite signal.
然而在该高频卫星通信收发装置发射信号时,会有部分发射信号通过该接收端终端元件,而造成该发射信号的能量损失,因而造成该发射信号的质量下降。因此,有必要在该接收端终端元件设计一功能以达到避免发射信号能量损失的目的。However, when the high-frequency satellite communication transceiver device transmits signals, part of the transmitted signals will pass through the terminal element at the receiving end, which will cause energy loss of the transmitted signals, thus resulting in a decrease in the quality of the transmitted signals. Therefore, it is necessary to design a function in the terminal element at the receiving end to avoid the energy loss of the transmitted signal.
发明内容 Contents of the invention
本实用新型的一实施例的应用于高频卫星通信的收发装置,包含一波导、一发射端、一接收端和一接收端终端元件。该波导用以接收该收发装置的接收信号和发射该收发装置的发射信号。该发射端连接至该波导,以将该发射信号传送至该波导。该接收端连接至该波导,并自该波导接收该接收信号。该接收端终端元件,连接至该波导,并用以消除该接收信号垂直极化方向的信号。该接收端终端元件包含一滤波单元,用以降低该发射信号进入该接收端终端元件的能量。According to an embodiment of the present invention, a transceiver device for high-frequency satellite communication includes a waveguide, a transmitting end, a receiving end, and a receiving end terminal element. The waveguide is used for receiving the receiving signal of the transceiver device and transmitting the transmitting signal of the transceiver device. The transmitting end is connected to the waveguide to transmit the transmitting signal to the waveguide. The receiving end is connected to the waveguide and receives the reception signal from the waveguide. The receiving terminal element is connected to the waveguide and used for eliminating signals in the vertical polarization direction of the received signal. The receiving end terminal element includes a filtering unit for reducing the energy of the transmitted signal entering the receiving end terminal element.
如上所述的收发装置,其中该接收端终端元件包含一吸波材料,用以消除该接收信号于该接收端终端元件的反射信号。In the above-mentioned transceiver device, wherein the receiving terminal element includes a wave-absorbing material for eliminating the reflected signal of the received signal from the receiving terminal element.
如上所述的收发装置,其中该滤波单元是一低通滤波器,其由一平面和多个突起横置的条状结构所构成。The transceiver device as described above, wherein the filtering unit is a low-pass filter, which is composed of a plane and a strip structure with a plurality of protrusions placed horizontally.
如上所述的收发装置,其中该发射端连接于该波导的一支状分歧通道的末端。The above-mentioned transceiver device, wherein the transmitting end is connected to the end of the branch branch channel of the waveguide.
如上所述的收发装置,其发射信号以次要模式发射。As mentioned above, the transmitting and receiving device transmits the signal in the secondary mode.
如上所述的收发装置,其中该接收端连接于该波导主通道的末端。The transceiver device as mentioned above, wherein the receiving end is connected to the end of the main channel of the waveguide.
如上所述的收发装置,其接收信号以主要模式接收。In the above-mentioned transceiver device, the received signal is received in the main mode.
如上所述的收发装置,其中该接收端连接于该波导的一支状分歧通道的末端。The above-mentioned transceiver device, wherein the receiving end is connected to the end of the branch branch channel of the waveguide.
如上所述的收发装置,其接收信号以次要模式接收。In the above-mentioned transceiver device, the received signal is received in the secondary mode.
如上所述的收发装置,其中该发射端连接于该波导主通道的末端。The above-mentioned transceiver device, wherein the transmitting end is connected to the end of the main channel of the waveguide.
如上所述的收发装置,其发射信号以主要模式发射。As mentioned above, the transmitting and receiving device transmits the signal in the main mode.
通过本实用新型的收发装置,可以避免发射信号能量的损失。Through the transmitting and receiving device of the utility model, the loss of transmitted signal energy can be avoided.
附图说明 Description of drawings
图1显示本实用新型的一实施例的应用于高频卫星通信的收发装置;及Fig. 1 shows a transceiver device applied to high-frequency satellite communication according to an embodiment of the present invention; and
图2显示图1的接收端终端元件的放大图。FIG. 2 shows an enlarged view of the receiver terminal element of FIG. 1 .
其中,附图标记说明如下:Wherein, the reference signs are explained as follows:
101收发装置101 transceiver device
102波导102 waveguide
103发射端103 transmitter
104接收端104 receiving end
105接收端终端元件105 Receiver Terminal Components
106吸波材料106 absorbing material
201条状结构201 strip structure
具体实施方式 Detailed ways
图1显示本实用新型的一实施例的应用于高频卫星通信的收发装置。该收发装置101包含一波导102、一发射端103、一接收端104和一接收端终端元件105。该波导102用以接收该收发装置101的接收信号和发射该收发装置101的发射信号。该发射端103连接至该波导102,以将该发射信号传送至该波导102。该接收端104连接至该波导102,并自该波导102接收该接收信号。该接收端终端元件105连接至该波导102,并于其底部以一阶梯状的吸波材料106覆盖,用以消除该接收信号于该接收端终端元件105的反射信号。该接收端终端元件105为降低该发射信号进入该接收端终端元件105的能量,其具有一滤波单元以阻绝该发射信号进入该接收端终端元件105。FIG. 1 shows a transceiver device applied to high-frequency satellite communication according to an embodiment of the present invention. The
图2显示该接收端终端元件105的放大图。如图2所示,该接收端终端元件105在其中间平面上具有多个横置的条状结构201,其也和该接收端终端元件105的平面构成一低通滤波器。该低通滤波器可通过收发装置101的接收信号,而阻绝该收发装置101的发射信号,使其避免该发射信号因该接收端终端元件105内的该吸波材料106而损失能量。FIG. 2 shows an enlarged view of the
再次参照图1,该收发装置101的发射端103连接于该波导102的一支状分叉的末端,因此其发射信号以次要模式(side mode)发射。该接收端104连接于该波导102主通道的末端,因此其接收信号以主要模式(main mode)接收。然而本实用新型的收发装置不限于图1的实施例的收发模式。换言之,该发射端103可连接于该波导102主通道的末端,以主要模式发射信号;而该接收端104可连接于该波导102的一支状分歧通道的末端,以次要模式接收信号,其收发装置也可运用该接收端终端元件105降低该发射信号进入该接收端终端元件105的能量。Referring again to FIG. 1 , the transmitting
本实用新型的技术内容及技术特点已揭示如上,然而所属领域的技术人员仍可能基于本实用新型的教导及揭示而作种种不背离本实用新型精神的替换及修改。因此,本实用新型的保护范围应不限于实施例所揭示的范围,而应包括各种不背离本实用新型的替换及修改,并为所附的权利要求书所涵盖。The technical content and technical features of the utility model have been disclosed above, but those skilled in the art may still make various replacements and modifications based on the teaching and disclosure of the utility model without departing from the spirit of the utility model. Therefore, the protection scope of the utility model should not be limited to the scope disclosed in the embodiments, but should include various replacements and modifications that do not deviate from the utility model, and are covered by the appended claims.
Claims (11)
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CNU2008200037608U CN201160279Y (en) | 2008-02-19 | 2008-02-19 | Transceiver for high-frequency satellite communication |
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CNU2008200037608U CN201160279Y (en) | 2008-02-19 | 2008-02-19 | Transceiver for high-frequency satellite communication |
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Granted publication date: 20081203 Termination date: 20130219 |