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Help CenterBatería de Níquel Cadmio Alcalina Sinterizada 20FP25H1C-R Para Aeronaves, Celda de Batería NI-CD de 1.2V 25Ah
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1.1 Purpose
The 20FP25H1CT-R battery pack (hereinafter referred to as the "battery pack") is mainly used for aircraft
Airborne emergency power supply. It can directly or indirectly start the aircraft engine and operate it before the aircraft engine starts working
Or provide emergency 24V DC power supply in case of generator failure.
1.2 Composition
The battery pack is mainly composed of individual batteries, combination shells, sockets, and other parts.
1.3 Usage Requirements
This "User and Maintenance Manual" is an important document for the use and maintenance of battery packs, and must be followed according to the instructions
Okay, otherwise, it will shorten the lifespan of the battery pack.
When conducting ground maintenance and inspection on an aircraft, the ground power supply (such as a power truck) should be connected, and the battery should not be used
Operate the battery pack (such as the roof cover), otherwise it will shorten the lifespan of the battery pack.
2 Main technical parameters
2.1 Rated capacity: 25 Ah (1-hour rate discharge).
2.2 Nominal voltage: 24V.
2.3 Maximum weight: 24.36 kg (charged electrolyte).
2.4 Maximum external dimensions: 370 mm × 174 mm × 229 mm.
2.5 Working conditions:
a) The ambient temperature should be between -10 ℃ and 50 ℃. If subjected to temperatures between -60 ℃ and 60 ℃, electricity should be used
Restore the temperature of the solution to the working temperature;
b) Airborne flight altitude ≤ 30000 meters (1170Pa);
c) The effect of 98m/s2 overload acceleration, with the acceleration direction from cover to bottom;
d) Under standard conditions, it can withstand an impact of 196m/s2, a vibration frequency of 5 Hz to 300Hz, and an acceleration of 49m/s2;
e) The aircraft charges the battery pack at a constant voltage of 28.5V ± 0.5V.
2.6 Open circuit voltage of rechargeable battery pack: not less than 25.5V.
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