Overview
The 2758 Saft nickel-cadmium battery consists of a stainless steel box (020), containing 20 individual cells VHP230KA-3. These cells are connected in series to obtain 24 V nominal. Individual cells are enclosed in a container that provides insulation, allowing them to be fitted side-by-side in the battery box. Interconnection of cells is via rigid, highly conductive, nickel-plated copper links (270 to 310). Each link is held in place by nickel-plated copper nuts (350) on the cells’ terminals. Inside the battery box, individual cells are held in place by partitions, liners and spacers (130), and a cover complete (050). The connector (200) connects the battery to the aircraft DC power.
ALL NICAD BATTERIES ARE UNCHARGED
Features
- Type of cells : VHP230KA-3
- Number of cells : 20
- Nominal voltage : 24 V
- Rated capacity C1Ah (Ah): 23 Ah
- Charge or discharge current 1 C1A : 23A
- Charge current 0.5 C1A : 11.5A
- Charge current 0.1 C1A : 2.3A
- Electrolyte : Solution of KOH
- Electrolyte level (mm): 20 mm (0.79 in)
- Consumable volume of electrolyte per cell : 60 cm3 (4.88 in3)
- End of charge voltage : 1.55 V / per cell
- End of life criterion in % : 100%
- End of life criteria in hour or minutes : 1 hour
- Battery maximum weight : 25.5 kg (56.2 lbs)
- Battery terminals : Connector according to ISO 5064/11 or MS 3509
Benefits
- The batteries are connected to the aircraft system:
- According to the aircraft manufacturer, to start the engine or the APU.
- On the ground, to provide power before electrical power is supplied to the aircraft systems.
- In flight, if a malfunction or a failure occurs in the power supply system.
Aircraft Application
- Airbus : A319, A320, A321
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