Hello,
I was just wondering, about the purpose of the 10-pin battery connector. Is there a possibility that they made it like that, to have cell redundancy?
I mean that assuming you have 4 x (4 cells in series), being parallel connected via some kind of semiconductor switches, and the full capacity of the battery is 5350 mAh, then if a cell brakes down during flight, the intelligent battery monitor board, could disconnect 1 row of (4 cells in series), and run the aircraft with the remaining (3/4) X 5350= 4012 mAh.
The other obvious reason to have the 10-pin connector, would be for larger contact area and thus lower resistance on the current path.
I have not yet seen a P4 battery disassembled, to have more data.
(If at least 4 power cables connect the cells to the monitor board, perhaps that is the case)
Thanks
I was just wondering, about the purpose of the 10-pin battery connector. Is there a possibility that they made it like that, to have cell redundancy?
I mean that assuming you have 4 x (4 cells in series), being parallel connected via some kind of semiconductor switches, and the full capacity of the battery is 5350 mAh, then if a cell brakes down during flight, the intelligent battery monitor board, could disconnect 1 row of (4 cells in series), and run the aircraft with the remaining (3/4) X 5350= 4012 mAh.
The other obvious reason to have the 10-pin connector, would be for larger contact area and thus lower resistance on the current path.
I have not yet seen a P4 battery disassembled, to have more data.
(If at least 4 power cables connect the cells to the monitor board, perhaps that is the case)
Thanks
