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JPS6111537B2 - - Google Patents
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JPS6111537B2 - - Google Patents

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Publication number
JPS6111537B2
JPS6111537B2 JP5953778A JP5953778A JPS6111537B2 JP S6111537 B2 JPS6111537 B2 JP S6111537B2 JP 5953778 A JP5953778 A JP 5953778A JP 5953778 A JP5953778 A JP 5953778A JP S6111537 B2 JPS6111537 B2 JP S6111537B2
Authority
JP
Japan
Prior art keywords
storage battery
signal
circuit
control signal
voltage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP5953778A
Other languages
Japanese (ja)
Other versions
JPS54150644A (en
Inventor
Osamu Saito
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP5953778A priority Critical patent/JPS54150644A/en
Publication of JPS54150644A publication Critical patent/JPS54150644A/en
Publication of JPS6111537B2 publication Critical patent/JPS6111537B2/ja
Granted legal-status Critical Current

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  • Control Of Electrical Variables (AREA)

Description

【発明の詳細な説明】 この説明は蓄電池の充放電制御装置に関し、特
に人工衛星に搭載した蓄電池の充放電制御方式に
関するものである。
DETAILED DESCRIPTION OF THE INVENTION This description relates to a storage battery charge/discharge control device, and particularly to a charge/discharge control method for a storage battery mounted on an artificial satellite.

第1図は人工衛星に搭載した蓄電池に対する従
来の充放電制御装置の一例を示すブロツク結線図
で、図において1は太陽電池、2は人工衛星にお
ける負荷、3はレギユレータ、4は蓄電池、5は
ラツチングリレー、R1,R2はそれぞれ抵抗、
CR1,CR2はそれぞれ逆流防止用ダイオードであ
る。また6は蓄電池4の温度およびその端子電圧
をモニタするモニタ回路、7,8はそれぞれリレ
ー駆動回路、9,10はそれぞれ単安定マルチバ
イブレータ、11は比較回路であり、比較回路1
1は基準電圧、たとえばツエナダイオードの降服
電圧と太陽電池1からCR1を介して入力される電
圧を分圧した電圧を比較し、太陽電池1の電圧が
所定値以下となるとき論理「1」の信号を出力す
る。12は波形整形回路である。また第1図中の
Aは蓄電池のフル充電、Bはトリクル充電を指令
する地上からのコマンド信号を表す。
Figure 1 is a block wiring diagram showing an example of a conventional charge/discharge control device for a storage battery mounted on a satellite. In the figure, 1 is a solar cell, 2 is a load on the satellite, 3 is a regulator, 4 is a storage battery, and 5 is a Latching relay, R 1 and R 2 are each resistance,
CR 1 and CR 2 are diodes for preventing backflow. Further, 6 is a monitor circuit that monitors the temperature of the storage battery 4 and its terminal voltage, 7 and 8 are relay drive circuits, 9 and 10 are monostable multivibrators, and 11 is a comparison circuit.
1 compares the reference voltage, for example, the breakdown voltage of a Zener diode, and the voltage obtained by dividing the voltage input from the solar cell 1 via CR 1 , and when the voltage of the solar cell 1 becomes less than a predetermined value, the logic becomes "1". Outputs the signal. 12 is a waveform shaping circuit. Further, in FIG. 1, A represents a command signal from the ground that instructs full charging of the storage battery, and B represents a command signal from the ground that instructs trickle charging.

また第2図は第1図の回路の各部の動作を示す
動作タイムチヤートであつて、第2図を参照しな
がら第1図の回路の動作を説明する。第1図にお
いて蓄電池4の温度とその端子電圧とがそれぞれ
所定レベルに対し第2図に示すとおり変化したと
すれば、モニタ回路6の出力信号101は第2図
信号101として示す波形のように変化する。信
号101は波形整形回路12を経て信号102と
なり(第1図の実施例では第2図に示すように信
号101と102とは同一波形である)単安定マ
ルチバイブレータ10に入力される。マルチバイ
ブレータ10は信号102の立上り点から所定時
間継続する信号103を出力する。第2図に信号
103の波形を示す。信号103はリレー駆動回
路を付勢しラツチングリレー5を接点R側に接続
する。この状態では太陽電池1で発生した電力は
抵抗R2を通して蓄電池4を充電し、いわゆるト
リクル充電モードとなる。すなわち蓄電池4の温
度が高いか端子電圧が高い時はトリクル充電を行
なう。一方、蓄電池4の温度および端子電圧が所
定のレベルを下まわつた場合はモニタ回路6の出
力信号101の立下り点を波形整形回路12で第
2図信号104として示すように検出し、この信
号を単安定マルチバイブレータ9に入力して信号
104を起点とし所定時間継続する信号105を
出力し、リレー駆動回路7を付勢しラツチングリ
レー5を接点S側に接続し抵抗R2を短絡する。
この状態では太陽電池1で発生した電力はラツチ
ングリレー5の接点Sを通じて蓄電池4を充電
し、いわゆるフル充電モードとなる。
FIG. 2 is an operation time chart showing the operation of each part of the circuit of FIG. 1, and the operation of the circuit of FIG. 1 will be explained with reference to FIG. In FIG. 1, if the temperature of the storage battery 4 and the terminal voltage thereof change from respective predetermined levels as shown in FIG. Change. The signal 101 passes through the waveform shaping circuit 12 and becomes the signal 102 (in the embodiment shown in FIG. 1, the signals 101 and 102 have the same waveform as shown in FIG. 2), which is input to the monostable multivibrator 10. The multivibrator 10 outputs a signal 103 that continues for a predetermined time from the rising point of the signal 102. FIG. 2 shows the waveform of signal 103. The signal 103 energizes the relay drive circuit and connects the latching relay 5 to the contact R side. In this state, the power generated by the solar cell 1 charges the storage battery 4 through the resistor R2 , resulting in a so-called trickle charge mode. That is, when the temperature of the storage battery 4 is high or the terminal voltage is high, trickle charging is performed. On the other hand, when the temperature and terminal voltage of the storage battery 4 fall below a predetermined level, the falling point of the output signal 101 of the monitor circuit 6 is detected by the waveform shaping circuit 12 as shown as a signal 104 in FIG. is input to the monostable multivibrator 9, which outputs a signal 105 that starts from the signal 104 and continues for a predetermined time, energizes the relay drive circuit 7, connects the latching relay 5 to the contact S side, and shorts the resistor R2 . .
In this state, the power generated by the solar cell 1 charges the storage battery 4 through the contact S of the latching relay 5, resulting in a so-called full charging mode.

又、上述の充電モードの制御とは独立に、太陽
電池1の電圧が所定の下限レベル以下に低下した
場合、比較回路11は第2図信号106で示すよ
うな波形の信号を出力し波形整形回路12に入力
して第2図に信号107として示すような波形の
信号を形成し、その立上り点で単安定マルチバイ
ブレータ9をトリガしてその時点から所定時間継
続する信号105を出力し、リレー駆動回路7を
付勢しラツチングリレー5を接点S側に接続し抵
抗R2を短絡する。この状態では蓄電池4からラ
ツチングリレー5の接点Sを通じ負荷2に電流を
流し太陽電池1による電力の不足分が蓄電池4か
ら供給される。すなわち蓄電池4はフル放電モー
ドとなる。このように従来の装置では蓄電池温度
及び蓄電池端子電圧が所定の下限レベル以下に低
下した場合の蓄電池4のフル充電制御と、太陽電
池1の電圧が所定の下限レベル以下に低下した場
合の蓄電池4のフル放電制御が互に無関係に行わ
れているため、蓄電池温度又はその端子電圧が所
定レベルを上まわりトリクル充電モードが必要と
なりラツチングリレー5の接点をR側に接続すべ
き制御と、太陽電池1の電圧が所定の下限レベル
以下に低下した場合にフル放電モードが必要とな
りラツチングリレー5の接点をS側に接続すべき
制御とが競合する場合がある。
In addition, independently of the control of the charging mode described above, when the voltage of the solar cell 1 drops below a predetermined lower limit level, the comparator circuit 11 outputs a signal with a waveform as shown in the signal 106 in FIG. 2, and performs waveform shaping. A signal having a waveform shown as signal 107 in FIG. 2 is input to the circuit 12, and at its rising point, the monostable multivibrator 9 is triggered, and from that point on, a signal 105 that continues for a predetermined time is output, and the relay is activated. The drive circuit 7 is energized, the latching relay 5 is connected to the contact S side, and the resistor R 2 is short-circuited. In this state, current is passed from the storage battery 4 to the load 2 through the contact S of the latching relay 5, and the shortage of power generated by the solar cell 1 is supplied from the storage battery 4. That is, the storage battery 4 is in full discharge mode. In this way, the conventional device performs full charge control of the storage battery 4 when the storage battery temperature and storage battery terminal voltage drop below a predetermined lower limit level, and controls the full charge of the storage battery 4 when the voltage of the solar cell 1 drops below a predetermined lower limit level. Full discharge control is performed independently of each other, so when the temperature of the storage battery or its terminal voltage exceeds a predetermined level, trickle charge mode is required, and control to connect the contact of latching relay 5 to the R side and solar When the voltage of the battery 1 drops below a predetermined lower limit level, a full discharge mode is required, which may conflict with the control to connect the contact of the latching relay 5 to the S side.

この競合の一例を第2図について説明する。第
2図の横軸に示す時刻t0点では蓄電池温度が所定
レベル以上に上りフル充電からトリクル充電に切
換えられ、時刻t1点ではトルク充電中であるが、
時刻t2点で太陽電池1の電圧が所定下限レベル以
下に低下し少時の遅延時間の後時刻t3で信号10
5が出力しラツチングリレー5によつて抵抗R2
が短絡されてフル放電モードとなる。この状態で
太陽電池1の電圧が回復した場合負荷2への電力
は太陽電池から供給されしたがつて蓄電池4はラ
ツチングリレー5の接点Sを経てフル充電され蓄
電池3の温度は上昇を続けるが、信号101は変
化しないのでリレー駆動回路8が付勢されること
なく、蓄電池4に重大な障害を与えることとな
る。
An example of this conflict will be explained with reference to FIG. At time t0 , shown on the horizontal axis in Figure 2, the storage battery temperature rises above a predetermined level and the switch is made from full charging to trickle charging, and at time t1 , torque charging is in progress.
At time t 2 , the voltage of solar cell 1 drops below the predetermined lower limit level, and after a short delay time, signal 10 is generated at time t 3 .
5 outputs resistance R 2 by latching relay 5.
is shorted and enters full discharge mode. When the voltage of the solar cell 1 is restored in this state, power to the load 2 is supplied from the solar cell, and the storage battery 4 is fully charged via the contact S of the latching relay 5, and the temperature of the storage battery 3 continues to rise. , the signal 101 does not change, so the relay drive circuit 8 is not energized, causing serious damage to the storage battery 4.

この発明は従来の装置における上述の欠点を除
去することを目的とし、この目的のためこの発明
では太陽電池の電圧が所定の下限レベルを下まわ
つた場合の蓄電池のフル放電モードの制御と、モ
ニタ回路の出力信号に対応しての蓄電池の充電モ
ードの制御とを競合させることなく、モニタ回路
の出力信号に対応して充電モードの制御を蓄電池
の放電モードの制御に対して優先させ、蓄電池の
フル充電は蓄電池の温度および端子電圧がそれぞ
れ所定レベル内にある場合に限り実行されるよう
にしたもので、以下この発明の一実施例について
説明する。
The present invention aims to eliminate the above-mentioned drawbacks in conventional devices, and for this purpose, the present invention provides control and monitoring of the full discharge mode of the storage battery when the voltage of the solar cell falls below a predetermined lower limit level. The control of the storage battery is controlled by giving priority to the control of the charging mode in response to the output signal of the monitor circuit over the control of the discharge mode of the storage battery, without conflicting with the control of the charging mode of the storage battery in response to the output signal of the circuit. Full charging is performed only when the temperature of the storage battery and the terminal voltage are within predetermined levels, and one embodiment of the present invention will be described below.

第3図はこの発明の一実施例を示すブロツク結
線図で、図において第1図と同一符号は同一又は
相当部分を示し、その動作も同一であるので重複
した説明は省略する。第3図において13は第1
図の波形整形回路12に相当し、ただインバータ
14とアンドゲート15とによつて信号101が
存在しない時にだけ信号106をアンドゲート1
5を通過させ信号108として単安定マルチバイ
ブレータ9を制御する。第4図は第3図の回路の
各部の動作を示す動作タイムチヤートであつて、
第4図を参照しながら第3図の回路の動作の第1
図の回路の動作と異る点を説明する。但し第4図
において第2図と同一符号は同一又は相当波形或
は相当動作を示すものである。またこの発明の説
明上比較回路11の出力である信号106を仮に
第1の制御信号と称し、モニタ回路6の出力であ
る信号101を仮に第2の制御信号と称すること
にする。第2の制御信号に応じて信号102又は
信号104を発生し、信号102を信号103と
してリレー駆動回路8によりラツチングリレー5
を接点R側に接続し、信号104から信号105
を発生しリレー駆動回路7によりラツチングリレ
ー5を接点S側に接続しフル充電とトリクル充電
との切換を行なうことは第1図の場合と同様であ
る。
FIG. 3 is a block diagram showing an embodiment of the present invention. In the figure, the same reference numerals as in FIG. 1 indicate the same or corresponding parts, and since the operations thereof are also the same, redundant explanation will be omitted. In Figure 3, 13 is the first
Corresponds to the waveform shaping circuit 12 shown in the figure, and only when the signal 101 is not present, the signal 106 is transferred to the AND gate 1 by the inverter 14 and the AND gate 15.
5 and controls the monostable multivibrator 9 as a signal 108. FIG. 4 is an operation time chart showing the operation of each part of the circuit in FIG.
Referring to FIG. 4, the first explanation of the operation of the circuit in FIG.
Points that differ from the operation of the circuit shown in the figure will be explained. However, in FIG. 4, the same symbols as in FIG. 2 indicate the same or equivalent waveforms or equivalent operations. Furthermore, for the purpose of explaining the present invention, the signal 106 that is the output of the comparison circuit 11 will be temporarily referred to as a first control signal, and the signal 101 that is the output of the monitor circuit 6 will be temporarily referred to as a second control signal. A signal 102 or a signal 104 is generated in accordance with the second control signal, and the relay drive circuit 8 uses the signal 102 as a signal 103 to latching the latching relay 5.
is connected to the contact R side, and the signal 104 to signal 105 is
This is the same as in the case of FIG. 1, in which the latching relay 5 is connected to the contact S side by the relay drive circuit 7 and switching between full charging and trickle charging is performed.

第1の制御信号すなわち信号106は第2の制
御信号の存在しないときだけゲート15を通過し
て信号108となり単安定マルチバイブレータ9
により信号105を発生しリレー駆動回路7によ
つてラツチングリレー5を接点S側に接続する。
したがつて第2の制御信号すなわち信号101が
論理「0」にあつてラツチングリレー5が接点S
側にありフル充電が行われているとき、第4図の
時刻t0に至り信号101が論理「1」となると信
号103を発生しラツチングリレー5を接点R側
に接続しトリクル充電を行うが、この状態のとき
時刻t2に至り太陽電池の電圧が所定下限レベル以
下となり第4図に示すように信号106が論理
「1」となつてもこの信号はゲート15で阻止さ
れるので信号108は論理「0」のままに保たれ
ラツチングリレー5を接点S側に接続することは
ないので、第1図の回路について前節で説明した
ような蓄電池4の事故を発生することはない。
The first control signal, the signal 106, passes through the gate 15 and becomes the signal 108 only in the absence of the second control signal to the monostable multivibrator 9.
A signal 105 is generated, and the relay drive circuit 7 connects the latching relay 5 to the contact S side.
Therefore, when the second control signal, that is, the signal 101 is at logic "0", the latching relay 5 closes the contact S.
When the battery is fully charged and the signal 101 becomes logic "1" at time t0 in Figure 4, the signal 103 is generated and the latching relay 5 is connected to the contact R side to perform trickle charging. However, in this state, at time t2 , the voltage of the solar cell falls below the predetermined lower limit level, and even if the signal 106 becomes logic "1" as shown in FIG. 4, this signal is blocked by the gate 15, so the signal 108 is kept at logic ``0'' and the latching relay 5 is not connected to the contact S side, so that a failure of the storage battery 4 as explained in the previous section with respect to the circuit of FIG. 1 will not occur.

以上の説明はこの発明を人工衛星に搭載する蓄
電池の充放電制御に応用する場合の例について説
明したが、この発明は人工衛星搭載の蓄電池ばか
りでなく、発生電圧に変化が生ずることのある直
流電源装置によつて充電されこの直流電源装置の
電圧が低下したときこの直流電源装置と並列に負
荷に対し電流を供給する蓄電池の充放電制御装置
に利用できることは申すまでもない。また第3図
の実施例では第1の信号106と第2の信号10
1とからリレー駆動回路7,8を付勢する信号を
発生するまでの信号処理回路に特定の回路を用い
たが、この実施例に示される特定の回路に限定さ
れることなく公知のどのような信号処理回路を用
いてもよいことは明らかであり、また第3図に示
す実施例では第2の信号101として蓄電池4の
温度と端子電圧をモニタし第4図に示すようにそ
の論理和を信号101としたが、第2の信号の作
成方法はこの実施例に限定されることなく蓄電池
4の状態を表す各種の測定値を出力しこれら測定
値から適宜なデータ処理を行つて単一の又は複数
の第2の信号を形成してもよい。たとえば第3図
のインバータ14に入力する信号は第2の信号1
01のうち蓄電池4の温度が所定レベル以上であ
るか所定レベル以下であるかを示す信号だけにす
ることもできる。
The above explanation has been about an example in which the present invention is applied to charge/discharge control of a storage battery mounted on an artificial satellite. However, this invention is applicable not only to storage batteries mounted on an artificial satellite, but also to DC Needless to say, the present invention can be used as a charge/discharge control device for a storage battery that supplies current to a load in parallel with the DC power supply when the voltage of the DC power supply drops after being charged by the power supply. Further, in the embodiment of FIG. 3, the first signal 106 and the second signal 10
Although a specific circuit is used for the signal processing circuit from 1 to 1 to generate the signal to energize the relay drive circuits 7 and 8, the circuit is not limited to the specific circuit shown in this embodiment, and any known circuit may be used. It is obvious that a similar signal processing circuit may be used, and in the embodiment shown in FIG. 3, the temperature and terminal voltage of the storage battery 4 are monitored as the second signal 101, and the logical sum of However, the method of creating the second signal is not limited to this embodiment, but it outputs various measured values representing the state of the storage battery 4, performs appropriate data processing from these measured values, and generates a single signal. or a plurality of second signals may be formed. For example, the signal input to the inverter 14 in FIG.
Of 01, only a signal indicating whether the temperature of the storage battery 4 is above a predetermined level or below a predetermined level may be used.

以上のようにこの発明によれば蓄電池の異常温
度上昇を防止する充放電制御を行うことができ
る。
As described above, according to the present invention, charging and discharging control can be performed to prevent abnormal temperature rise of the storage battery.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は人工衛星に搭載した蓄電池に対する従
来の充放電制御装置の一例を示すブロツク結線
図、第2図は第1図の回路の各部の動作を示す動
作タイムチヤート、第3図はこの発明の一実施例
を示すブロツク結線図、第4図は第3図の回路の
各部の動作を示す動作タイムチヤートである。 図において1は太陽電池、2は負荷、3はレギ
ユレータ、4は蓄電池、5はラツチングリレー、
6はモニタ回路、7,8はそれぞれリレー駆動回
路、9,10はそれぞれ単安定マルチバイブレー
タ、11は比較回路、13は波形整形回路、14
はインバータ、15はアンドゲートである。なお
各図中同一符号は同一又は相当部分を示すものと
する。
Fig. 1 is a block wiring diagram showing an example of a conventional charge/discharge control device for a storage battery mounted on an artificial satellite, Fig. 2 is an operation time chart showing the operation of each part of the circuit in Fig. 1, and Fig. 3 is an invention according to the present invention. FIG. 4 is a block diagram showing one embodiment of the present invention, and FIG. 4 is an operation time chart showing the operation of each part of the circuit of FIG. In the figure, 1 is a solar cell, 2 is a load, 3 is a regulator, 4 is a storage battery, 5 is a latching relay,
6 is a monitor circuit, 7 and 8 are each a relay drive circuit, 9 and 10 are each a monostable multivibrator, 11 is a comparison circuit, 13 is a waveform shaping circuit, and 14
is an inverter, and 15 is an AND gate. Note that the same reference numerals in each figure indicate the same or corresponding parts.

Claims (1)

【特許請求の範囲】[Claims] 1 電圧に変化が生ずる直流電源装置と逆流防止
用ダイオードの直列接続回路、この直列接続回路
に並列に接続される負荷、蓄電池とこの蓄電池に
直列に蓄電池の放電方向の極性で接続されるダイ
オードとの直列回路を上記負荷と並列に接続した
蓄電池放電回路、上記ダイオードに対し並列に接
続され蓄電池充電電流を制限する電流制限抵抗、
上記直流電源装置の出力電圧をあらかじめ定める
基準電圧と比較し上記出力電圧が所定値以下とな
るとき第1の制御信号を出力する比較回路、上記
蓄電池の状態をモニタし少くとも上記蓄電池の温
度があらかじめ定めた温度を超過した場合には第
2の制御信号を出力するモニタ回路、上記第2の
制御信号が存在しないときに上記第1の制御信号
の発生によつて上記電流制限抵抗を短絡する第1
の制御回路、上記第2の制御信号に応じて上記電
流制限抵抗の短絡を開放し又は短絡する第2の制
御回路を備えたことを特徴とする蓄電池の充放電
制御装置。
1. A series connection circuit of a DC power supply device and a reverse current prevention diode in which voltage changes occur, a load connected in parallel to this series connection circuit, a storage battery and a diode connected in series to this storage battery with the polarity in the discharge direction of the storage battery. a storage battery discharging circuit in which a series circuit of is connected in parallel with the load; a current limiting resistor connected in parallel with the diode to limit the storage battery charging current;
a comparison circuit that compares the output voltage of the DC power supply with a predetermined reference voltage and outputs a first control signal when the output voltage is below a predetermined value; A monitor circuit that outputs a second control signal when a predetermined temperature is exceeded, and short-circuits the current limiting resistor by generating the first control signal when the second control signal is not present. 1st
A charge/discharge control device for a storage battery, comprising a second control circuit that opens or shorts the current limiting resistor in response to the second control signal.
JP5953778A 1978-05-19 1978-05-19 Charge/discharge controller for storage battery Granted JPS54150644A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5953778A JPS54150644A (en) 1978-05-19 1978-05-19 Charge/discharge controller for storage battery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5953778A JPS54150644A (en) 1978-05-19 1978-05-19 Charge/discharge controller for storage battery

Publications (2)

Publication Number Publication Date
JPS54150644A JPS54150644A (en) 1979-11-27
JPS6111537B2 true JPS6111537B2 (en) 1986-04-03

Family

ID=13116105

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5953778A Granted JPS54150644A (en) 1978-05-19 1978-05-19 Charge/discharge controller for storage battery

Country Status (1)

Country Link
JP (1) JPS54150644A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5785840U (en) * 1980-11-13 1982-05-27
JPS63213431A (en) * 1987-03-02 1988-09-06 宇宙開発事業団 Electric source of satellite

Also Published As

Publication number Publication date
JPS54150644A (en) 1979-11-27

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