CN105024452B - DC uninterrupted power supply method and line - Google Patents

DC uninterrupted power supply method and line Download PDF

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Publication number
CN105024452B
CN105024452B CN201510489134.9A CN201510489134A CN105024452B CN 105024452 B CN105024452 B CN 105024452B CN 201510489134 A CN201510489134 A CN 201510489134A CN 105024452 B CN105024452 B CN 105024452B
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busbar
direct current
normal
uninterrupted
time delay
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CN105024452A (en
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牛晓帆
柴和平
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Xian Aircraft Design and Research Institute of AVIC
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Xian Aircraft Design and Research Institute of AVIC
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Abstract

The invention provides a DC uninterrupted power supply method and line. The DC uninterrupted power supply line comprises a DC uninterrupted bus bar, a time-delay disconnection relay, a DC emergency bus bar, at least one DC normal bus bar and at least one diode. Each DC normal bus bar is connected with the time-delay disconnection relay via one diode corresponding to the DC normal bus bar. The two contacts of the time-delay disconnection relay are respectively connected with the DC emergency bus bar and the DC uninterrupted bus bar under the condition that the time-delay disconnection relay is powered on, wherein the DC emergency bus bar is connected with an emergency power supply, and the at least one DC normal bus bar is connected with a power supply. With application of the DC uninterrupted power supply line, problems in the prior art that electricity utilization equipment is large in size, high in weight and high in cost are solved so that the effects of simplifying the system design and enhancing economical efficiency are achieved.

Description

DC uninterrupted method of supplying power to and circuit
Technical field
The present invention relates to circuit field, in particular to a kind of DC uninterrupted method of supplying power to and circuit.
Background technology
In prior art, aircraft DC power-supply system is generally met an urgent need by direct current normal power source, direct-current ground power supply and direct current The part of power supply three constitutes, and for security consideration, typically direct current normal power source and direct-current ground power supply is not allowed in system design Power to electrical network on machine simultaneously.
Fig. 1 is the connection diagram of the aircraft DC power-supply system list normal power source channel configurations according to correlation technique, such as Shown in Fig. 1, DC generator (or vertoro) 1 is connected by catalyst 4 with the normal busbar 8 of direct current in figure, direct current ground Face power supply 2 is connected by catalyst 5 with the normal busbar 8 of direct current, and accumulator 3 is connected by the emergent busbar 9 of catalyst 6 and direct current Connect, the normal busbar 8 of direct current is connected by the emergent busbar 9 of diode 7 and direct current.
When DC generator (or vertoro) 1 is to aviation power supply, catalyst 4 is connected, and catalyst 5 disconnects, direct current Electromotor (or vertoro) 1 is powered by catalyst 4 to the normal busbar 8 of direct current;Supply to aircraft in direct-current ground power supply 2 When electric, catalyst 4 disconnects, and catalyst 5 is connected, and direct-current ground power supply 2 is powered by catalyst 5 to the normal busbar 8 of direct current;Appoint In the case of what, the emergent busbar 9 of direct current is entered by catalyst 6 or the normal busbar 8 of direct current by accumulator 3 by diode 7 Row power supply.Because catalyst 4,5 does not allow to be also turned on, aircraft is being changed by the power supply of DC generator (or vertoro) 1 It is to be powered or be converted to DC generator (or vertoro) 1 by the power supply of direct-current ground power supply 2 to power by direct-current ground power supply 2 During, the normal busbar 8 of direct current occurs short term outage.
Fig. 2 is the connection signal of the non-parallel architecture of the double normal power source passages of aircraft DC power-supply system according to correlation technique Figure, as shown in Fig. 2 DC generator (or vertoro) 1 is connected by catalyst 5 with the normal busbar 12 of direct current, direct current Electromotor (or vertoro) 2 is connected by catalyst 6 with the normal busbar 13 of direct current, and direct-current ground power supply 3 is by contact Device 7 is connected with the normal busbar 12 of direct current, and accumulator 4 is connected by the emergent busbar 14 of catalyst 8 and direct current, and direct current normally converges Stream bar 12 is connected by catalyst 9 with the normal busbar 13 of direct current, and the normal busbar 12 of direct current should with direct current by diode 10 Anxious busbar 14 connects, and the normal busbar 13 of direct current is connected by the emergent busbar 14 of diode 11 and direct current.
When DC generator (or vertoro) 1,2 is to aviation power supply, catalyst 7,9 disconnects, and catalyst 5,6 connects Logical, DC generator (or vertoro) 1,2 is powered respectively by catalyst 5,6 to the normal busbar 12,13 of direct current.Straight When stream ground power supply 3 is to aviation power supply, catalyst 5,6 disconnects, and catalyst 7,9 is connected, and direct-current ground power supply 3 passes through catalyst 7 Power to the normal busbar 12 of direct current, the normal busbar 12 of direct current is powered by catalyst 9 to the normal busbar 13 of direct current.It is any In the case of, the emergent busbar 14 of direct current passes through respectively two by accumulator 4 by catalyst 8 or the normal busbar 12,13 of direct current Pole pipe 10,11 is powered.When DC generator (or vertoro) 1 fails, catalyst 5 disconnects, and catalyst 9 is connected, The normal busbar 13 of direct current is powered by catalyst 9 to the normal busbar 12 of direct current, in the process the normal busbar 12 of direct current Short term outage occurs;When DC generator (or vertoro) 2 fails, catalyst 6 disconnects, and catalyst 9 is connected, The normal busbar 12 of direct current is powered by catalyst 9 to the normal busbar 13 of direct current, in the process the normal busbar 13 of direct current Short term outage occurs;Further, since catalyst 5,6 does not allow to be also turned on catalyst 7,9, aircraft is being sent out by direct current The power supply of motor (or vertoro) 1,2 is converted to be powered by direct-current ground power supply 3 or is converted to by the power supply of direct-current ground power supply 3 In the power supply process of DC generator (or vertoro) 1,2, the normal busbar 12,13 of direct current occurs in short-duration power It is disconnected.
In correlation technique, other many normal power source channel configurations of aircraft DC power-supply system are on direct-current ground power supply and machine When each normal power source passage is powered conversion each other on normal power source interchannel or machine, also all can inevitably occur short When power failure.For being powered by the normal busbar of direct current on aircraft and requiring the electrical equipment of continuous work, in order to be able to It is enough to continue normal work during power failure, it is necessary to accumulator to be set in interiors of products, but so, can be increased again The volume of electrical equipment, weight and cost.
The content of the invention
The invention provides a kind of DC uninterrupted method of supplying power to and circuit, at least to solve electrical equipment in correlation technique Volume is big, weight big and the problem of high cost.
According to an aspect of the invention, there is provided a kind of DC uninterrupted supply line, including:It is DC uninterrupted to conflux Bar, time delay disconnect relay, direct current emergent busbar, the normal busbar of at least one direct current, at least one diode;Each Being connected by an its corresponding diode and time delay disconnection relay for the normal busbar of direct current, it is disconnected in the time delay In the case of the connection of open relay, the time delay disconnect two contacts of relay respectively with the emergent busbar of the direct current and The DC uninterrupted busbar is connected;Wherein, the emergent busbar of the direct current is connected with emergency power supply, and described at least one is straight Flow normal busbar to be connected with power supply.
Preferably, it is defeated by an its corresponding diode after electricity on the normal busbar of at least one direct current Go out unidirectional current control time delay and disconnect relay connection, the emergent busbar of the direct current disconnects relay to the direct current by time delay Uninterrupted busbar is powered;After the normal busbar dead electricity of at least one direct current, relay is disconnected by the time delay and is existed Remain up in first time period, the emergent busbar of the direct current disconnects relay in the first time period by the time delay Device to the DC uninterrupted busbar is powered.
Preferably, on the normal busbar of at least one direct current after electricity, the normal busbar of at least one direct current Voltage higher than the DC uninterrupted busbar voltage, the normal busbar of at least one direct current and the direct current not between Disconnected busbar is powered to electrical equipment.
Preferably, the situation of the normal busbar dead electricity of at least one direct current includes one below:One direct current is normal Busbar is in the situation for switching to occur dead electricity during the DC source passage by other normal works is powered;The direct current is just Often busbar powered by direct-current ground power supply switch to be powered by electromotor on aircraft or vertoro during occur losing The situation of electricity.
Preferably, in the case of the normal busbar dead electricity of at least one direct current, at least one direct current normally converges Stream bar can not export unidirectional current and control the time delay disconnection relay connection by corresponding diode.
According to a further aspect in the invention, there is provided a kind of method of DC uninterrupted power supply, including:Between providing direct current not Disconnected busbar, time delay disconnect relay, direct current emergent busbar, the normal busbar of at least one direct current, at least one diode; The normal busbar of each direct current disconnects relay and is connected by an its corresponding diode and the time delay, described In the case that time delay disconnects the connection of relay, the time delay disconnects two contacts of relay and meets an urgent need with the direct current respectively and converges Stream bar is connected with the DC uninterrupted busbar;Wherein, the emergent busbar of the direct current is connected with emergency power supply, it is described at least The normal busbar of one direct current is connected with power supply.
Preferably, after electricity on the normal busbar of at least one direct current, by described its corresponding diode Output unidirectional current control time delay disconnects relay and connects, the emergent busbar of the direct current by time delay disconnect relay to it is described directly Flow uninterrupted busbar to power;After the normal busbar dead electricity of at least one direct current, by the time delay disconnect after Electrical equipment is remained up in first time period, and the emergent busbar of the direct current is disconnected by the time delay in the first time period Open relay to the DC uninterrupted busbar is powered.
Preferably, on the normal busbar of at least one direct current after electricity, the normal busbar of at least one direct current Voltage higher than the DC uninterrupted busbar voltage, the normal busbar of at least one direct current and the direct current not between Disconnected busbar is powered to electrical equipment.
Preferably, the situation of the normal busbar dead electricity of at least one direct current includes one below:One direct current is normal Busbar is in the situation for switching to occur dead electricity during the DC source passage by other normal works is powered;The direct current is just Often busbar powered by direct-current ground power supply switch to be powered by electromotor on aircraft or vertoro during occur losing The situation of electricity.
Preferably, in the case of the normal busbar dead electricity of at least one direct current, at least one direct current normally converges Stream bar can not export unidirectional current and control the time delay disconnection relay connection by corresponding diode.
By the present invention, using DC uninterrupted supply line, the circuit includes:DC uninterrupted busbar, time delay are broken Open relay, direct current are met an urgent need busbar, the normal busbar of at least one direct current, at least one diode;Each direct current is normal Being connected by an its corresponding diode and time delay disconnection relay for busbar, the connection of relay is disconnected in time delay In the case of, time delay disconnects two contacts of relay and is connected with the emergent busbar of direct current and DC uninterrupted busbar respectively;Its In, the emergent busbar of direct current is connected with emergency power supply, and the normal busbar of at least one direct current is connected with power supply, solves related skill The volume of electrical equipment is big in art, weight is big and high cost problem, and then reached simplified system design, improved economy Effect.
Description of the drawings
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, this Bright schematic description and description does not constitute inappropriate limitation of the present invention for explaining the present invention.In the accompanying drawings:
Fig. 1 is the connection diagram of the aircraft DC power-supply system list normal power source channel configurations according to correlation technique;
Fig. 2 is the connection signal of the non-parallel architecture of the double normal power source passages of aircraft DC power-supply system according to correlation technique Figure;
Fig. 3 is the circuit diagram of DC uninterrupted supply line according to embodiments of the present invention;
Fig. 4 is another connection diagram of uninterrupted power supply circuit according to embodiments of the present invention.
Specific embodiment
Below with reference to accompanying drawing and in conjunction with the embodiments describing the present invention in detail.It should be noted that not conflicting In the case of, the feature in embodiment and embodiment in the application can be mutually combined.
In order to solve the electrical equipment of the continuous work of requirement on aircraft to adapt to be produced when DC power system is powered and changed Short term outage and arranging accumulator in interiors of products causes the problem that aircraft system design is complicated, economy is reduced, A kind of aircraft DC uninterrupted power supply circuit is embodiments provided, can be carried to the electrical equipment for having continuous job requirement For uninterrupted power supply, thus can eliminate this part electrical equipment interiors of products arrange the volume that accumulator brought, Weight and cost overhead, so as to simplify the system design of aircraft, improve the economy of aircraft.
A kind of DC uninterrupted method of supplying power to being applied on aircraft is embodiments provided, the method includes:Carry For a DC uninterrupted busbar, a time delay disconnects relay, the emergent busbar of direct current, and with aircraft DC electricity The corresponding diode of origin system normal power source number of channels, the normal busbar of direct current.The normal busbar of the direct current passes through two poles Pipe output unidirectional current control time delay disconnects the break-make of relay, the emergent busbar of direct current by time delay disconnection relay to direct current not Interruption busbar is powered.
For aircraft DC power-supply system list normal power source channel configurations, after electricity on the normal busbar of direct current, lead to Cross diode output unidirectional current control time delay and disconnect relay and connect, make the emergent busbar of direct current by time delay disconnection relay to DC uninterrupted busbar is powered, from DC uninterrupted busbar and the normal busbar of direct current jointly to there is uninterrupted power supply requirement Electrical equipment (hereinafter referred to as uninterrupted electrical equipment) power supply.The normal busbar of direct current switchs to being powered by direct-current ground power supply Occur after dead electricity during being powered by normal power source on machine (electromotor or vertoro), it is impossible to straight by diode output Stream electric control time delay disconnects relay and connects, and now time delay disconnects relay can be in a timing based on its own time delay turn-off characteristic It is interior to continue to remain up, make DC uninterrupted busbar still be powered by the emergent busbar of direct current, in the process by direct current not Interruption busbar is individually powered to uninterrupted electrical equipment;After the normal busbar of direct current switchs to by normal power source is powered on machine, Again by diode output unidirectional current control time delay disconnect relay connect, now uninterrupted electrical equipment revert to again by DC uninterrupted busbar and the normal busbar of direct current are powered jointly.
For many normal power source channel configurations of aircraft DC power-supply system, when electricity on the normal busbar of arbitrary direct current Afterwards, unidirectional current is exported by corresponding diode and controls time delay disconnection relay connection, make the emergent busbar of direct current pass through time delay Disconnect relay to power to DC uninterrupted busbar, the normal busbar of each direct current after DC uninterrupted busbar and upper electricity is total to In the same direction uninterrupted electricity supply and use equipment is powered.The normal busbar of each direct current switchs to by normal electricity on machine being powered by direct-current ground power supply Source (electromotor or vertoro) occurs after dead electricity during powering, it is impossible to export DC controlled by corresponding diode Time delay processed disconnects relay and connects, now time delay disconnect relay based on its own time delay turn-off characteristic can within a certain period of time after It is continuous to remain up, make DC uninterrupted busbar still be powered by the emergent busbar of direct current, in the process by DC uninterrupted remittance Stream bar is individually powered to uninterrupted electrical equipment;After the normal busbar of each direct current switchs to by normal power source is powered on machine, again Unidirectional current is exported by diode and controls time delay disconnection relay connection, now uninterrupted electrical equipment is reverted to by direct current again Uninterrupted busbar and the normal busbar of direct current are powered jointly.After arbitrary normal power source channel failure, the power channel it is straight Flow normal busbar after switching to dead electricity occur during the DC source passage by other normal works is powered, by other just Often the normal busbar of direct current of power channel exports unidirectional current and controls time delay disconnection relay connection by respective diode, makes straight Flow uninterrupted busbar still to be powered by the emergent busbar of direct current, now the uninterrupted electrical equipment of trouble power passage by direct current not Interruption busbar is individually powered;The normal busbar of direct current of pending fault power channel switchs to be powered by other normal power source passages Afterwards, the uninterrupted electrical equipment of the power channel reverts to common by DC uninterrupted busbar and the normal busbar of direct current again Power supply.
Fig. 3 is the circuit diagram of DC uninterrupted supply line according to embodiments of the present invention, as shown in figure 3, this is straight Stream uninterrupted power supply circuit includes that the 1, time delay of a DC uninterrupted busbar disconnects the emergent remittance of 2, direct current of relay The normal busbar 5 of the stream direct current of diode 4, of bar 3,.
After electricity on the normal busbar 5 of direct current, unidirectional current control time delay disconnection relay 2 is exported by diode 4 and is connected, Make the emergent busbar 3 of direct current disconnect relay 2 by time delay to power to DC uninterrupted busbar 1, confluxed by DC uninterrupted Bar 1 and the normal busbar 5 of direct current are powered to uninterrupted electrical equipment jointly.The normal busbar 5 of direct current is by direct-current ground power supply Power supply switch to by normal power source on machine (electromotor or vertoro) power during occur after dead electricity, it is impossible to by two poles The output unidirectional current control time delay of pipe 4 disconnects relay 2 and connects, and now time delay disconnection relay 2 is disconnected special based on its own time delay Property can continue within a certain period of time to remain up, make DC uninterrupted busbar 1 still be powered by the emergent busbar 3 of direct current, here During individually powered to uninterrupted electrical equipment from DC uninterrupted busbar 1;Treat that the normal busbar 5 of direct current switchs to by machine After normal power source is powered, disconnect relay 2 again by the output unidirectional current control time delay of diode 4 and connect, now uninterruptedly use Electric equipment is reverted to again is powered jointly by DC uninterrupted busbar 1 and the normal busbar 5 of direct current.
Fig. 4 is another connection diagram of uninterrupted power supply circuit according to embodiments of the present invention, as shown in figure 4, when straight Flow on normal busbar 5,7 after electricity, unidirectional current control time delay disconnection relay 2 is exported by diode 4,6 and is connected, answer direct current Anxious busbar 3 disconnects relay 2 and powers to DC uninterrupted busbar 1 by time delay, after DC uninterrupted busbar 1 and upper electricity The normal busbar 5,7 of direct current power to uninterrupted electricity supply and use equipment jointly.The normal busbar 5,7 of direct current is by direct-current ground electricity Source power switch to by normal power source on machine (electromotor or vertoro) power during occur after dead electricity, it is impossible to by two The output unidirectional current control time delay of pole pipe 4,6 disconnects relay 2 and connects, and it is disconnected based on its own time delay that now time delay disconnects relay 2 It is opening characteristic to continue within a certain period of time to remain up, make DC uninterrupted busbar 1 still be powered by the emergent busbar 3 of direct current, Individually powered to uninterrupted electrical equipment from DC uninterrupted busbar 1 in the process;Treat that the normal busbar 5,7 of direct current switchs to After being powered by normal power source on machine, disconnect relay 2 again by the output unidirectional current control time delay of diode 4,6 and connect, now Uninterrupted electrical equipment is reverted to again is powered jointly by DC uninterrupted busbar 1 and the normal busbar 5,7 of direct current.
After arbitrary normal power source channel failure, the normal busbar 5 (or 7) of direct current of the power channel is switching to by another The DC source passage of normal work occurs after dead electricity during powering, and is normally confluxed by the direct current of another normal power source passage Bar 7 (or 5) exports unidirectional current control time delay disconnection relay 2 and connects by diode 6 (or 4), makes DC uninterrupted busbar 1 Still powered by the emergent busbar 3 of direct current, now the uninterrupted electrical equipment of trouble power passage is single by DC uninterrupted busbar 1 Solely power supply;The normal busbar 5 (or 7) of direct current of pending fault power channel switchs to normally be confluxed by another normal power source channel DC After bar 7 (or 5) power supply, the uninterrupted electrical equipment of the power channel is reverted to by DC uninterrupted busbar 1 and direct current again Normal busbar 5 (or 7) is powered jointly.
The preferable enforcement of the DC uninterrupted supply line of aircraft DC power-supply system other many normal power source channel configurations Mode is similar with single, double normal power source channel configurations, it is only necessary to preferably real in single, double normal power source passage uninterrupted power supply circuit Apply and corresponding diode and the normal busbar of direct current are increased according to increased normal power source port number on the basis of mode.When On the normal busbar of arbitrary direct current after electricity, unidirectional current is exported by corresponding diode and controls time delay and disconnect relay to connect, made The emergent busbar of direct current is powered by time delay disconnection relay to DC uninterrupted busbar, DC uninterrupted busbar and upper electricity The normal busbar of each direct current afterwards is powered to uninterrupted electricity supply and use equipment jointly.The normal busbar of each direct current is by direct-current ground electricity Source power switch to by normal power source on machine (electromotor or vertoro) power during occur after dead electricity, it is impossible to by phase The diode output unidirectional current control time delay answered disconnects relay and connects, and it is disconnected based on its own time delay that now time delay disconnects relay It is opening characteristic to continue within a certain period of time to remain up, make DC uninterrupted busbar still be powered by the emergent busbar of direct current, Individually powered to uninterrupted electrical equipment from DC uninterrupted busbar during this;Treat that the normal busbar of each direct current switchs to by machine After upper normal power source is powered, disconnect relay again by diode output unidirectional current control time delay and connect, now uninterruptedly use Electric equipment is reverted to again is powered jointly by DC uninterrupted busbar and the normal busbar of each direct current.When arbitrary normal power source leads to After road failure, the mistake that the normal busbar of direct current of the power channel is powered in the DC source passage switched to by other normal works Occur in journey after dead electricity, unidirectional current control is exported by respective diode by the direct current of other normal power source passages normal busbar Time delay disconnects relay and connects, and makes DC uninterrupted busbar still be powered by the emergent busbar of direct current, now trouble power passage Uninterrupted electrical equipment individually powered by DC uninterrupted busbar;The normal busbar of pending fault power channel direct current switch to by After other normal power source passages are powered, the uninterrupted electrical equipment of the power channel is reverted to by DC uninterrupted busbar again Power jointly with the normal busbar of direct current.
The preferred embodiments of the present invention are the foregoing is only, the present invention is not limited to, for the skill of this area For art personnel, the present invention can have various modifications and variations.It is all within the spirit and principles in the present invention, made any repair Change, equivalent, improvement etc., should be included within the scope of the present invention.

Claims (10)

1. a kind of DC uninterrupted supply line, it is characterised in that include:DC uninterrupted busbar, time delay disconnect relay, Direct current is met an urgent need busbar, the normal busbar of at least one direct current, at least one diode;The normal busbar of each direct current passes through One its corresponding diode disconnects relay and is connected with the time delay, and in the time delay situation that relay is connected is disconnected Under, the time delay disconnect two contacts of relay respectively with the emergent busbar of the direct current and the DC uninterrupted busbar It is connected;Wherein, the emergent busbar of the direct current is connected with emergency power supply, the normal busbar of at least one direct current and power supply phase Even.
2. DC uninterrupted supply line according to claim 1, it is characterised in that
After electricity on the normal busbar of at least one direct current, unidirectional current control is exported by an its corresponding diode Time delay disconnects relay and connects, and the emergent busbar of the direct current disconnects relay to the DC uninterrupted busbar by time delay Power supply;
After the normal busbar dead electricity of at least one direct current, relay is disconnected by the time delay and is protected in first time period Hold connection, the emergent busbar of the direct current in the first time period by time delay disconnection relay to the direct current not Interruption busbar is powered.
3. DC uninterrupted supply line according to claim 1 and 2, it is characterised in that at least one direct current On normal busbar after electricity, the electricity of the voltage of the normal busbar of at least one direct current higher than the DC uninterrupted busbar Pressure, the normal busbar of at least one direct current and the DC uninterrupted busbar are powered to electrical equipment.
4. DC uninterrupted supply line according to claim 2, it is characterised in that at least one direct current normally converges The situation of stream bar dead electricity includes one below:
The normal busbar of one direct current is switching to dead electricity occur during the DC source passage by other normal works is powered Situation;
The normal busbar of at least one direct current switchs to by electromotor on aircraft or becomes repoussage being powered by direct-current ground power supply There is the situation of dead electricity in stream device during powering.
5. DC uninterrupted supply line according to claim 2, it is characterised in that at least one direct current normally converges In the case of stream bar dead electricity, the normal busbar of at least one direct current can not export unidirectional current control by corresponding diode The time delay disconnects relay and connects.
6. a kind of method of DC uninterrupted power supply, it is characterised in that include:
There is provided DC uninterrupted busbar, time delay disconnection relay, the emergent busbar of direct current, at least one direct current normally to conflux Bar, at least one diode;
The normal busbar of each direct current disconnects relay and is connected by an its corresponding diode and the time delay, in institute In the case of stating time delay disconnection relay connection, the time delay disconnects two contacts of relay and meets an urgent need with the direct current respectively and converges Stream bar is connected with the DC uninterrupted busbar;Wherein, the emergent busbar of the direct current is connected with emergency power supply, it is described at least The normal busbar of one direct current is connected with power supply.
7. method according to claim 6, it is characterised in that
After electricity on the normal busbar of at least one direct current, DC controlled is exported by described its corresponding diode Time delay processed disconnects relay and connects, and the emergent busbar of the direct current DC uninterrupted is confluxed by time delay disconnection relay to described Bar is powered;
After the normal busbar dead electricity of at least one direct current, relay is disconnected in first time period by the time delay Inside remain up, the emergent busbar of the direct current in the first time period by the time delay disconnect relay to it is described directly Flow uninterrupted busbar to power.
8. the method according to claim 6 or 7, it is characterised in that the electricity on the normal busbar of at least one direct current Afterwards, the voltage of the normal busbar of at least one direct current higher than the DC uninterrupted busbar voltage, described at least one The individual normal busbar of direct current and the DC uninterrupted busbar are powered to electrical equipment.
9. method according to claim 7, it is characterised in that the situation of the normal busbar dead electricity of at least one direct current Including one below:
The normal busbar of one direct current is switching to dead electricity occur during the DC source passage by other normal works is powered Situation;
The normal busbar of at least one direct current switchs to by electromotor on aircraft or becomes repoussage being powered by direct-current ground power supply There is the situation of dead electricity in stream device during powering.
10. method according to claim 7, it is characterised in that the feelings of the normal busbar dead electricity of at least one direct current Under condition, the normal busbar of at least one direct current can not export unidirectional current and control the time delay and disconnect by corresponding diode Relay is connected.
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CN113745058B (en) * 2021-10-09 2023-12-01 陕西航空电气有限责任公司 Control method of direct-current emergency bus bar contactor in aviation power distribution system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6031298A (en) * 1997-12-19 2000-02-29 International Business Machines Corporation 2N redundant power system and method using cross-coupled AC power transfer
CN204089325U (en) * 2014-08-18 2015-01-07 江西洪都航空工业集团有限责任公司 The novel power supply circuits of a kind of flight control system
CN104269842A (en) * 2014-09-09 2015-01-07 株洲变流技术国家工程研究中心有限公司 Direct-current supply device of control system
CN104600832A (en) * 2015-01-26 2015-05-06 哈尔滨飞机工业集团有限责任公司 High power load loading equipment emergency power supply control system and control method thereof

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2906787B1 (en) * 2006-10-10 2009-03-20 Airbus France Sa SYSTEM AND METHOD FOR CONTINUOUS POWER SUPPLYING AN ELECTRICAL NETWORK ON BOARD AN AIRCRAFT

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6031298A (en) * 1997-12-19 2000-02-29 International Business Machines Corporation 2N redundant power system and method using cross-coupled AC power transfer
CN204089325U (en) * 2014-08-18 2015-01-07 江西洪都航空工业集团有限责任公司 The novel power supply circuits of a kind of flight control system
CN104269842A (en) * 2014-09-09 2015-01-07 株洲变流技术国家工程研究中心有限公司 Direct-current supply device of control system
CN104600832A (en) * 2015-01-26 2015-05-06 哈尔滨飞机工业集团有限责任公司 High power load loading equipment emergency power supply control system and control method thereof

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