CN212540593U - Analog switch device and test system - Google Patents
Analog switch device and test system Download PDFInfo
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- CN212540593U CN212540593U CN202021525072.5U CN202021525072U CN212540593U CN 212540593 U CN212540593 U CN 212540593U CN 202021525072 U CN202021525072 U CN 202021525072U CN 212540593 U CN212540593 U CN 212540593U
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Abstract
The present application relates to an analog switching device and a test system. The device comprises: a separation and combination position detection module; an aviation plug; the aviation plug is used for connecting a control loop aviation socket at the bottom of the distribution automation terminal; the distribution automation terminal is used for outputting a separation and combination position instruction; a secondary cable; the secondary cable is respectively connected with the separation and combination position detection module and the aviation plug; the separation and combination position detection module is conducted after receiving the separation and combination position instruction so as to feed back a separation and combination signal or a division signal to the distribution automation terminal. The utility model provides an analog switch device relies on distribution automation terminal power to provide self working power, need not can detect whether break down for distribution automation terminal with the distribution lines outage, does not influence the user power consumption to device simple structure, convenient to use, labour saving and time saving has improved work efficiency.
Description
Technical Field
The application relates to the technical field of distribution automation, in particular to an analog switch device and a test system.
Background
The automatic complete sets of equipment of 10kV post switch is widely applied to the overhead distribution lines of 10kV, and the equipment is divided into a post switch body, a distribution automation terminal and an outdoor voltage transformer, and secondary aerial plug cables are adopted among all the parts to connect.
When the on-column switch has a closing refusing or opening refusing condition, whether the switch body fault or the terminal control loop fault is judged at first, and due to the fact that a circuit is electrified, the power failure application procedure is complex, and therefore subsequent power failure maintenance work can be carried out only after the body fault is determined, but the switch at the moment is always in an electrified operation condition and cannot be switched on and off through the terminal, so that whether the switch has the fault or not can not be verified, the switch is not operated without the switch, the function of the terminal and the condition of the control loop are not verified, and the work efficiency of field fault detection is seriously affected.
In the implementation process, the inventor finds that at least the following problems exist in the conventional technology:
the existing fault maintenance method for the power distribution automation terminal has the problem of low efficiency.
Disclosure of Invention
In view of the above, it is necessary to provide an analog switch device and a test system for solving the above technical problems.
In order to achieve the above object, in one aspect, an embodiment of the present invention provides an analog switch device, including:
a separation and combination position detection module;
an aviation plug; the aviation plug is used for connecting a control loop aviation socket at the bottom of the distribution automation terminal; the power distribution automation terminal is used for outputting a separation and combination position instruction;
a secondary cable; the secondary cable is respectively connected with the separation and combination position detection module and the aviation plug;
the separation and combination position detection module is conducted after receiving the separation and combination position instruction so as to feed back a separation and combination signal or a separation signal to the distribution automation terminal.
In one of the embodiments, the first and second electrodes are,
the deciliter position detection module comprises a signal activation circuit and a signal output circuit; the signal activation circuit and the signal output circuit are both connected with a secondary cable.
In one embodiment, the secondary cable is connected with a corresponding pin of the aviation socket of the control loop through an aviation plug; the secondary cable is a multi-core cable;
the signal activation circuit comprises a first relay and a second relay;
the negative pole of the first relay, the negative pole of the second relay and the power supply negative pole pin of the control circuit aviation socket are all connected with the same cable in the secondary cables;
the positive pole of the first relay, the positive pole of the second relay and the pin of the positive pole of the power supply of the aviation socket of the control circuit are all connected with the same cable in the secondary cables;
one end of a coil of the first relay is connected with a power supply negative electrode pin of the control loop aviation socket through a secondary cable, and the other end of the coil of the first relay is connected with a position control power supply positive electrode pin of the control loop aviation socket through another secondary cable;
one end of a coil of the second relay is connected with a negative pin of a power supply of the aviation socket of the control circuit through a secondary cable, and the other end of the coil of the second relay is connected with a positive pin of a position-division control power supply of the aviation socket of the control circuit through another secondary cable;
one end of a normally closed contact of the second relay is connected with a normally open contact of the first relay, and the other end of the normally closed contact of the second relay is connected with a power supply positive pin of the control circuit aviation socket through a secondary cable;
one end of the normally closed contact of the first relay is connected with the normally open contact of the second relay, and the other end of the normally closed contact of the first relay is connected with the power supply positive pin of the control circuit aviation socket through a secondary cable.
In one of the embodiments, the first and second electrodes are,
after the pin of the positive electrode of the on-position control power supply is electrified, the coil of the first relay is electrified and attracted, and the signal output circuit is activated to output an on-position signal;
after the pin of the positive electrode of the position-dividing control power supply is electrified, the coil of the second relay is electrified and attracted, and the signal output circuit is activated to output a position-dividing signal;
when the coil of the first relay is electrified and attracted, a normally open contact of the first relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the second relay, a normally open contact of the first relay, the coil of the first relay and a power supply negative electrode of the control loop aviation socket form a first self-holding loop for maintaining the electrified attraction state of the first coil; the normally closed contact of the first relay is disconnected, and the positive power supply of the aviation socket of the control circuit, the normally closed contact of the first relay, the normally open contact of the second relay, the coil of the second relay and the negative power supply of the aviation socket of the control circuit form a first self-holding releasing circuit which is used for releasing the attraction state of the coil of the second relay;
when the coil of the second relay is electrified and attracted, a normally open contact of the second relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the first relay, a normally open contact of the second relay, the coil of the second relay and a power supply negative electrode of the control loop aviation socket form a second self-holding loop for maintaining the electrified attraction state of the second coil; and the normally closed contact of the second relay is disconnected, and the positive power supply of the control circuit aviation socket, the normally closed contact of the second relay, the normally open contact of the first relay, the coil of the first relay and the negative power supply of the control circuit aviation socket form a second self-holding releasing circuit for releasing the attraction state of the coil of the first relay.
In one of the embodiments, the first and second electrodes are,
one end of the other normally open contact of the first relay is connected with a switch on pin of the aviation socket of the control circuit through a secondary cable; one end of the other normally open contact of the second relay is connected with a switch position-dividing pin of the aviation socket of the control circuit through a secondary cable;
the other end of the other normally open contact of the first relay and the other end of the other normally open contact of the second relay are connected with a switch on-off position signal common end pin of the aviation socket of the control circuit through the same secondary cable.
In one embodiment, the device further comprises a guide rail;
the first relay and the second relay are both fixed on the guide rail.
In one embodiment, the terminal block further comprises a secondary terminal block;
the secondary cable is connected with the first relay and the second relay through the secondary terminal strip respectively;
and the secondary terminal strip, the first relay and the second relay are all fixed on the guide rail.
In one embodiment, the secondary cable further comprises a spare cable for expanding access of other signals; the first relay and the second relay are both miniature relays.
An analog switch test system comprises a distribution automation terminal and the analog switch device connected with the distribution automation terminal;
the distribution automation terminal comprises a control loop aviation socket; the control circuit aviation socket is connected with the analog switch device.
In one embodiment, the system further comprises an on-pole switch and an outdoor voltage transformer; the pole-mounted switch and the outdoor voltage transformer are connected with the distribution automation terminal.
One of the above technical solutions has the following advantages and beneficial effects:
this application passes through secondary cable direct access distribution automation terminal bottom's control circuit aviation socket with dividing position detection module, rely on distribution automation terminal power to provide self working power supply, dividing position detection module switches on after receiving the dividing position instruction that distribution automation terminal sent, with to the distribution automation terminal feedback closed position signal or branch position signal, thereby reach under the circumstances that the circuit does not cut off the power supply, replace column switch body divide-shut brake contact to accomplish the debugging work to distribution automation terminal, verify distribution automation terminal have the abnormal so that carry out timely maintenance to it, do not influence user's power consumption, and device simple structure, high durability and convenient use, the work efficiency of the on-the-spot troubleshooting trouble of maintainer has been improved, time saving and labor saving.
Drawings
The foregoing and other objects, features and advantages of the application will be apparent from the following more particular description of preferred embodiments of the application, as illustrated in the accompanying drawings. Like reference numerals refer to like parts throughout the drawings, and the drawings are not intended to be drawn to scale in actual dimensions, emphasis instead being placed upon illustrating the subject matter of the present application.
FIG. 1 is a diagram of an exemplary embodiment of an analog switching device;
FIG. 2 is a block diagram of an analog switching device in one embodiment;
FIG. 3 is a schematic illustration of an aircraft plug in one embodiment;
FIG. 4 is a schematic diagram of a secondary cable connection in one embodiment;
FIG. 5 is a schematic circuit diagram of an analog switching device in one embodiment;
FIG. 6 is a block diagram of an analog switch test system in one embodiment.
Detailed Description
To facilitate an understanding of the present application, the present application will now be described more fully with reference to the accompanying drawings. Embodiments of the present application are set forth in the accompanying drawings. This application may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein in the description of the present application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application.
It will be understood that, as used herein, the terms "first," "second," and the like may be used herein to describe various elements, but these elements are not limited by these terms. These terms are only used to distinguish one element from another.
It will be understood that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or be connected to the other element through intervening elements. Further, "connection" in the following embodiments is understood to mean "electrical connection", "communication connection", or the like, if there is a transfer of electrical signals or data between the connected objects.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs. The terminology used herein in the description of the present application is for the purpose of describing particular embodiments only and is not intended to be limiting of the application. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
On 10KV overhead distribution lines, when the post switch indicates the first kind safety switch who ensures the power consumption safety on the wire pole of being used in, the main effect is the high pressure of buffer circuit, accessible distribution automation terminal opens and shuts the floodgate operation to the post switch, when the post switch appears refusing to close or refusing to divide the condition, need at first judge whether post switch body trouble or distribution automation terminal control circuit trouble, traditional maintenance mode directly carries out the divide-shut operation to the switch through distribution automation terminal, just can carry out subsequent power failure maintenance work after confirming that the post switch body breaks down, because of the circuit is electrified, switch this moment often is in the live working's condition, just will apply for the switch to have a power failure when the on-the-spot maintenance, rethread distribution automation terminal directly carries out the divide-shut operation to the switch and judges. The mode is time-consuming and labor-consuming, the power failure application procedure is complex, the work efficiency of on-site troubleshooting is seriously influenced, and the power utilization of a user is also directly influenced.
In order to make the objects, technical solutions and advantages of the present application more apparent, the present application is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.
The analog switch device and the test system provided by the application can be applied to the application environment shown in fig. 1. The simulation switch device is connected with a control loop aviation socket of the distribution automation terminal through a secondary cable, and after receiving a separation and combination instruction sent by the distribution automation terminal, the simulation switch device feeds back a corresponding combination signal or a separation signal to the distribution automation terminal, and the combination signal or the separation signal is used for indicating the distribution automation terminal to confirm that the body breaks down under the condition that the combination signal or the separation signal is not detected.
In one embodiment, as shown in fig. 2, an analog switch device is provided, which is described by taking the device as an example applied to fig. 1, and may include:
a separation and combination position detection module;
an aviation plug; the aviation plug is used for connecting a control loop aviation socket at the bottom of the distribution automation terminal; the distribution automation terminal is used for outputting a separation and combination position instruction;
a secondary cable; the secondary cable is respectively connected with the separation and combination position detection module and the aviation plug;
the separation and combination position detection module is conducted after receiving the separation and combination position instruction so as to feed back a separation and combination signal or a division signal to the distribution automation terminal.
Specifically, the opening and closing position detection module is used for feeding back a corresponding opening and closing position signal or a corresponding opening position signal to the distribution automation terminal after responding to opening and closing operations of the distribution automation terminal. When need overhaul the maintenance to distribution automation terminal promptly, insert the control circuit aviation socket of distribution automation terminal bottom with analog switch device's aviation plug, after distribution automation terminal goes up the electricity, when pressing distribution automation terminal's divide-shut brake button, distribution automation terminal sends the branch position instruction to analog switch's branch position detection module through the secondary cable, branch position detection module switches on after receiving the branch position instruction that distribution automation terminal sent, convey corresponding closed position signal or the branch position signal to distribution automation terminal through the secondary cable, if distribution automation terminal does not detect corresponding closed position signal or the branch position signal, then confirm distribution automation terminal body and break down.
Wherein, the soldering tin welding of a secondary cable accessible is in aviation plug pin department, aviation plug and aviation socket phase-match, and the control circuit aviation socket of different distribution automation terminal bottoms can have the difference condition, only need to change the aviation plug that corresponds can.
This application relies on distribution automation terminal power to provide self working power through the control circuit aviation socket with analog switch device's aviation plug direct access distribution automation terminal bottom to divide the position instruction through secondary cable reception distribution automation terminal transmission, and to distribution automation terminal feeds back corresponding position signal or the branch position signal of closing, and distribution automation terminal is according to whether detecting corresponding position signal or the branch position signal of closing by dividing the position detection module feedback, judges whether distribution automation terminal breaks down, is convenient for carry out timely maintenance to it, and device simple structure easily carries, has improved the work efficiency that maintainer field investigation trouble.
In a specific embodiment, the deciliter position detection module comprises a signal activation circuit and a signal output circuit; the signal activation circuit and the signal output circuit are both connected with a secondary cable.
Specifically, when pressing distribution automation terminal's combined floodgate button, distribution automation terminal will close the position instruction and send to analog switch deciliter position detection module through the secondary cable, deciliter position detection module's signal activation circuit switches on after receiving the instruction that closes, arouse signal output circuit to switch on and output and close the position signal, transmit to distribution automation terminal through the secondary cable, distribution automation terminal is when detecting this signal that closes, can confirm that distribution automation terminal body state is normal, when not detecting this signal that closes, confirm that the body breaks down, thereby in time overhaul.
When the separating brake button of the distribution automation terminal is pressed down, the distribution automation terminal sends the separating instruction to the analog switch separating and closing position detection module through the secondary cable, the signal activation circuit of the separating and closing position detection module is conducted after receiving the separating instruction, the excitation signal output circuit is conducted and outputs the separating signal, the signal is transmitted to the distribution automation terminal through the secondary cable, the distribution automation terminal can confirm that the state of the distribution automation terminal is normal when detecting the separating signal, when the separating signal is not detected, the body is confirmed to be out of order, and therefore the distribution automation terminal can be overhauled in time.
In a specific embodiment, the secondary cable can be connected with a corresponding pin of the aviation socket of the control loop through the aviation plug; the secondary cable may be a multi-core cable;
the signal activation circuit may include a first relay and a second relay;
the negative pole of the first relay, the negative pole of the second relay and the power supply negative pole pin of the control circuit aviation socket are all connected with the same cable in the secondary cables;
the positive pole of the first relay, the positive pole of the second relay and the pin of the positive pole of the power supply of the aviation socket of the control circuit are all connected with the same cable in the secondary cables;
one end of a coil of the first relay is connected with a power supply negative electrode pin of the control loop aviation socket through a secondary cable, and the other end of the coil of the first relay is connected with a position control power supply positive electrode pin of the control loop aviation socket through another secondary cable;
one end of a coil of the second relay is connected with a negative pin of a power supply of the aviation socket of the control circuit through a secondary cable, and the other end of the coil of the second relay is connected with a positive pin of a position-division control power supply of the aviation socket of the control circuit through another secondary cable;
one end of a normally closed contact of the second relay is connected with a normally open contact of the first relay, and the other end of the normally closed contact of the second relay is connected with a power supply positive pin of the control circuit aviation socket through a secondary cable;
one end of the normally closed contact of the first relay is connected with the normally open contact of the second relay, and the other end of the normally closed contact of the first relay is connected with the power supply positive pin of the control circuit aviation socket through a secondary cable.
Specifically, the control circuit aviation socket of the distribution automation terminal comprises a plurality of pins, the secondary schematic diagram of the distribution automation terminal marks the corresponding definition of each pin of the aviation socket, the pins comprise a power supply negative electrode pin, a power supply positive electrode pin, a combined control power supply positive electrode pin and a separated control power supply positive electrode pin, and the power supply negative electrode pin can also be defined as a combined negative electrode pin or a separated negative electrode pin. And connecting the secondary cable with corresponding connection points of the first relay and the second relay according to the definition of each pin.
And connecting the first relay and the second relay with corresponding pins on a control loop aviation socket of the distribution automation terminal according to the connection mode. When the distribution automation terminal is powered on, the power supply positive pin and the power supply negative pin of the aviation socket are electrified, namely, the whole control circuit is electrified, when a closing button of the distribution automation terminal is pressed, the closing control power supply positive pin of the aviation socket is electrified, the coil of the first relay is electrified and attracted, the excitation signal output circuit is conducted and outputs a closing signal, the closing signal is transmitted to the corresponding pin of the distribution automation terminal through a secondary cable, the distribution automation terminal can confirm that the state of the body of the distribution automation terminal is normal when detecting the closing signal, and when the closing signal is not detected, the body is confirmed to be faulted, so that the maintenance is carried out in time.
When the separating brake button of the distribution automation terminal is pressed, a positive pin of a separating control power supply of the aviation socket is electrified, a coil of the second relay is electrified and attracted, an excitation signal output circuit is conducted and outputs a separating signal, the distribution automation terminal sends the separating instruction to an analog switch separating and combining position detection module through a secondary cable, a signal activation circuit of the separating and combining position detection module is conducted after receiving the separating instruction, the excitation signal output circuit is conducted and outputs the separating signal, the separating signal is transmitted to a corresponding pin of the distribution automation terminal through the secondary cable, the distribution automation terminal can confirm that the state of a distribution automation terminal body is normal when detecting the separating signal, and when the separating signal is not detected, the body is confirmed to be out of order, so that the aerial socket is timely overhauled.
In a specific embodiment, the secondary cable further comprises a spare cable for expanding access of other signals; the first relay and the second relay are both miniature relays.
Specifically, the spare cable can be used for expanding the access of other signals, for example, the access of switch energy storage signal, can increase the spare cable according to the pin and the actual demand of distribution automation terminal aviation socket of different grade type to it can to change corresponding aviation plug according to aviation socket. Under the more condition of secondary cable quantity of using, also can number every secondary cable according to the definition of the aviation socket pin of connecting, use white word pipe box in the outside of every secondary cable and mark, the maintainer of being convenient for is worked a telephone switchboard, improves work efficiency.
The relay can be but not limited to small-size relay, and small-size relay size is less, and weight is lighter, and the maintainer of being convenient for carries, conveniently climbs the pole and uses, also can select suitable type according to the practical application demand.
In a particular embodiment, a guide rail may also be included;
the first relay and the second relay are both fixed on the guide rail.
Specifically, first relay and second relay adopt guide rail type installation, fix on the guide rail, and the material of guide rail is not limited, for the ease of maintainer carries, conveniently climbs the pole, can choose for use the weight lighter and corrosion-resistant aluminium system guide rail etc..
In a specific embodiment, the terminal block further comprises a secondary terminal block;
the secondary cable is connected with the first relay and the second relay through the secondary terminal strip respectively;
and the secondary terminal strip, the first relay and the second relay are all fixed on the guide rail.
The secondary terminal row is convenient for the maintainer to wire, makes the wiring more pleasing to the eye, maintains more convenient and fast.
In a specific embodiment, after a pin of the positive electrode of the on-position control power supply is electrified, a coil of the first relay is electrified and attracted, and the on-position signal is output by the activation signal output circuit;
after the pin of the positive electrode of the position-dividing control power supply is electrified, the coil of the second relay is electrified and attracted, and the signal output circuit is activated to output a position-dividing signal;
when the coil of the first relay is electrified and attracted, a normally open contact of the first relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the second relay, a normally open contact of the first relay, the coil of the first relay and a power supply negative electrode of the control loop aviation socket form a first self-holding loop for maintaining the electrified attraction state of the first coil; the normally closed contact of the first relay is disconnected, and the positive power supply of the aviation socket of the control circuit, the normally closed contact of the first relay, the normally open contact of the second relay, the coil of the second relay and the negative power supply of the aviation socket of the control circuit form a first self-holding releasing circuit which is used for releasing the attraction state of the coil of the second relay;
when the coil of the second relay is electrified and attracted, a normally open contact of the second relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the first relay, a normally open contact of the second relay, the coil of the second relay and a power supply negative electrode of the control loop aviation socket form a second self-holding loop for maintaining the electrified attraction state of the second coil; and the normally closed contact of the second relay is disconnected, and the positive power supply of the control circuit aviation socket, the normally closed contact of the second relay, the normally open contact of the first relay, the coil of the first relay and the negative power supply of the control circuit aviation socket form a second self-holding releasing circuit for releasing the attraction state of the coil of the first relay.
Specifically, when the distribution automation terminal is powered on, under the condition that the coils of the first relay and the second relay are not powered (initial state), a closing button of the distribution automation terminal is pressed, a pin of a positive electrode of a closing control power supply of the aviation socket is electrified, the positive electrode of the closing control power supply, the coil of the first relay and a negative electrode of the power supply form a loop, and the coil of the first relay is powered on and attracted; a normally open contact of the first relay is closed, a normally closed contact of the second relay keeps a closed state, a first self-holding loop is formed by the positive electrode of the power supply, the normally closed contact of the second relay, the closed normally open contact of the first relay, a coil of the first relay and the negative electrode of the power supply, the coil of the first relay is kept continuously electrified, and the signal activation circuit continuously excites the signal output circuit to be conducted and output a closing signal; and the normally closed contact of the first relay is disconnected, and the power supply anode, the normally closed contact of the disconnected first relay, a normally open contact of the second relay, the coil of the second relay and the power supply cathode can not form a loop, so that the signal activation circuit can not be influenced.
When a switching-on button of the distribution automation terminal is pressed in an initial state, and then a switching-off button of the distribution automation terminal is pressed, a pin of a positive electrode of a position-separating control power supply of the aviation socket is electrified, a loop is formed by a positive electrode of the position-separating control power supply, a coil of a second relay and a negative electrode of the power supply, and the coil of the second relay is electrified and pulled in; the first self-holding loop becomes a second self-holding releasing loop, the normally closed contact of the second relay is disconnected, no current passes through the coil of the first relay, and the normally open contact of the closed first relay is disconnected again, so that the attraction state of the coil of the first relay is released; the normally closed contact of the disconnected first relay is closed again, a normally open contact of the second relay is closed, a second self-holding loop is formed by the power supply anode, the normally closed contact of the first relay, the normally open contact of the closed second relay, the coil of the second relay and the power supply cathode, the coil of the second relay is kept electrified continuously, and the signal activation circuit continuously excites the signal output circuit to be conducted and output the position-dividing signal.
When a closing button of the distribution automation terminal is pressed again, a pin of the positive electrode of the closing control power supply of the aviation socket is electrified, the positive electrode of the closing control power supply, a coil of the first relay and the negative electrode of the power supply form a loop again, and the coil of the first relay is electrified and closed; the second self-holding loop becomes a first self-holding releasing loop, the normally closed contact of the first relay is disconnected, no current passes through the coil of the second relay, and the normally open contact of the closed second relay is disconnected again, so that the attraction state of the coil of the second relay is released; the normally closed contact of the disconnected second relay is closed again, a normally open contact of the first relay is closed, the power supply positive electrode, the normally closed contact of the second relay, the normally open contact of the closed first relay, the coil of the first relay and the power supply negative electrode form a first self-holding loop again, the coil of the first relay is kept charged continuously, and the signal activation circuit continuously excites the signal output circuit to be conducted and output a closing signal.
Like above-mentioned operation in-process, if distribution automation terminal can drive first relay and second relay and take place above-mentioned action, and normally detect corresponding deciliter position signal, then can confirm that distribution automation terminal body state is normal, if not detect this closed position signal, then confirm that the body breaks down to in time overhaul.
In a specific embodiment, one end of the other normally open contact of the first relay is connected with a switch on pin of the aviation socket of the control loop through a secondary cable; one end of the other normally open contact of the second relay is connected with a switch position-dividing pin of the aviation socket of the control circuit through a secondary cable;
the other end of the other normally open contact of the first relay and the other end of the other normally open contact of the second relay are connected with a switch on-off position signal common end pin of the aviation socket of the control circuit through the same secondary cable.
Specifically, when a closing button of the distribution automation terminal is pressed in an initial state, the first self-holding loop is conducted, the coil of the first relay keeps an attraction state, the other normally open contact of the first relay is closed, the signal output circuit is conducted, and the switch closing pin outputs a closing signal to the switch closing signal common end.
After a closing button of the distribution automation terminal is pressed, when a separating button of the distribution automation terminal is pressed, the first self-holding loop becomes a second self-holding releasing loop, no current passes through a coil of the first relay, the closing state is not maintained, the other normally open contact of the closed first relay is disconnected again, and a switch closing pin cannot output a closing signal to a switch closing signal public end; and the second self-holding loop is conducted, the coil of the second relay keeps the attraction state, the other normally open contact of the second relay keeps the closed state, the signal output circuit is conducted, and the switch position-dividing pin continuously outputs the position-dividing signal to the switch position-dividing and closing signal public end.
When a switching-on button of the distribution automation terminal is pressed again, the second self-holding loop becomes a first self-holding releasing loop, the coil of the second relay does not pass current any more, the pull-in state is not maintained any more, the other normally open contact of the closed second relay is disconnected again, and the switch position dividing pin cannot output a position dividing signal to the switch position dividing and combining signal common end; and the first self-holding loop is conducted again, the coil of the first relay maintains the attraction state again, the other normally open contact of the first relay maintains the closed state again, the signal output circuit is conducted, and the switch closing pin continuously outputs the closing signal to the switch closing signal public end again.
If when the switching-off and switching-on button of the distribution automation terminal is operated, the distribution automation terminal detects corresponding switching-off and switching-on signals, the normal state of the distribution automation terminal body can be confirmed, and if the switching-off and switching-on signals are not detected, the body is confirmed to be broken down, so that the maintenance is carried out in time.
In a specific example, as shown in fig. 3, the aviation plug of the analog switch device is a 10-core plug, that is, 10-core cables can be used for connection, and each cable is sequentially sleeved with a white character code tube according to the number from 1 to 10 and marked.
As shown in fig. 4, according to the pin definitions of the control loop aviation socket at the bottom of the distribution automation terminal, the first and the second cables are defined as switch closing position (HW) and switch opening position (FW), the third and the fourth cables are defined as power negative (CN-) and power positive (CN +), the power voltage is 24V in the application scenario, the fifth cable is defined as standby, the sixth cable is defined as switch closing and opening signal common (YXCOM), the seventh and the eighth cables are defined as closing control power negative (CN-) and closing control power positive (HZ +), i.e. closing output-and closing output in fig. 4, and the ninth and the tenth cables are defined as opening control power negative (CN-) and opening control power positive (FZ +), i.e. opening output-and opening output in fig. 4, respectively, each corresponding cable is connected to the aviation plug in fig. 3, the conductor cross-sectional area of the secondary cable is 1.5 square millimeters. It should be noted that the first cable, the second cable, etc. in this application may be used herein to describe each of the secondary cables (e.g., multi-core cables), but these cables are not limited by these terms. These terms are only used to distinguish a first cable from another cable.
As shown in fig. 5, two relays (the first relay is 1ZJ, and the second relay is 2ZJ) are used to simulate the switching-on/off coil of the pole-mounted switch, the working voltage of the relay is 24V in the application scenario, the rated current is not less than 5A, and the corresponding secondary cable is connected to the corresponding connection position of the relay according to fig. 4. When the distribution automation terminal is powered on, CN + and CN-are powered on, namely the whole control loop is powered on, if a closing button of the distribution automation terminal is pressed at the moment, HZ + is powered on, and at the moment, 1ZJ
The two ends of the coil are electrified and attracted, CN +, a closed normally closed contact (R) of 2ZJ, a closed normally open contact (ninu, fifu) of 1ZJ and a coil of 1ZJ
And CN-forming a first self-sustaining loop, 1ZJ
Two ends of the coil are electrified and attracted to drive another normally open contact (R) of 1ZJ to close, so that HW signal is transmitted to distribution automation terminal, and the closing signal is kept unchanged by first self-holding loop.
If the opening button of the distribution automation terminal is pressed at the moment, FZ + is electrified, 1ZJ is electrified, and the self-holding is released, and at the moment, 2ZJ
The two ends of the coil are electrified and attracted, CN +, a closed normally closed contact (R) of 1ZJ and a closed normally open contact (R) of 2ZJPoint (ninu, fifu) and 2ZJ coil
And CN-forming a second self-sustaining loop, 2ZJ
Two ends of the coil are electrified and attracted to drive another normally open contact (R & C & lt 2 & gt) of 2ZJ to close, so that the FW signal is transmitted to the distribution automation terminal, and the branch position signal is kept unchanged through a second self-holding loop.
If the distribution automation terminal detects the corresponding separation and combination signals during the operation, the distribution automation terminal can be determined not to have faults; if the distribution automation terminal does not detect the corresponding separation and combination position signal, the distribution automation terminal can be determined to have a fault and needs to be maintained timely. The on-site test of the distribution automation terminal is completed in a matching way by replacing the on-column switch.
This application is received respectively with a pair of normally open contact and normally closed contact between first relay and the second relay through the connected mode of establishing ties in the return circuit that closing self-sustaining and separating brake self-sustaining removed, the purpose of this connected mode is when pressing the divide-shut brake button at distribution automation terminal, can remove the working power supply of the coil of another relay when the relay coil that self-sustaining corresponds is electrified, represent like this that the contact of switch closing position and switch separating position just can carry out corresponding action change according to the button of pressing, simultaneously with corresponding signal transmission to distribution automation terminal.
More than, this application relies on distribution automation terminal power to provide self working power supply through the control circuit aviation socket with analog switch device's aviation plug direct access distribution automation terminal bottom, directly utilizes the divide-shut brake button on the distribution automation terminal to control, whether the function and the control circuit that detect the distribution automation terminal body are normal, the analog switch device of this application has simple structure, small, light in weight, convenient to use, easily carry, improve work efficiency's advantage.
In one embodiment, as shown in fig. 6, there is provided an analog switch testing system, which may include a distribution automation terminal and an analog switch device as described above connected to the distribution automation terminal;
the distribution automation terminal comprises a control loop aviation socket; the control circuit aviation socket is connected with the analog switch device. The specific structure of the analog switch device has been described in detail above, and thus is not described again.
Specifically, through inserting analog switch device's aviation plug in the control circuit aviation socket of distribution automation terminal bottom, distribution automation terminal goes up the electricity back, when pressing distribution automation terminal's closing button, if distribution automation terminal detects the closed position signal that analog switch device sent, then can confirm that distribution automation terminal body state is normal, when not detecting this closed position signal, confirms that the body breaks down. When the separating brake button of the distribution automation terminal is pressed, if the distribution automation terminal detects a separating signal sent by the analog switch device, the normal state of the distribution automation terminal body can be confirmed, and when the separating signal is not detected, the body is confirmed to be broken down, so that the maintenance and repair are carried out on the body, and the subsequent maintenance work is carried out.
In a specific embodiment, the system also comprises an on-pole switch and an outdoor voltage transformer; the pole-mounted switch and the outdoor voltage transformer are connected with the distribution automation terminal.
Specifically, when the pole switch appears refusing to close or refuse the condition of branch, the maintainer can carry the analog switch device of this application and test on the pole, insert analog switch device's aviation plug on distribution automation terminal's control circuit aviation socket and carry out test operation, distribution automation terminal is gone up the electricity after, when pressing distribution automation terminal's divide-shut brake button, if distribution automation terminal detects the corresponding divide-shut position signal that analog switch device sent, then can confirm that distribution automation terminal body state is normal, the problem that the pole switch refused to close or refuse the branch appears probably is that the pole switch body breaks down, the maintainer needs to maintain the pole switch. If the distribution automation terminal does not detect the corresponding on-off position signal sent by the analog switch device, the distribution automation terminal is confirmed to be out of order, and the maintainer needs to maintain the distribution automation terminal and then perform subsequent debugging work.
In summary, when the on-column switch is turned on or turned off, the aviation plug of the analog switch device is directly connected to the control loop aviation socket at the bottom of the distribution automation terminal, the power supply of the distribution automation terminal is used for providing working power, the dividing and combining position command sent by the distribution automation terminal is received through the secondary cable, the corresponding dividing and combining position signal is fed back to the distribution automation terminal, the distribution automation terminal judges whether the distribution automation terminal body fails according to whether the corresponding dividing and combining position signal fed back by the dividing and combining position detection module is detected, and the dividing and combining of the on-column switch are replaced in the mode to complete the field test of the distribution automation terminal in a matching mode. This application device simple structure, small, light in weight carry when conveniently climbing the pole to need not cut off the power supply line among the test procedure, do not influence the user power consumption, labour saving and time saving has alleviateed the field operation personnel's the work degree of difficulty and has improved work efficiency.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
The above-mentioned embodiments only express several embodiments of the present application, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
1. An analog switching device, comprising:
a separation and combination position detection module;
an aviation plug; the aviation plug is used for connecting a control loop aviation socket at the bottom of the distribution automation terminal; the distribution automation terminal is used for outputting a separation and combination position instruction;
a secondary cable; the secondary cable is respectively connected with the separation and combination position detection module and the aviation plug;
the separation and combination position detection module is conducted after receiving the separation and combination position instruction so as to feed back a separation and combination signal or a division signal to the distribution automation terminal.
2. The analog switching device according to claim 1,
the deciliter position detection module comprises a signal activation circuit and a signal output circuit; the signal activation circuit and the signal output circuit are both connected with the secondary cable.
3. The analog switch device of claim 2, wherein the secondary cable is connected to a corresponding pin of the control loop aviation socket through the aviation plug; the secondary cable is a multi-core cable;
the signal activation circuit comprises a first relay and a second relay;
the negative electrode of the first relay, the negative electrode of the second relay and the power supply negative electrode pin of the control circuit aviation socket are connected with the same cable in the secondary cables;
the positive pole of the first relay, the positive pole of the second relay and the power supply positive pole pin of the control loop aviation socket are all connected with the same cable in the secondary cables;
one end of a coil of the first relay is connected with a power supply negative electrode pin of the control loop aviation socket through the secondary cable, and the other end of the coil of the first relay is connected with a closed control power supply positive electrode pin of the control loop aviation socket through the other secondary cable;
one end of a coil of the second relay is connected with a power supply negative electrode pin of the control loop aviation socket through the secondary cable, and the other end of the coil of the second relay is connected with a position-division control power supply positive electrode pin of the control loop aviation socket through another secondary cable;
one end of a normally closed contact of the second relay is connected with a normally open contact of the first relay, and the other end of the normally closed contact of the second relay is connected with a power supply positive pin of the control circuit aviation socket through the secondary cable;
one end of the normally closed contact of the first relay is connected with the normally open contact of the second relay, and the other end of the normally closed contact of the first relay is connected with the power supply positive pin of the control circuit aviation socket through the secondary cable.
4. The analog switching device according to claim 3,
after the pin of the positive electrode of the on-position control power supply is electrified, the coil of the first relay is electrified and attracted, and the signal output circuit is activated to output the on-position signal;
after the positive pin of the position-dividing control power supply is electrified, the coil of the second relay is electrified and attracted, and the signal output circuit is activated to output the position-dividing signal;
when the coil of the first relay is electrified and attracted, a normally open contact of the first relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the second relay, a normally open contact of the first relay, the coil of the first relay and a power supply negative electrode of the control loop aviation socket form a first self-holding loop for maintaining the electrified attraction state of the first coil; the normally closed contact of the first relay is disconnected, and the positive electrode of the power supply of the control circuit aviation socket, the normally closed contact of the first relay, the normally open contact of the second relay, the coil of the second relay and the negative electrode of the power supply of the control circuit aviation socket form a first self-holding releasing loop for releasing the attraction state of the coil of the second relay;
when the coil of the second relay is electrified and attracted, a normally open contact of the second relay is closed, and a power supply positive electrode of the control loop aviation socket, a normally closed contact of the first relay, a normally open contact of the second relay, the coil of the second relay and a power supply negative electrode of the control loop aviation socket form a second self-holding loop for maintaining the electrified attraction state of the second coil; the normally closed contact disconnection of second relay, the power positive pole of control circuit aviation socket the normally closed contact of second relay a normally open contact of first relay the coil of first relay and the power negative pole of control circuit aviation socket forms second self-sustaining and removes the return circuit, is used for removing the actuation state of the coil of first relay.
5. The analog switching device according to claim 4,
one end of the other normally open contact of the first relay is connected with a switch on pin of the aviation socket of the control circuit through the secondary cable; one end of the other normally open contact of the second relay is connected with a switch position-dividing pin of the aviation socket of the control circuit through the secondary cable;
the other end of the other normally open contact of the first relay and the other end of the other normally open contact of the second relay are connected with a switch on-off position signal common end pin of the aviation socket of the control circuit through the same secondary cable.
6. The analog switching device according to any one of claims 3 to 5, further comprising a guide rail;
the first relay and the second relay are both fixed on the guide rail.
7. The analog switching device of claim 6, further comprising a secondary terminal block;
the secondary cable is connected with the first relay and the second relay through the secondary terminal strip respectively;
the secondary terminal strip, the first relay and the second relay are all fixed on the guide rail.
8. An analogue switch device according to any one of claims 3 to 5, characterised in that the secondary cable further comprises a reserve cable for extending access to other signals; the first relay and the second relay are both miniature relays.
9. An analog switch test system comprising a distribution automation terminal and an analog switch device according to any one of claims 1 to 8 connected to the distribution automation terminal;
the distribution automation terminal comprises a control loop aviation socket; the control loop aviation socket is connected with the analog switch device.
10. The analog switch testing system of claim 9, further comprising a pole top switch and an outdoor voltage transformer; the pole top switch and the outdoor voltage transformer are connected with the distribution automation terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021525072.5U CN212540593U (en) | 2020-07-28 | 2020-07-28 | Analog switch device and test system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202021525072.5U CN212540593U (en) | 2020-07-28 | 2020-07-28 | Analog switch device and test system |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112185069A (en) * | 2020-09-29 | 2021-01-05 | 浙江工业职业技术学院 | Circuit early warning system |
| CN113009381A (en) * | 2021-03-10 | 2021-06-22 | 中国人民解放军海军航空大学青岛校区 | Aviation wire ground setting device |
-
2020
- 2020-07-28 CN CN202021525072.5U patent/CN212540593U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112185069A (en) * | 2020-09-29 | 2021-01-05 | 浙江工业职业技术学院 | Circuit early warning system |
| CN113009381A (en) * | 2021-03-10 | 2021-06-22 | 中国人民解放军海军航空大学青岛校区 | Aviation wire ground setting device |
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Address after: No.11, nanshai Road, Haizhu District, Guangzhou, Guangdong 510300 Patentee after: Guangzhou Southern POWER Group Electric Apparatus Co.,Ltd. Address before: No.11, nanshai Road, Haizhu District, Guangzhou, Guangdong 510300 Patentee before: GUANGZHOU SOUTHERN POWER GROUP ELECTRIC APPARATUS CO.,LTD. |