CAN communication, RS485 communication, controller temperature holding module, fan bus voltage, current acquisition module, PWM output control, speed module, fan speed input acquisition module, fan temperature control module. Electromagnetic compatibility CE101, CE107, RE101, power supply characteristic test GJB181A-2003 Aircraft Power Supply Characteristics Steady state voltage test, voltage spike test and voltage transient test are carried out.
Order Number | Operating voltage(VDC) | Electric current(A) | Power(W) | Maximum speed(RPM) | Operation temperature(℃) | Additional Features | Explanations |
1 | 28 |
2.3 |
64.4 | 23500 | -70℃-85℃ | 4-way fan control |
CAN communication, RS485 communication, controller temperature holding module, fan bus voltage, current acquisition module, PWM output control, speed module, fan speed input acquisition module, fan temperature control module. Electromagnetic compatibility CE101, CE107, RE101, power supply characteristic test GJB181A-2003 Aircraft Power Supply Characteristics Steady state voltage test, voltage spike test and voltage transient test are carried out. |