Insulating container for battery, battery control device, and battery-failure detection method
10147976 ยท 2018-12-04
Assignee
Inventors
Cpc classification
H01M50/24
ELECTRICITY
H01M10/4257
ELECTRICITY
H01M2010/4271
ELECTRICITY
Y02E60/10
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
H01M50/204
ELECTRICITY
H01M10/482
ELECTRICITY
H01M50/284
ELECTRICITY
International classification
H01M10/42
ELECTRICITY
G01M3/18
PHYSICS
H01M10/48
ELECTRICITY
Abstract
A battery assembly heat insulating container includes a box body and a lid body. The box body has an opening on its upper surface, and contains a battery module formed by connecting a plurality of battery cells in series or in parallel. The lid body is placed on the upper surface of the box body. The battery assembly heat insulating container is adapted to provide heat insulation between an external space and an internal space formed by the box body and the lid body and configured to contain the battery module. A circuit member configured to detect leakage of active material from the battery module is provided at the bottom of the box body.
Claims
1. A battery assembly heat insulating container, comprising: a battery assembly formed by connecting a plurality of battery cells in series or in parallel; a box body containing the battery assembly formed by connecting a plurality of battery cells in series or in parallel, an opening being formed on an upper surface of the box body; and a lid body placed on the upper surface of the box body, the battery assembly heat insulating container being adapted to provide heat insulation between an external space and an internal space being formed by the box body and the lid body and containing the battery assembly, wherein the battery assembly heat insulating container further comprises a circuit member configured to detect leakage of a liquid active material from the battery assembly, the circuit member being provided at a bottom of the box body, wherein the circuit member includes a first lead wire provided proximate a bottom surface of the box body stacked on a first insulating layer, a second lead wire stacked on a second insulating layer, a third insulating layer, an internal space containing the battery assembly provided above the third insulating layer, and holes defined in the third and second insulating layers respectively, configured to pass the liquid active material leaked from the battery assembly therethrough to reach the second lead wire and the first lead wire, the leaked active liquid material thereby being detected.
2. The battery assembly heat insulating container according to claim 1, wherein the first lead wire and the second lead wire each include comb teeth spread in a comb teeth pattern.
3. The battery assembly heat insulating container according to claim 2, wherein the comb teeth of the second lead wire are positioned between the comb teeth of the first lead wire.
4. The battery assembly heat insulating container according to claim 2, wherein an orientation of the comb teeth of the first lead wire is different from an orientation of the comb teeth of the second lead wire.
5. The battery assembly heat insulating container according to claim 1, wherein the first and second lead wires are wired separately from a heater wire provided on the bottom surface of the box body.
6. The battery assembly heat insulating container according to claim 1, wherein a resistance of at least one of the first and second lead wires is adapted to change upon contact with the liquid active material.
Description
BRIEF DESCRIPTION OF DRAWINGS
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(2)
(3)
(4)
(5)
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(8)
(9)
DESCRIPTION OF EMBODIMENTS
(10) Hereinafter, a heat insulating container for a battery assembly (referred to as the battery assembly heat insulating container), a control device for the battery assembly (referred to as the battery assembly control device), and a failure detection method for the battery assembly (referred to as the battery assembly failure detection method) according to the present invention, e.g., applied to a NaS battery will be described with reference to
(11) Firstly, as shown in
(12) The box body 12 is formed of a plate member of, e.g., stainless steel, and formed in a box shape having a hollow area. The hollow area is a space sealed in an air-tight manner. The hollow area is configured to be connectable to an external space through a vacuum valve (not shown). A porous vacuum heat insulating board 16 formed by solidifying glass fiber in a plate shape using adhesive fills the hollow area to provide vacuum heat insulating structure for the box body 12.
(13) In the same manner as in the case of the box body 12, the lid body 14 is formed of a plate member of, e.g., stainless steel. A heat insulating material layer for achieving the required minimum heat insulating property is placed on an inner surface (lower surface) of the lid body 14, and at least two stacked detachable heat insulating plates 22 are filled in a hollow area 20 to provide air heat insulating structure only in the lid body 14 (upper surface). In the structure, the amount of heat radiation from the upper surface of the heat insulating container 10 can be controlled.
(14) A battery module 28 (battery assembly) formed by connecting a plurality of battery cells 26 in series and/or in parallel upright is placed in an internal space 24 of the heat insulating container 10 formed by the box body 12 and the lid body 14. In order to suppress damages and abnormal heating of the battery cells 26 or leakage of active material, etc., though not shown, as fire extinction sand, silica sand fills a gap between the box body 12 and the battery module 28.
(15) As shown in
(16) Further, at the bottom of the box body 12 of the heat insulating container 10, a heater member 34 for heating the battery module 28 at high temperature and a circuit member 36 stacked on the heater member 34, for detecting leakage of active material from the battery module 28, are provided.
(17) As also shown in
(18) The circuit member 36 includes a first insulating layer 50a stacked on the upper soaking plate 48 of the heater member 34, a first lead wire 52A stacked on the first insulating layer 50a, a second insulating layer 50b stacked on the first lead wire 52A, a second lead wire 52B stacked on the second insulating layer 50b, and a third insulating layer 50c stacked on the second lead wire 52B. The battery module 28 is fixedly placed on the third insulating layer 50c. As in the case of the heater member 34, for example, mica sheets may be used for the first insulating layer 50a, the second insulating layer 50b, and the third insulating layer 50c. For example, nickel wires, etc, may be used for the first lead wire 52A and the second lead wire 52B.
(19) The first lead wire 52A and the second lead wire 52B are spread over an entire graphic pattern 54 (see
(20) Further, as shown in
(21) Therefore, in the battery module 28, if leakage of active material occurs in one or more battery cells 26, the leaked active material passes through the holes 58a of the third insulating layer 50c to reach the second lead wire 52B, or the leaked active material passes through the holes 58a of the third insulating layer 50c and the holes 58b of the second insulating layer 50b to reach the first lead wire 52A, or the leaked active material passes through the holes 58a of the third insulating layer 50c to reach the second lead wire 52B, and thereafter, passes through the holes 58b of the second insulating layer 50b to reach the first lead wire 52A.
(22) If the active material contacts the first lead wire 52A, for example short circuiting between adjacent comb teeth 56a may occur, and erosion (corrosion) or disconnection of the first lead wire 52A may occur in its portion which contacts the active material. If short circuiting occurs between the comb teeth 56a, the resistance value of the first lead wire 52A is decreased as a whole. Further, if a portion of the first lead wire 52A is eroded or disconnected, the resistance value of the first lead wire 52A becomes large as a whole. This phenomenon may occur also in the second lead wire 52B.
(23) In this regard, in the case where resistance values of the first lead wire 52A and the second lead wire 52B are measured, and if there is a change in any one or more of the resistance value R1 of the first lead wire 52A, the resistance value R2 of the second lead wire 52B, and the difference R between the resistance value R1 of the first lead wire 52A and the resistance value R2 of the second lead wire 52B, it is proven that a failure has occurred in one or more battery cells 26 of the battery module 28 due to leakage of active material. The resistance values R1 and R2 of the first lead wire 52A and the second lead wire 52B vary depending on changes in the temperature of the internal space 24 in accordance with temperature characteristics of the constituent material. Therefore, the expected change widths (r1 and r2) in the resistance values R1 and R2 of the first lead wire 52A and the second lead wire 52B due to expected changes in the temperature are determined beforehand, e.g., empirically. In the case where the resistance value R1 of the first lead wire 52A changes (becomes high or low) in excess of the predetermined change width r1, or in the case where the resistance value R2 of the second lead wire 52B changes (becomes high or low) in excess of the predetermined change width r2, it is determined that a failure has occurred in one or more battery cells 26 due to leakage of active material. In the case where the difference R between the resistance value R1 of the first lead wire 52A and the resistance value R2 of the second lead wire 52B is considered, since the above described change widths can be absorbed or canceled out, it may be determined that a failure has occurred due to leakage of active material upon detection of the change in the difference R. It is a matter of course that a predetermined threshold value r.sub.th (which may be smaller than the change widths r1 and r2) may be used to determine that a failure has occurred due to leakage of active material upon detection of a change in the difference R equal to or more than the threshold value r.sub.th. In this regard, if disconnection or short circuiting occurs at the same time in both of the first lead wire 52A and the second lead wire 52B, there is a concern that no significant change in the difference R between the resistance value R1 and the resistance value R2 can be confirmed. However, since the first lead wire 52A is placed below the second lead wire 52B, in the structure, it is very unlikely that disconnection or short circuiting occurs at the same time in both of the first lead wire 52A and the second lead wire 52B. However, in order to avoid the risk of the delay in the initial response to the occurrence of a failure, in addition to monitoring of difference R between the resistance value R1 and the resistance value R2, it is preferable to monitor the change in the resistance value R1 of the first lead wire 52A and the change in resistance value R2 of the second lead wire 52B concurrently.
(24) The resistance value R1 of the first lead wire 52A can be determined by supplying minute sensing current I1 to the first lead wire 52A to detect the voltage V1 applied between both terminals of the first lead wire 52A, and computing the equation R1=V1/I1. Likewise, the resistance value R2 of the second lead wire 52B can be determined by supplying minute sensing current I2 to the second lead wire 52B to detect the voltage V2 applied between both terminals of the second lead wire 52B, and computing the equation R2=V2/I2.
(25) As described above, in the battery assembly heat insulating container 10 according to the present embodiment, the circuit member 36 for detecting leakage of active material from the battery module 28 is provided at the bottom of the box body 12. In the structure, it is possible to easily detect the presence of battery cells 26 having leakage of active material, and it is possible to realize a failure detection scheme which is different from the scheme of detecting changes in the depth of discharge in each block 30. Consequently, it is possible to detect the presence of battery cells 26 having leakage of active material in real time, and avoid the risk of the delay in the initial response to the occurrence of a failure.
(26) In particular, the first lead wire 52A and the second lead wire 52B are spread over the entire graphic pattern 54 formed by projecting at least the battery module 28 on the bottom of the box body 12. Therefore, it becomes possible to detect that a failure has occurred in one or more battery cells 26 due to leakage of active material reliably, and in real time. In the present embodiment, both of the first lead wire 52A and the second lead wire 52B are spread in a comb teeth pattern, and in particular, the comb teeth 56b of the second lead wire 52B are positioned between the adjacent comb teeth 56a of the first lead wire 52A. Therefore, for example, by determining the pitches of the comb teeth 56a of the first lead wire 52A and the comb teeth 56b of the second lead wire 52B to be equal to or less than twice the arrangement pitch of the battery cells 26, the interval between the comb teeth 56a of the first lead wire 52A and the comb teeth 56b of the second lead wire 52B that are adjacent to one another in a plan view becomes equal to or less than the arrangement pitch of the battery cells 26. In the structure, even if a failure occurred in only one battery cell 26 due to leakage of active material, it becomes possible to detect the battery cell 26 having the failure reliably, and in real time. It is a matter of course that the same advantages can be obtained by adopting an arrangement where the orientation of the comb teeth 56a of the first lead wire 52A is different from the orientation of the comb teeth 56b of the second lead wire 52B as shown in
(27) In the above described example, the two lead wires (first lead wire 52A and second lead wire 52B) are used. Alternatively, only one lead wire (first lead wire 52A or second lead wire 52B) may be used, or three or more lead wires may be used.
(28) Next, the battery assembly control device according to the present embodiment (hereinafter referred to as the control device 100) will be described with reference to
(29) As shown in
(30) The temperature measurement unit 108 measures the operating temperature T of each of the battery modules 28 based on detection values sent through the temperature measurement lines 124 from temperature sensors (not shown) provided for the battery modules 28, respectively. For example, the temperature sensors use thermocouples, or utilize changes in the electric resistance due to the temperature.
(31) Preferably, the voltage measurement unit 110 can measure the voltage for each of the blocks 30 in the battery module 28. This is aimed to perform measurement accurately, and to reliably prevent excessive electric charging and excessive electric discharging.
(32) An example of circuit structure corresponding to one battery module 28 will be explained as circuit structure of the voltage measurement unit 110. As shown in
(33) For example, in the case of sending voltage values of the first block 30A to the fourth block 30D to the computation unit 118 by turns, firstly, the relay 130 is turned on, and then, both of the first switch circuit SW1 and the second switch circuit SW2 are turned on. This switch timing is transmitted to the computation unit 118, and a signal indicating the positive sign bit is transmitted from the computation unit 118 to the differential A/D converter 134 through the photo-coupler 138. When the first switch circuit SW1 and the second switch circuit SW2 are turned on, the voltage applied between both terminals of the first block 30A is supplied to the differential A/D converter 134 through the rectifier 132, and directly converted into a digital signal. The digital signal is transmitted to the computation unit 118 through the photo-coupler array 136.
(34) Thereafter, while maintaining the ON state of the second switch circuit SW2, the first switch circuit SW1 is turned off, and the third switch circuit SW3 is turned on. This switch timing is transmitted to the computation unit 118. This time, a signal indicating the negative sign bit is transmitted from the computation unit 118 to the differential A/D converter 134 through the photo-coupler 138. Since the second switch circuit SW2 and the third switch circuit SW3 are turned on, this time, the voltage applied between both terminals of the second block 30B is supplied to the differential A/D converter 134 through the rectifier 132, and converted into a digital signal. Then, the sign is inverted (converted into a positive voltage value), and the resulting signal is transmitted to the computation unit 118 through the photo-coupler array 136. Then, in the same manner, the voltage applied between both terminals of the third block 30C, and the voltage applied between both terminals of the fourth block 30D are converted into digital signals, respectively, and the digital signals are transmitted to the computation unit 118.
(35) For the brevity of explanation, the circuit structure shown in
(36) The computation unit 118 determines the discharge cut off voltage and the charge cut off voltage for each of the four battery modules 28 by turns.
(37) Specifically, at the time of electric discharging, based on the operating temperature T measured by the temperature measurement unit 108 and the electric discharging current I.sub.d measured by the electric current measurement unit 116, the internal resistance R of the battery module 28, the temperature coefficient K.sub.t (subject to change depending on the operating temperature T), the computation unit 118 calculates the discharge cut off voltage V.sub.L using the following equation (1) for comparison with the operating voltage V measured by the voltage measurement unit 110.
V.sub.L=V.sub.onI.sub.dRK.sub.t(1)
(38) where V.sub.o denotes open circuit voltage of the battery cell 26 immediately before shortage of sodium occurs at the cathode (V.sub.o is approximately 1.82 V), and n denotes the number of battery cells 26 included in the block 30.
(39) Then, after the following relational inequality (2) satisfied, it is determined that electric discharging has been completed (end of electric discharging), and a signal for finishing electric discharging of the battery cells 26 is generated, and outputted.
V.sub.L>V(2)
(40) Further, at the time of electric charging, based on the charging current I.sub.c measured by the electric current measurement unit 116 and the internal resistance R of the battery module 28, charge cut off voltage V.sub.H is determined from the following computation equation (3) for comparison with the operating voltage V measured by the voltage measurement unit 110.
V.sub.H==(V.sub.I+)nI.sub.cR(3)
(41) where V.sub.I denotes open circuit voltage of the battery cell 26 at the end of electric charging (V.sub.I is approximately 2.075 V), n denotes the number of the battery cells 26 included in the block 30, and a denotes polarization resistance produced at the end of electric charging ( is approximately 0.05 to 0.15 V). That is, the cut off voltage V.sub.H is calculated considering the polarization resistance based on the theoretical open circuit voltage at the end of electric charging as the NaS battery.
(42) Then, after the following relational inequality (4) is satisfied, it is determined that electric charging has been completed (end of electric charging), and a signal for finishing electric charging of the battery cells 26 is generated, and outputted.
V.sub.H<V(4)
(43) Determination to prohibit or stop electric charging or electric discharging is made based on the measurement values of the measured temperature, voltage, and electric current to operate the NaS battery further reliably.
(44) Also in the temperature measurement unit 108 as described above, it is preferable to connect the differential A/D converter 134, the photo-coupler array 136, etc. as in the case of the voltage measurement unit 110.
(45) In the measurement control unit 104, measurement values (data) of the temperature, voltage, and electric current measured by the temperature measurement unit 108, the voltage measurement unit 110, and the electric current measurement unit 116 are supplied to the computation unit 118, and sent to, e.g., a remote monitoring device through the interface 122 and the external cable (including the network).
(46) As shown in
(47) The heater drive unit 106 implements ON/OFF control of the heaters 142 by supplying heater power or stopping supply of heater power to the heaters 142 through the heater power supply lines 144, in accordance with a heater control signal (e.g., contact signal) outputted from the measurement control unit 104 in accordance with a predetermined time schedule. In this example, the heater 142 is made up of the bottom surface heater wire 44 (5.6 kW) described above and an unillustrated side surface heater wire (1.8 kW), both of which can be controlled independently, and provided for each of the battery modules 28.
(48) Each of the bottom surface heaters and each of the side surface heaters repeat cycles including an ON period and an OFF period having the same length with a phase shift cycle. By this heater control, the operating temperature of the NaS battery is kept within a desired temperature range, and consumed electrical energy is substantially balanced between two lines of the three-phase three-wire system alternating current power supply.
(49) Preferably, the active material leakage detection unit 120 can detect leakage of active material for each of the battery modules 28 based on at least one of the resistance value R1 of the first lead wire 52A, the resistance value R2 of the second lead wire 52B, and the difference R between the resistance value R1 and the resistance value R2. This is aimed to avoid the risk of the delay in the initial response to the occurrence of a failure.
(50) As an example of circuit structure corresponding to one battery module 28 will be explained as circuit structure of the active material leakage detection unit 120. As shown in
(51) The resistance measurement unit 146 includes a sensing current supply circuit 150 for supplying minute sensing current I1 to the first lead wire 52A and minute sensing current I2 to the second lead wire 523, a second voltage measurement unit 152 for measuring the voltage V1 applied between both terminals of the first lead wire 52A and the voltage V2 applied between both terminals of the second lead wire 52B, and a resistance computation unit 154 for calculating the resistance value R1 of the first lead wire 52A and the resistance value R2 of the second lead wire 52B based on the voltage values V1 and V2 from the second voltage measurement units 152 and the sensing current values I1 and I2. It should be noted that the other terminals of the first lead wire 52A and the second lead wire 52B are connected to the ground GND, and have the ground potential.
(52) For example, as shown in
(53) For example, in the case of sending the voltage values of the first lead wire 52A and the second lead wire 52B to the resistance computation unit 154 by turns, firstly, the second relays 158 are turned on, and subsequently, the sixth switch circuit SW6 is turned on. By turning on the sixth switch circuit SW6, the voltage V1 applied between both of the terminals of the first lead wire 52A (the other terminal of the first lead wire 52A has the ground potential) is supplied to the second differential A/D converter 162 through the second rectifier 160, and converted into a digital signal. The digital signal is sent to the resistance computation unit 154 through the second digital signal photo-coupler array 164.
(54) Thereafter, the sixth switch circuit SW6 is turned off, and the seventh switch circuit SW7 is turned on. This time, the voltage V2 applied between both terminals of the second lead wire 52B (the other terminal of the second lead wire 52B has the ground potential) is supplied to the second differential A/D converter 162 through the second rectifier 160, and converted into a digital signal. The digital signal is sent to the resistance computation unit 154 through the second digital signal photo-coupler array 164.
(55) In the circuit structure shown in
(56) The resistance computation unit 154 computes the resistance value R1 of the first lead wire 52A based on the voltage value V1 of the first lead wire 52A (voltage applied between both terminals of the first lead wire 52A) from the second voltage measurement unit 152, and the sensing current value I1 supplied to the first lead wire 52A, and computes the resistance value R2 of the second lead wire 52B based on the voltage value V2 (voltage applied between both terminals of the second lead wire 52B) from the second voltage measurement unit 152 and the sensing current value I2 supplied to the second lead wire 52B. These resistance values R1 and R2 are supplied to the determination unit 148.
(57) The determination unit 148 stores the resistance value R1 of the first lead wire 52A and the resistance value R2 of the second lead wire 52B when operation of each battery module 28 is started for the first time, as reference resistance values Ra and Rb, respectively, in a memory. Further, as described above, the memory stores the expected change widths (r1 and r2) in the resistance values R1 and R2 of the first lead wire 52A and the second lead wire 52B due to expected changes in the temperature and a threshold value r.sub.th used for comparison with the difference R.
(58) Further, based on the resistance values R1 and R2 supplied form the resistance computation unit 154 in real time, and reference resistance values Ra and Rb, the determination unit 148 calculates the resistance change R1 (=|R1Ra|) of the first lead wire 52A, the resistance change R2 (=|R2Rb|) of the second lead wire 52B, and the difference R (|R1R2|) between the resistance value R1 and the resistance value R2.
(59) Further, if any one or more of the following relational equations (a) to (c) are satisfied, the determination unit 148 determines that leakage of active material has occurred in one or more battery cells 26 of the battery module 28, and outputs a leakage detection signal including information of the battery module 28 (module number, etc.).
R1>r1Relational inequality (a):
R2>r2Relational inequality (b):
R>r.sub.thRelational inequality (c):
(60) The leakage detection signal from the determination unit 148 is sent to, e.g., a remote monitoring device through the interface 122 and the external cable (including the network).
(61) As described above, in the control device 100 according to the embodiment of the present invention, the heat insulating container 10 contains the first lead wire 52A and the second lead wire 52B provided separately from the heater wire 44, the resistance measurement unit 146 for measuring the resistance value R1 of the first lead wire 52A and the resistance value R2 of the second lead wire 52B, and the determination unit 148 for outputting the leakage detection signal indicating the presence of leakage of active material from the battery module 28 if there is a change in the resistance values R1 and R2 measured by the resistance measurement unit 146. Therefore, it is possible to easily detect the presence of battery modules 28 having leakage of active material, and it is possible to realize a failure detection scheme which is different from the scheme of detecting changes in the depth of discharge in each block. Consequently, it is possible to detect the presence of battery modules 28 having leakage of active material in real time, and avoid the risk of the delay in the initial response to the occurrence of a failure.
(62) It is a matter of course that the battery assembly heat insulating container, the battery assembly control device, and the battery assembly failure detection method according to the present invention is not limited to the embodiments described above, and various structure can be adopted without deviating the gist of the present invention.