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display prevent diagrams from the battery program. In the battery program of these prevent blueprints, a battery condition detection signal thirty is connected to each battery cellular 1 . Battery state detection signal thirty proven within FIG. 7 will get a voltage recognition circuit thirty-one to identify the voltage of each electric battery cell one ; a cell stability signal thirty-two to equal the actual current of each electric battery cellular one ; the heat detection signal 33 in order to identify battery temperature; along with a negative feedback circuit 34 to control these detection as well as balance tour, process signals input through individuals circuits, and result which data in the electric battery state recognition signal 30 via an isolated conversation signal 35 . Battery program of Figure. six is provided with the plurality associated with battery obstructs two , and signals result from battery condition detection tour 30 connected to each electric battery block two tend to be input to some main control circuit 36 . The primary control circuit thirty six regulates battery system based on the signals enter through every battery state recognition signal 30 .
Battery state recognition circuits 30 tend to be applied by surface-mounting on circuit boards 7 . Because shown in FIGS. three-5, the circuit board seven applying battery power condition recognition circuit 30 is connected opposite battery prevent 2 fatal airplane 2 A on top of the electric battery block 2 within the figures. The circuit board seven associated with FIGS. 3 as well as 4 offers each ends attached to endplates four by way of set anchoring screws twenty nine . Additionally, the actual circuit card seven from the figures is also connected via set anchoring screws 29 up of the gas wear out epithelial duct 6 , that is mounted on battery block 2 terminal airplane two A. A circuit board seven could be solidly mounted on the battery prevent two by affixing it towards the gas exhaust epithelial duct