CN201018508Y - A pre-satellite receiving and transmitting circuit - Google Patents
A pre-satellite receiving and transmitting circuit Download PDFInfo
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- CN201018508Y CN201018508Y CNU2007200839873U CN200720083987U CN201018508Y CN 201018508 Y CN201018508 Y CN 201018508Y CN U2007200839873 U CNU2007200839873 U CN U2007200839873U CN 200720083987 U CN200720083987 U CN 200720083987U CN 201018508 Y CN201018508 Y CN 201018508Y
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Abstract
本实用新型涉及通信领域,尤其是一种前置卫星接收发射电路,其特征在于:包括分离信号和电源的分频电路、发射端接收保护电路、安装在接收天线根部的低噪声放大电路和接收端接收保护电路,以上电路顺次连接,设置电源稳压变换电路,分频电路的电压输出经电源稳压变换电路后向其他电路提供。本实用新型具有低噪放大、保护、小型等性能优点,适合卫通收发天线距离较近,位置狭窄,传输电缆根数受限情况下使用。
The utility model relates to the communication field, in particular to a front-end satellite receiving and transmitting circuit, which is characterized in that it includes a frequency division circuit for separating signals and power supplies, a receiving protection circuit at the transmitting end, a low-noise amplifier circuit installed at the root of the receiving antenna, and a receiving The terminal receives the protection circuit, the above circuits are connected in sequence, and the power supply voltage stabilization conversion circuit is set, and the voltage output of the frequency division circuit is provided to other circuits after the power supply voltage stabilization conversion circuit. The utility model has the performance advantages of low-noise amplification, protection, small size, etc., and is suitable for use under the conditions that the distance between satellite transceiver antennas is relatively short, the location is narrow, and the number of transmission cables is limited.
Description
技术领域technical field
本实用新型涉及通信领域,尤其是一种前置卫星接收发射电路。The utility model relates to the communication field, in particular to a front satellite receiving and transmitting circuit.
背景技术Background technique
由于卫星收发频率不同,卫通天线一般分别为收发两副天线,在收发天线距离较近的情况下,卫星收发天线隔离度只有十几dB左右。因此,卫通信号发射时,会有发射功率进入接收天线,并且此干扰信号相对卫星接收信号较大。而目前卫星通信领域广泛采用的双工器,需设置隔离电路来避免收发天线之间的信号干扰,虽然具有防止大信号进入接收前端、引起接收信号饱和甚至烧毁的功能,但它空间尺寸很大,插入损耗大,噪声系数也较大,不便于狭窄位置使用。现有技术缺乏同时满足小空间尺寸和低噪声接收的方案。Due to the different frequencies of satellite transmission and reception, Satcom antennas generally have two antennas for transmitting and receiving. When the distance between the transmitting and receiving antennas is relatively close, the isolation of the satellite transmitting and receiving antennas is only about ten dB or so. Therefore, when the satellite communication signal is transmitted, there will be transmission power entering the receiving antenna, and this interference signal is relatively large compared to the satellite receiving signal. At present, the duplexer, which is widely used in the field of satellite communication, needs to set up an isolation circuit to avoid signal interference between the transmitting and receiving antennas. Although it has the function of preventing large signals from entering the receiving front end, causing saturation or even burning of the received signal, it has a large space , the insertion loss is large, and the noise figure is also large, which is not convenient for use in narrow places. The prior art lacks a solution that satisfies both small space size and low-noise reception.
实用新型内容Utility model content
本实用新型的目的在于设计一种小体积且低噪声接收的前置卫星接收发射电路。The purpose of the utility model is to design a small-volume and low-noise receiving front-end satellite receiving and transmitting circuit.
为实现本实用新型所述目的,本实用新型提供前置卫星接收发射电路,包括分离信号和电源的分频电路、发射端接收保护电路、安装在接收天线根部的低噪声放大电路和接收端接收保护电路,以上电路顺次连接,设置电源稳压变换电路,分频电路的电压输出经电源稳压变换电路后向其他电路提供。In order to achieve the purpose of the utility model, the utility model provides a front-end satellite receiving and transmitting circuit, including a frequency division circuit for separating signals and power supplies, a receiving protection circuit at the transmitting end, a low-noise amplifier circuit installed at the root of the receiving antenna, and a receiving and receiving circuit at the receiving end. The protection circuit, the above circuits are connected in sequence, and the power supply voltage stabilization conversion circuit is set, and the voltage output of the frequency division circuit is provided to other circuits after being passed through the power supply voltage stabilization conversion circuit.
而且,低噪声放大电路由一级放大、滤波器、二级放大串联构成。Moreover, the low-noise amplifier circuit is composed of a first-stage amplifier, a filter, and a second-stage amplifier in series.
而且,发射端接收保护电路由发射射频开关和发射端跟随保护电路构成,所述发射端跟随保护电路采用双二极管保护电路,分频电路经发射射频开关触点选通发射天线或发射端跟随保护电路,发射端跟随保护电路接入低噪声放大电路。Moreover, the transmitting end receiving protection circuit is composed of a transmitting radio frequency switch and a transmitting end following protection circuit. The transmitting end following protection circuit adopts a double diode protection circuit, and the frequency division circuit selects the transmitting antenna or the transmitting end following protection through the transmitting radio frequency switch contact. circuit, the transmitting end is connected to the low noise amplifier circuit following the protection circuit.
而且,接收端接收保护电路由接收射频开关和接收端跟随保护电路构成,所述接收端跟随保护电路采用双二极管保护电路,接收天线经接收射频开关触点连接接收端跟随保护电路,接收端跟随保护电路接入低噪声放大电路。Moreover, the receiving protection circuit at the receiving end is composed of a receiving radio frequency switch and a receiving end following protection circuit. The receiving end following protection circuit adopts a double diode protection circuit. The protection circuit is connected to the low noise amplifier circuit.
而且,所述发射射频开关和接收射频开关采用dowkey公司的微波射频开关409芯片。Moreover, the transmitting radio frequency switch and the receiving radio frequency switch adopt the microwave
本实用新型提供的前置卫星接收发射电路在接收天线根部设置低噪声放大电路,将接收信号先一步处理后送入后续信号处理电路,加强了接收信号质量,提高了信噪比。并且这种处理降低了收发两副天线之间空间距离的要求,减小了卫星前端设备体积。本实用新型还集成实现发射与接收信号通路,采用射频开关划分发射和接收过程,以简便的电路切换结构降低了发射功率对接收的干扰;采用了保护电路,防止放大器件损坏;采用单电缆传输电源与信号,缩减了电源及布线所占位置。本发明具有低噪放大、保护、小型等性能优点。与现有双工器相比,本实用新型发明体积小,总量轻,只有普通双工器的1/3~1/4大小,适合卫通收发天线距离较近,位置狭窄,传输电缆根数受限情况下使用。The front-end satellite receiving and transmitting circuit provided by the utility model is equipped with a low-noise amplifier circuit at the root of the receiving antenna, and the received signal is firstly processed and then sent to the subsequent signal processing circuit, which strengthens the quality of the received signal and improves the signal-to-noise ratio. Moreover, this processing reduces the requirement for the space distance between the two transmitting and receiving antennas, and reduces the volume of the satellite front-end equipment. The utility model is also integrated to realize the transmission and reception signal path, adopts the radio frequency switch to divide the transmission and reception process, reduces the interference of the transmission power to the reception with the simple circuit switching structure; adopts the protection circuit to prevent the damage of the amplifying device; Power supply and signal, reducing the space occupied by power supply and wiring. The invention has performance advantages such as low-noise amplification, protection and small size. Compared with the existing duplexer, the utility model is small in size and light in weight, only 1/3 to 1/4 of the size of the ordinary duplexer. Use in limited numbers.
附图说明Description of drawings
图1是本实用新型的结构框图;Fig. 1 is a block diagram of the utility model;
图2是本实用新型实施例的发射端接收保护电路图;Fig. 2 is the receiving protection circuit diagram of the transmitting end of the utility model embodiment;
图3是本实用新型实施例的分频电路图。Fig. 3 is a frequency division circuit diagram of the embodiment of the utility model.
具体实施方式Detailed ways
参见说明书附图1,本实用新型提供前置卫星接收发射电路,包括分离信号和电源的分频电路1、发射端接收保护电路2、安装在接收天线根部的低噪声放大电路3和接收端接收保护电路4,以上电路顺次连接,设置电源稳压变换电路5,分频电路1的电压输出经电源稳压变换电路5后向其他电路提供。现有技术的双工器取得接收信号后直接向后续信号处理电路传输,因此信噪比容易受发射频率影响,本实用新型在接收天线根部设置低噪声放大电路3,将接收信号先一步处理后送入后续信号处理电路,加强了接收信号质量,提高信噪比,节约了设备体积。发射端接收保护电路2和接收端接收保护电路4作用是卫通发射时断开接收天线通路,防止大信号进入接收前端、引起接收信号饱和甚至烧毁;卫通接收时,将卫通天线接收的信号经过低噪声放大电路3进行放大、滤波,最后将信号传输到后续接收处理装置。本实用新型的卫通发射与接收共享信号通道,可以节约体积,而且本实用新型电源与信号在一根同轴电缆上传输,进一步减小体积,通过分频电路1将电源与信号分开即可分别满足信号传输和电源提供。参见图3,具体实施时分频电路1采用分频电感L,分频电感L可采用高频空心电感设计,线圈耦合发射信号的功率时不至于烧毁。分频后分频电路1的电压输出通过电源稳压变换电路5进行稳压和电压转化,具体实施时电源稳压变换电路5可根据要求选用稳压芯片U7805。分频后分频电路1的电压输出由稳压芯片U7805的Vin引脚进入,转换后的电压经Vout引脚输出,箭头表示表示该路直流电压输出作为工作电源向其他各电路提供,U7805的GND引脚接地。Referring to the accompanying
具体实施时,低噪声放大电路3可采用一级放大+滤波器+二级放大相串联的形式。两级放大均采用HMC356LP3芯片,该芯片具有1dB高压缩点,可实现噪声2dB的指标要求。同时印制版技术采用微带技术进行低噪声匹配,使放大器输入输出阻抗严格匹配至50Ω,不仅仅满足低噪声要求,同时减小模块尺寸。滤波器可采用SBP347-N芯片,其频率f=327~367MHz,抑制比35dB。During specific implementation, the low-
本实用新型提供了进一步的保护电路设计方案,以便实施。参见附图2,发射端接收保护电路2由发射射频开关21和发射端跟随保护电路22构成。所述发射端跟随保护电路22采用双二极管保护电路,由一个负极接地的二极管c1和一个正极接地的二极管c2构成。分频电路1经发射射频开关触点选通发射天线或发射端跟随保护电路22,发射端跟随保护电路22接入低噪声放大电路3。接收端接收保护电路4由接收射频开关41和接收端跟随保护电路42构成,所述接收端跟随保护电路42同样采用双二极管保护电路,接收天线经接收射频开关触点连接接收端跟随保护电路42,接收端跟随保护电路42接入低噪声放大电路3。本实用新型采用一种思路设计发射端接收保护电路2和接收端接收保护电路4,不同的仅是开关和双二极管位置相交换。采用射频开关划分发射和接收过程,以简便的电路切换结构降低了发射功率对接收的干扰。The utility model provides a further protection circuit design scheme for implementation. Referring to FIG. 2 , the receiving
发射射频开关和接收射频开关可采用dowkey公司的微波射频开关409芯片。只需控制电源通断,409芯片可以快速响应改换通道。The transmitting radio frequency switch and the receiving radio frequency switch can use the microwave
卫通接收时,接收射频开关41接通,处于接收位置。卫通天线接收的信号,首先经过接收端跟随保护电路42,目的是阻止意外大电流对放大器的损坏,然后经过低噪声放大电路3的一级放大33、滤波器32、二级放大31,最后通过分频电路1将信号传输到后续信号处理装置进行接收处理。此时,直流电源与接收信号在一根电缆上双向传输,直流电源通过分频电路1,作为电源供电。When Satcom is receiving, the receiving
卫通发射时,通过分频电路1将电源与发射信号分开,发射信号通过发射射频开关21选择发射位置,将发射信号通过发射天线发射出去。此时,接收射频开关41断开,也就是将接收天线耦合的发射信号与接收部分电路断开,对接低噪声放大电路3进行保护。During satellite transmission, the
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| CNU2007200839873U CN201018508Y (en) | 2007-04-02 | 2007-04-02 | A pre-satellite receiving and transmitting circuit |
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| CNU2007200839873U CN201018508Y (en) | 2007-04-02 | 2007-04-02 | A pre-satellite receiving and transmitting circuit |
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| CN201018508Y true CN201018508Y (en) | 2008-02-06 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102800142A (en) * | 2012-07-26 | 2012-11-28 | 成都泰然科技有限公司 | Intelligent lock, intelligent key and bidirectional interaction control method thereof |
| CN105277198A (en) * | 2015-10-23 | 2016-01-27 | 卜放 | Vehicle-mounted wireless navigation signal processing system and circuit |
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2007
- 2007-04-02 CN CNU2007200839873U patent/CN201018508Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102800142A (en) * | 2012-07-26 | 2012-11-28 | 成都泰然科技有限公司 | Intelligent lock, intelligent key and bidirectional interaction control method thereof |
| CN102800142B (en) * | 2012-07-26 | 2015-04-08 | 成都泰然科技有限公司 | Intelligent lock, intelligent key and bidirectional interaction control method thereof |
| CN105277198A (en) * | 2015-10-23 | 2016-01-27 | 卜放 | Vehicle-mounted wireless navigation signal processing system and circuit |
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Granted publication date: 20080206 Termination date: 20130402 |