CN113541328A - Power supply and communication device and system of electric equipment on arrow - Google Patents

Power supply and communication device and system of electric equipment on arrow Download PDF

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Publication number
CN113541328A
CN113541328A CN202110774337.8A CN202110774337A CN113541328A CN 113541328 A CN113541328 A CN 113541328A CN 202110774337 A CN202110774337 A CN 202110774337A CN 113541328 A CN113541328 A CN 113541328A
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China
Prior art keywords
power supply
interface transformer
controller
communication device
power
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Pending
Application number
CN202110774337.8A
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Chinese (zh)
Inventor
张洪倩
舒畅
马超
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing One Space Aerospace Technology Co Ltd
Beijing Zero One Space Electronics Co Ltd
Beijing Zero One Space Technology Research Institute Co Ltd
Chongqing Zero One Space Technology Group Co Ltd
Xian Zero One Space Technology Co Ltd
Original Assignee
Chongqing One Space Aerospace Technology Co Ltd
Beijing Zero One Space Electronics Co Ltd
Beijing Zero One Space Technology Research Institute Co Ltd
Chongqing Zero One Space Technology Group Co Ltd
Xian Zero One Space Technology Co Ltd
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Application filed by Chongqing One Space Aerospace Technology Co Ltd, Beijing Zero One Space Electronics Co Ltd, Beijing Zero One Space Technology Research Institute Co Ltd, Chongqing Zero One Space Technology Group Co Ltd, Xian Zero One Space Technology Co Ltd filed Critical Chongqing One Space Aerospace Technology Co Ltd
Priority to CN202110774337.8A priority Critical patent/CN113541328A/en
Publication of CN113541328A publication Critical patent/CN113541328A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J50/00Circuit arrangements or systems for wireless supply or distribution of electric power
    • H02J50/005Mechanical details of housing or structure aiming to accommodate the power transfer means, e.g. mechanical integration of coils, antennas or transducers into emitting or receiving devices
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J13/00Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network
    • H02J13/00006Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network characterised by information or instructions transport means between the monitoring, controlling or managing units and monitored, controlled or operated power network element or electrical equipment
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J13/00Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network
    • H02J13/00006Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network characterised by information or instructions transport means between the monitoring, controlling or managing units and monitored, controlled or operated power network element or electrical equipment
    • H02J13/00028Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network characterised by information or instructions transport means between the monitoring, controlling or managing units and monitored, controlled or operated power network element or electrical equipment involving the use of Internet protocols
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J50/00Circuit arrangements or systems for wireless supply or distribution of electric power
    • H02J50/10Circuit arrangements or systems for wireless supply or distribution of electric power using inductive coupling
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/00032Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by data exchange
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/02Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from ac mains by converters
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B3/00Line transmission systems
    • H04B3/02Details
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B3/00Line transmission systems
    • H04B3/54Systems for transmission via power distribution lines
    • YGENERAL 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
    • Y04INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
    • Y04SSYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
    • Y04S20/00Management or operation of end-user stationary applications or the last stages of power distribution; Controlling, monitoring or operating thereof
    • Y04S20/20End-user application control systems
    • Y04S20/242Home appliances

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Power Sources (AREA)

Abstract

The application provides power supply and communication device, system of electrical equipment on arrow, power supply and communication device include: the power supply controller, the power receiving controller and the isolation voltage transformation module; the input end of the power supply controller is connected with the power supply end of the power supply equipment when in use, and the output end of the power supply controller is connected with the isolation transformation module; the input end of the power receiving controller is connected with the isolation transformation module, and the output end of the power receiving controller is connected with the power supply end of a power receiving device when in use; the problem of be used for among the prior art cable network structure complicacy, the quality heavy assembly degree of difficulty big for power supply and communication is solved to this application, utilizes single net twine can realize the transmission and the power supply control of signal on the arrow, under the prerequisite of guaranteeing communication quality, has saved the relevant cable of power transmission for the relation of connection between the equipment is more succinct, has reduced the complexity of cable network on the arrow.

Description

Power supply and communication device and system of electric equipment on arrow
Technical Field
The invention relates to the technical field of spaceflight, in particular to a power supply and communication device and system for electric equipment on an arrow.
Background
The electric equipment on the rocket generally comprises a control system and a remote measuring system, wherein the control system generally comprises a servo subsystem, an rocket-borne computer or a comprehensive control machine, an inertia system, a navigation subsystem, an attitude control subsystem and the like, and each subsystem generally comprises a single control machine. The telemetering system usually comprises a telemetering transmitter, a remote control receiver and other devices, and in addition, the rocket also comprises a safety controller, a data acquisition system and other stand-alone devices according to the requirements.
The single devices on the arrow need to be powered, and meanwhile, the arrow-mounted computer or the comprehensive control machine is used as a control core on the arrow, so that various states and instruction information on the arrow are generally fused and resolved, a control instruction is obtained according to a control algorithm, and the work of related devices on the arrow is controlled. Therefore, the rocket-borne computer or the comprehensive control machine generally communicates with other single machines on the rocket, information interaction may exist between the single machines on the rocket, namely, the single machines on the rocket have power supply and communication requirements, and the traditional method is to complete power supply and communication of equipment through a cable network on the rocket; due to the fact that a plurality of single-machine devices are involved, the outstanding defects that a cable network topology structure on an arrow is complex, the quality is heavy, the assembly difficulty is large and the like are caused.
Disclosure of Invention
The application provides a power supply and communication device and system of electrical equipment on arrow, solves the problem that the cable network structure that is used for power supply and communication among the prior art is complicated, the quality is big heavily assembled the degree of difficulty, utilizes single net twine can realize the transmission and the power supply control of signal on the arrow, under the prerequisite of guaranteeing communication quality, has saved the relevant cable of power transmission for the relation of connection between the equipment is more succinct, has reduced the complexity of cable network on the arrow.
In a first aspect, the present invention provides a power supply and communication device for an electrical apparatus on an arrow, the power supply and communication device comprising: the power supply controller, the power receiving controller and the isolation voltage transformation module; the input end of the power supply controller is connected with the power supply end of the power supply equipment when in use, and the output end of the power supply controller is connected with the isolation transformation module; the input end of the power receiving controller is connected with the isolation transformation module, and the output end of the power receiving controller is connected with the power supply end of a power receiving device when in use; the isolation transformation module comprises a first interface transformer, a second interface transformer, a third interface transformer and a fourth interface transformer, wherein the primary side of the first interface transformer and the primary side of the second interface transformer are connected with a communication end of power supply equipment when in use, the secondary side of the first interface transformer is connected with the primary side of the third interface transformer through a network cable, the secondary side of the second interface transformer is connected with the primary side of the fourth interface transformer through a network cable, the central tap end of the secondary side of the first interface transformer is connected with the first output end of the power supply controller, and the central tap end of the secondary side of the second interface transformer is connected with the grounding end of the power supply controller; the secondary side of the third interface transformer and the secondary side of the fourth interface transformer are connected with a communication end of a power receiving device when in use, the primary side center tap end of the third interface transformer is connected with the power input end of the power receiving controller, and the primary side center tap end of the fourth interface transformer is connected with the grounding end of the power receiving controller.
Optionally, the isolation transformer module further comprises: a fifth interface transformer, a sixth interface transformer, a seventh interface transformer and an eighth interface transformer; the primary side of the fifth interface transformer and the primary side of the sixth interface transformer are connected with a communication end of a power supply device when in use, the secondary side of the fifth interface transformer is connected with the primary side of the seventh interface transformer through a network cable, the secondary side of the sixth interface transformer is connected with the primary side of the eighth interface transformer through a network cable, the central tap end of the secondary side of the fifth interface transformer is connected with the grounding end of the power supply controller, and the central tap end of the secondary side of the sixth interface transformer is connected with the second output end of the power supply controller; the secondary side of the seventh interface transformer and the secondary side of the eighth interface transformer are connected with a communication end of a power receiving device when in use, the primary center tap end of the seventh interface transformer is connected with the power input end of the power receiving controller, and the primary center tap end of the eighth interface transformer is connected with the grounding end of the power receiving controller.
Optionally, the power supply and communication device further comprises: the first input end of the first rectifying circuit is connected with the primary side center tap end of the third interface transformer, the second input end of the first rectifying circuit is connected with the primary side center tap end of the fourth interface transformer, the first output end of the first rectifying circuit is connected with the power supply input end of the power receiving controller, and the second output end of the first rectifying circuit is connected with the grounding end of the power receiving controller.
Optionally, the power supply and communication device further comprises: and a first input end of the second rectifying circuit is connected with a primary side center tap end of the seventh interface transformer, a second input end of the second rectifying circuit is connected with a primary side center tap end of the eighth interface transformer, a first output end of the second rectifying circuit is connected with a power supply input end of the power receiving controller, and a second output end of the second rectifying circuit is connected with a grounding end of the power receiving controller.
Optionally, the power supply and communication device further comprises: the first end of the first resistor is connected with the first input end of the power supply controller; the source electrode of the first MOS tube is connected with the second end of the first resistor, the grid electrode of the first MOS tube is connected with the first control end of the power supply controller, and the drain electrode of the first MOS tube is connected with the first output end of the power supply controller.
Optionally, the power supply and communication device further comprises: a first end of the second resistor is connected with a second input end of the power supply controller; and the source electrode of the second MOS tube is connected with the second end of the second resistor, the grid electrode of the second MOS tube is connected with the second control end of the power supply controller, and the drain electrode of the second MOS tube is connected with the second output end of the power supply controller.
Optionally, the power supply and communication device further comprises: and the first end of the first capacitor is connected with the first output end of the first rectifying circuit, and the second end of the first capacitor is connected with the second output end of the first rectifying circuit.
Optionally, the power supply and communication device further comprises: and the input end of the voltage stabilizing module is connected with the output end of the power receiving controller, and the output end of the voltage stabilizing module is connected with the power supply end of the power receiving equipment when in use.
Optionally, the voltage stabilization module comprises: the first end of the voltage stabilization management chip is connected with the output end of the power receiving controller; the positive end of the second capacitor is connected with the output end of the power receiving controller, and the negative end of the second capacitor is grounded; the first end of the inductor is connected with the second end of the voltage stabilization management chip, and the second end of the inductor is connected with a power supply end of the powered device; the cathode of the rectifier diode is connected with the second end of the voltage stabilization management chip, and the anode of the rectifier diode is grounded; and the positive end of the third capacitor is connected with the second end of the inductor, and the negative end of the third capacitor is grounded.
In a second aspect, the present invention provides a power supply and communication system for an electrical device on an arrow, the power supply and communication system comprising: the rocket-borne computer, the remote measuring device, the attitude control device, the inertial measurement unit, the servo controller and the power supply and communication device of the rocket-borne electrical equipment; the rocket-borne computer is respectively connected with the remote measuring device, the attitude control device, the inertial measurement unit and the servo controller through the power supply and communication device.
Compared with the prior art, the invention has the following beneficial effects:
according to the invention, the power supply controller is coupled with the power receiving controller through the isolation transformation module, so that the communication between the power supply equipment on the rocket and other equipment is realized through a network cable, and meanwhile, the power supply equipment can supply power to other power receiving equipment, namely, the transmission and power supply control of signals on the rocket can be realized by utilizing a single network cable; because the signal of communication transmission is differential signal, increase the power supply bias on the signal line through the power supply controller, it is equivalent to increasing the common mode interference, so the network communication between the two is not influenced by the power supply mode; meanwhile, the power receiving controller is additionally arranged in the power receiving equipment at the rear end and used for receiving power supply input of the power supply equipment, and the power supply process of the power receiving controller does not affect reliable transmission of signals.
Drawings
Fig. 1 is a schematic structural diagram of a power supply and communication device of an electric apparatus on an arrow according to an embodiment of the present application;
FIG. 2 is a schematic structural diagram of another power supply and communication device for an electric apparatus on an arrow according to an embodiment of the present disclosure;
fig. 3 is a schematic structural diagram of a power supply and communication system of an electric device on an arrow according to an embodiment of the present application.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.
Example one
Fig. 1 is a schematic structural diagram of a power supply and communication device for an electric apparatus on an arrow provided in an embodiment of the present application, and as shown in fig. 1, the power supply and communication device for an electric apparatus on an arrow includes:
the power supply controller, the power receiving controller and the isolation voltage transformation module;
the input end of the power supply controller is connected with the power supply end of the power supply equipment when in use, and the output end of the power supply controller is connected with the isolation transformation module; the input end of the power receiving controller is connected with the isolation transformation module, and the output end of the power receiving controller is connected with the power supply end of a power receiving device when in use;
the isolation transformation module comprises a first interface transformer T1, a second interface transformer T2, a third interface transformer T3 and a fourth interface transformer T4, wherein the primary side of the first interface transformer T1 and the primary side of the second interface transformer T2 are connected with a communication end of power supply equipment when in use, the secondary side of the first interface transformer T1 is connected with the primary side of the third interface transformer T3 through a network cable, the secondary side of the second interface transformer T2 is connected with the primary side of the fourth interface transformer T4 through a network cable, the secondary side center tap end 5 of the first interface transformer T1 is connected with a first output end of the power supply controller, and the secondary side center tap end 5 of the second interface transformer T2 is connected with a grounding end of the power supply controller; the secondary side of the third interface transformer T3 and the secondary side of the fourth interface transformer T4 are connected to a communication terminal of a powered device when in use, the primary side center tap terminal 5 of the third interface transformer T3 is connected to a power input terminal of the powered controller, and the primary side center tap terminal 5 of the fourth interface transformer T4 is connected to a ground terminal of the powered controller.
It should be noted that the electric devices on the arrow include, but are not limited to, a servo controller, an arrow-mounted computer, an inertial measurement unit, an attitude control unit, and a remote measurement receiver, the functions of the devices are independent of each other, but the devices are communicated with the arrow-mounted computer, and the arrow-mounted computer monitors and controls the work of the electric devices; according to the different design thoughts, still can contain the equipment of solitary power supply control and management on the arrow, this equipment has realized the power supply management and control of other singlets. In this embodiment, the communication between the rocket computer and other single machines is completed through the network cable by using ideas and methods of active Ethernet (POE, Power On Ethernet) and industrial Ethernet, and Power is supplied to other single machines at the same time, that is, signal transmission and Power supply control can be realized by using a single network cable; the arrow load computer is used as power supply equipment, the telemetering system, the inertial measurement unit and the like are used as powered equipment, the power supply equipment supplies power for the client equipment of the POE system and is also a manager of the whole POE Ethernet power supply process, and the powered equipment receives the power supply load, namely the client equipment of the POE system.
In practical application, the powered device and the power supply device are electrically and communicatively connected through the power supply and communication device of the rocket-powered electrical device in this embodiment, as shown in fig. 1, the power supply controller is connected with the powered controller through 2 pairs of differential communication lines of a gigabit network port, if the power supply controller increases a +48V level (which may be other suitable voltage values) at the secondary center tap end 5 of the first interface transformer, the secondary center tap end 5 of the second interface transformer is grounded, and since the output of each interface transformer is a differential signal, that is, finally, the signals of the secondary pin 3 and the secondary pin 4 of the first interface transformer are differenced, the +48V level commonly increased in the signals can be processed, so that a normal communication signal is obtained, and the communication signal is transmitted to the primary pin 1 and the primary pin 2 of the third interface transformer; similarly, communication signals between the secondary side pin 3 and the secondary side pin 4 of the second interface transformer can also be normally transmitted to the primary side pin 1 and the primary side pin 2 of the fourth interface transformer; and a 48V level difference is added between the 2 pairs of differential communication lines, that is, a 48V level difference exists between the primary center tap of the third interface transformer and the primary center tap of the fourth interface transformer, and the power can be supplied to the subsequent powered device through the powered controller. In the embodiment, the intermediate tap of the interface transformer is used for loading or acquiring the power supply energy.
Compared with the prior art, the embodiment has the following beneficial effects:
in the embodiment, the power supply controller is coupled with the power receiving controller through the isolation voltage transformation module, so that the communication between the power supply equipment on the rocket and other equipment is completed through a network cable, and meanwhile, the power supply equipment can supply power to other power receiving equipment, namely, the transmission and power supply control of signals on the rocket can be realized by using a single network cable; because the signal of communication transmission is differential signal, increase the power supply bias on the signal line through the power supply controller, it is equivalent to increasing the common mode interference, so the network communication between the two is not influenced by the power supply mode; meanwhile, the power receiving controller is additionally arranged in the power receiving equipment at the rear end and used for receiving power supply input of the power supply equipment, and the power supply process of the power receiving controller does not affect reliable transmission of signals.
Example two
Fig. 2 is a schematic structural diagram of another power supply and communication device for an electric apparatus on an arrow provided in an embodiment of the present application, and as shown in fig. 2, based on a first embodiment, the isolation transformer module further includes:
a fifth interface transformer T5, a sixth interface transformer T6, a seventh interface transformer T7, and an eighth interface transformer T8;
the primary side of the fifth interface transformer T5 and the primary side of the sixth interface transformer T6 are connected to a communication terminal of a power supply device when in use, the secondary side of the fifth interface transformer T5 is connected to the primary side of the seventh interface transformer T7 through a network cable, the secondary side of the sixth interface transformer T6 is connected to the primary side of the eighth interface transformer T8 through a network cable, the secondary side center tap terminal 5 of the fifth interface transformer T5 is connected to the ground terminal of the power supply controller, and the secondary side center tap terminal 5 of the sixth interface transformer T6 is connected to the second output terminal of the power supply controller; when in use, the secondary side of the seventh interface transformer T7 and the secondary side of the eighth interface transformer T8 are connected to a communication terminal of a powered device, the primary side center tap terminal 5 of the seventh interface transformer T7 is connected to the power input terminal VIN of the powered controller, and the primary side center tap terminal 5 of the eighth interface transformer T8 is connected to the ground terminal of the powered controller.
In this embodiment, the power supply and communication apparatus further includes: a first resistor R1, wherein a first end of the first resistor R1 is connected with a first input end of the power supply controller; a first MOS transistor Q1, a source of the first MOS transistor Q1 is connected to the second end of the first resistor R1, a gate of the first MOS transistor Q1 is connected to the first control end GATEA of the power supply controller, and a drain of the first MOS transistor Q1 is connected to the first output end OUTA of the power supply controller.
In this embodiment, the power supply and communication apparatus further includes: a second resistor R2, wherein a first end of the second resistor R2 is connected with a second input end of the power supply controller; a second MOS transistor Q2, a source of the second MOS transistor Q2 is connected to the second end of the second resistor R2, a gate of the second MOS transistor Q2 is connected to the second control end of the power supply controller, and a drain of the second MOS transistor Q2 is connected to the second output end OUTB of the power supply controller.
In this embodiment, in order to improve the reliability of power supply and communication, two pairs of communication and power supply lines are provided in this embodiment, as shown in fig. 2, a first interface transformer T1, a second interface transformer T2, a third interface transformer T3 and a fourth interface transformer T4 constitute a first pair of communication and power supply lines, a fifth interface transformer T5, a sixth interface transformer T6, a seventh interface transformer T7 and an eighth interface transformer T8 constitute a second pair of communication and power supply lines, and the switching between the first pair of communication and power supply lines and the second pair of communication and power supply lines is realized by controlling the operating states of a first MOS transistor and a second MOS transistor through a power supply controller; for example, if a first control terminal GATEA of the power supply controller outputs a high level and a second control terminal GATEB of the power supply controller outputs a low level, the first MOS transistor is turned on and the second MOS transistor is turned off, so that the first output terminal of the power supply controller outputs a voltage to the secondary side center tap end of the first interface transformer, and the power supply controller selects a first pair of communication and power supply lines; therefore, when the power supply controller detects that the currently working communication and power supply line has faults, the other line can be switched to carry out communication and power supply, and the reliability of the system is improved.
EXAMPLE III
As shown in fig. 2, according to the first embodiment or the second embodiment, the power supply and communication apparatus further includes: the first input end of the first rectifying circuit is connected with the primary side center tap end 5 of the third interface transformer T3, the second input end of the first rectifying circuit is connected with the primary side center tap end 5 of the fourth interface transformer T4, the first output end of the first rectifying circuit is connected with the power supply input end VIN of the power receiving controller, and the second output end of the first rectifying circuit is connected with the grounding end GND of the power receiving controller.
Based on the second embodiment, the power supply and communication apparatus further includes: and a first input end of the second rectifying circuit is connected with the primary side center tap end 5 of the seventh interface transformer T7, a second input end of the second rectifying circuit is connected with the primary side center tap end 5 of the eighth interface transformer T8, a first output end of the second rectifying circuit is connected with a power supply input end VIN of the power receiving controller, and a second output end of the second rectifying circuit is connected with a ground end GND of the power receiving controller.
The first rectifying circuit and the second rectifying circuit are used for rectifying alternating currents output by the first pair of communication and power supply lines and the second pair of communication and power supply lines into direct-current voltages; the first rectifying circuit comprises a rectifying bridge consisting of a first diode D1, a second diode D2, a third diode D3 and a fourth diode D4, the second rectifying circuit comprises a rectifying bridge consisting of a fifth diode D5, a sixth diode D6, a seventh diode D7 and an eighth diode D8, and the specific connection relation is as shown in FIG. 2. In this embodiment, the diode rectifier bridge is added to the power-receiving control end to improve the adaptability of the product and also increase the reliability of the system.
In this embodiment, the power supply and communication apparatus further includes: a first capacitor C1, a first terminal of the first capacitor C1 is connected to the first output terminal of the first rectifying circuit, and a second terminal of the first capacitor C1 is connected to the second output terminal of the first rectifying circuit; the first capacitor C1 is used for filtering the direct current output by the rectifying circuit.
In this embodiment, the power supply and communication apparatus further includes: and the input end of the voltage stabilizing module is connected with the output end VOUT of the power receiving controller, and the output end of the voltage stabilizing module is connected with the power supply end of the power receiving equipment when in use. Wherein the voltage stabilization module comprises: the first end of the voltage stabilization management chip is connected with the output end of the power receiving controller; the positive end of the second capacitor is connected with the output end of the power receiving controller, and the negative end of the second capacitor is grounded; the first end of the inductor is connected with the second end of the voltage stabilization management chip, and the second end of the inductor is connected with a power supply end of the powered device; the cathode of the rectifier diode is connected with the second end of the voltage stabilization management chip, and the anode of the rectifier diode is grounded; and the positive end of the third capacitor is connected with the second end of the inductor, and the negative end of the third capacitor is grounded.
Example four
Fig. 3 is a schematic structural diagram of a power supply and communication system of an arrow-mounted electrical device according to an embodiment of the present disclosure, and as shown in fig. 3, the power supply and communication system includes: the rocket-borne computer, the telemetering device, the attitude control device, the inertial group, the servo controller and the power supply and communication device of the rocket-borne electrical equipment of the embodiment are adopted; the rocket-borne computer is respectively connected with the remote measuring device, the attitude control device, the inertial measurement unit and the servo controller through the power supply and communication device.
It should be noted that, the rocket-borne computer in the present invention adds other power supply and distribution management and control functions on the basis of the original communication core. Specifically, the communication between the rocket computer and other single machines is completed through the network cable by using ideas and methods of active Ethernet (POE, Power On Ethernet) and industrial Ethernet, and the other single machines are powered, namely, signal transmission and Power supply control can be realized by using a single network cable. In addition, except for the rocket-borne computer, other single machines are not directly connected with each other in a power supply and communication mode, so that the communication and power supply among the single machine equipment are determined to be mutually isolated by the hardware characteristics of the scheme, the normal work of other equipment can be guaranteed not to be influenced by the fault of a single design, particularly the reliable operation of the rocket-borne computer, which is the core on the rocket, is not influenced by the fault of other equipment, and the reliability of the system is further enhanced. The communication and power supply system of the electric equipment on the arrow provided by the embodiment can simplify the equipment connection on the arrow, improve the system reliability and shorten the assembly time. As shown in fig. 3, according to the design concept of the present invention, an arrow-mounted computer is used as a core, the conventional communications between the single computers on the arrow, such as RS-422 communications or CAN communications, are unified into industrial ethernet communications based on gigabit ethernet lines as transmission media, and the power supply and distribution management of each single computer is implemented by applying an active ethernet design method. Specifically, a power supply controller is added at a power supply device such as an interface end of an rocket-borne computer for adding power supply bias to a network cable so as to supply power to a single-machine device at the back end. Because the signal transmitted by communication is a differential signal, a power supply bias is added to the signal wire, which is equivalent to increase of common-mode interference, so that the power supply mode does not influence the network communication between the signal wire and the signal wire. Similarly, a power receiving controller is added in the power receiving equipment at the back end for receiving the power supply input of the rocket-borne computer, and the power is supplied to a DC/DC converter at the next stage, and further the specific voltage value actually needed on the board is obtained through conversion, and the power supply process of the power receiving controller does not influence the reliable transmission of signals. Therefore, on the premise of ensuring the communication quality, related cables for power supply transmission are saved, the system connection relationship is simpler, and the complexity of a cable network on the rocket is reduced.
It should be noted that the invention utilizes a network cable to complete high-speed communication and power supply and distribution management between rocket-mounted devices, uses a traditional rocket-mounted computer as a control core of the rocket-mounted devices, and utilizes the network cable to realize information interaction with other single machines and power supply and distribution management of the single machines, namely, the rocket-mounted computer can control power-on of other designs, communicate with other single machines of a network, acquire state information of other single machines and send control instructions. The method can also be adopted to realize the communication and power supply requirements among other single machines on the rocket; because the standards of the POE network are different and the load carrying capacity is different, the implementation can be carried out according to the power consumption of the power receiving end equipment to carry out related device type selection and circuit design work, the scheme implementation proposal is carried out according to the IEEE802.3bt standard, the load end can support the maximum 71.5W power equipment, and the control power supply requirement of the traditional arrow equipment can be met; because the reliability requirement of rocket or missile equipment is high, the interfaces among the equipment can adopt a parallel redundancy design, and the system reliability is further improved; the connection between the devices preferably adopts a reinforced network port and seven or more network cables, so that the reliability of power supply and communication signal transmission of a single machine is reliably and effectively ensured; in order to ensure the reliability of communication, the communication between the rocket-borne computer and other single computers preferably selects industrial Ethernet communication protocols with higher reliability and stronger noise resistance, such as EthercCAT, Profinet and the like; in this embodiment, the arrow indicates that the interface end diode circuits of other single units can be optimized and adjusted to be field effect transistor circuits, so that the power loss on the diodes can be reduced, and the power supply requirements of the single unit product circuits can be guaranteed; the network interface RJ45 type standard interface can be used as a military shielding reinforced network connector, the connection mode of the network connector is generally bayonet or three-head thread connection, and the network connector has the outstanding characteristics of high reliability, environment resistance, vibration impact resistance, high waterproof grade and the like, and can further enhance the adaptability of the network connector in complex electromagnetic and mechanical environments.
Finally, it is noted that, in this document, relational terms such as "first" and "second," and the like, may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although the present invention has been described in detail with reference to the preferred embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the spirit and scope of the invention as defined in the appended claims.

Claims (10)

1. A power supply and communication device for an electrical apparatus on an arrow, the power supply and communication device comprising:
the power supply controller, the power receiving controller and the isolation voltage transformation module;
the input end of the power supply controller is connected with the power supply end of the power supply equipment when in use, and the output end of the power supply controller is connected with the isolation transformation module; the input end of the power receiving controller is connected with the isolation transformation module, and the output end of the power receiving controller is connected with the power supply end of a power receiving device when in use;
the isolation transformation module comprises a first interface transformer, a second interface transformer, a third interface transformer and a fourth interface transformer, wherein the primary side of the first interface transformer and the primary side of the second interface transformer are connected with a communication end of power supply equipment when in use, the secondary side of the first interface transformer is connected with the primary side of the third interface transformer through a network cable, the secondary side of the second interface transformer is connected with the primary side of the fourth interface transformer through a network cable, the central tap end of the secondary side of the first interface transformer is connected with the first output end of the power supply controller, and the central tap end of the secondary side of the second interface transformer is connected with the grounding end of the power supply controller; the secondary side of the third interface transformer and the secondary side of the fourth interface transformer are connected with a communication end of a power receiving device when in use, the primary side center tap end of the third interface transformer is connected with the power input end of the power receiving controller, and the primary side center tap end of the fourth interface transformer is connected with the grounding end of the power receiving controller.
2. The power supply and communication device for the on-rocket electrical equipment according to claim 1, wherein said isolation transformer module further comprises:
a fifth interface transformer, a sixth interface transformer, a seventh interface transformer and an eighth interface transformer;
the primary side of the fifth interface transformer and the primary side of the sixth interface transformer are connected with a communication end of a power supply device when in use, the secondary side of the fifth interface transformer is connected with the primary side of the seventh interface transformer through a network cable, the secondary side of the sixth interface transformer is connected with the primary side of the eighth interface transformer through a network cable, the central tap end of the secondary side of the fifth interface transformer is connected with the grounding end of the power supply controller, and the central tap end of the secondary side of the sixth interface transformer is connected with the second output end of the power supply controller; the secondary side of the seventh interface transformer and the secondary side of the eighth interface transformer are connected with a communication end of a power receiving device when in use, the primary center tap end of the seventh interface transformer is connected with the power input end of the power receiving controller, and the primary center tap end of the eighth interface transformer is connected with the grounding end of the power receiving controller.
3. The power supply and communication device for an on-rocket electrical apparatus according to claim 1, wherein said power supply and communication device further comprises:
the first input end of the first rectifying circuit is connected with the primary side center tap end of the third interface transformer, the second input end of the first rectifying circuit is connected with the primary side center tap end of the fourth interface transformer, the first output end of the first rectifying circuit is connected with the power supply input end of the power receiving controller, and the second output end of the first rectifying circuit is connected with the grounding end of the power receiving controller.
4. The power supply and communication device for an on-rocket electrical apparatus according to claim 2, wherein said power supply and communication device further comprises:
and a first input end of the second rectifying circuit is connected with a primary side center tap end of the seventh interface transformer, a second input end of the second rectifying circuit is connected with a primary side center tap end of the eighth interface transformer, a first output end of the second rectifying circuit is connected with a power supply input end of the power receiving controller, and a second output end of the second rectifying circuit is connected with a grounding end of the power receiving controller.
5. The power supply and communication device for an on-rocket electrical apparatus according to claim 2, wherein said power supply and communication device further comprises:
the first end of the first resistor is connected with the first input end of the power supply controller;
the source electrode of the first MOS tube is connected with the second end of the first resistor, the grid electrode of the first MOS tube is connected with the first control end of the power supply controller, and the drain electrode of the first MOS tube is connected with the first output end of the power supply controller.
6. The power supply and communication device for an on-rocket electrical apparatus according to claim 5, wherein said power supply and communication device further comprises:
a first end of the second resistor is connected with a second input end of the power supply controller;
and the source electrode of the second MOS tube is connected with the second end of the second resistor, the grid electrode of the second MOS tube is connected with the second control end of the power supply controller, and the drain electrode of the second MOS tube is connected with the second output end of the power supply controller.
7. The power supply and communication device for an on-rocket electrical apparatus according to claim 3, wherein said power supply and communication device further comprises:
and the first end of the first capacitor is connected with the first output end of the first rectifying circuit, and the second end of the first capacitor is connected with the second output end of the first rectifying circuit.
8. The power supply and communication device for an electrical apparatus on an arrow according to any one of claims 1 to 7, characterized in that the power supply and communication device further comprises:
and the input end of the voltage stabilizing module is connected with the output end of the power receiving controller, and the output end of the voltage stabilizing module is connected with the power supply end of the power receiving equipment when in use.
9. The power supply and communication device for the on-rocket electrical equipment according to claim 8, wherein the voltage stabilization module comprises:
the first end of the voltage stabilization management chip is connected with the output end of the power receiving controller;
the positive end of the second capacitor is connected with the output end of the power receiving controller, and the negative end of the second capacitor is grounded;
the first end of the inductor is connected with the second end of the voltage stabilization management chip, and the second end of the inductor is connected with a power supply end of the powered device;
the cathode of the rectifier diode is connected with the second end of the voltage stabilization management chip, and the anode of the rectifier diode is grounded;
and the positive end of the third capacitor is connected with the second end of the inductor, and the negative end of the third capacitor is grounded.
10. A power supply and communication system for an electrical device on an arrow, the power supply and communication system comprising:
rocket-borne computers, telemetry means, attitude control means, inertial sets, servo controllers and power supply and communication means for the rocket-borne electrical apparatuses according to claims 1 to 9;
the rocket-borne computer is respectively connected with the remote measuring device, the attitude control device, the inertial measurement unit and the servo controller through the power supply and communication device.
CN202110774337.8A 2021-07-08 2021-07-08 Power supply and communication device and system of electric equipment on arrow Pending CN113541328A (en)

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CN101753319A (en) * 2008-12-18 2010-06-23 启碁科技股份有限公司 Network equipment
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CN207339876U (en) * 2017-08-28 2018-05-08 福建星网物联信息系统有限公司 A kind of cloud terminal based on POE power supplies
CN111314092A (en) * 2020-03-17 2020-06-19 杭州锐格思科技有限公司 PD circuit based on relay control
CN210839610U (en) * 2020-02-18 2020-06-23 广州市迪士普音响科技有限公司 Series Ethernet power supply system
US20200344079A1 (en) * 2019-04-25 2020-10-29 Lifesafety Power, Inc. Access Control Apparatus and Method Therefor

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101753319A (en) * 2008-12-18 2010-06-23 启碁科技股份有限公司 Network equipment
CN102164076A (en) * 2011-03-18 2011-08-24 北京星网锐捷网络技术有限公司 Network interface redundancy realization method, redundant network interface device and switch equipment
CN202817700U (en) * 2012-09-13 2013-03-20 深圳市金威源科技股份有限公司 Power receiving conversion circuit based on power provided by ethernet
CN204425515U (en) * 2015-01-26 2015-06-24 宝鸡石油机械有限责任公司 Based on the measuring truck video monitoring system of Power over Ethernet
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Application publication date: 20211022