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Fuel pump control unit FPC

Fuel pump control unit FPC

Fuel pump control unit FPC is part of a fuel pump in civil aircraft. The fuel pump is propelled by brushless DC (BLDC) motor in explosion-proof design. FPC controls run-up, rotational speed, and maximum current of the BLDC motor. FPC control unit allows setting, monitoring, and recording of all operational parameters.

FPC unit functions

Control function

FPC unit controls:

Checking function

FPC control unit disconnect the BLDC motor under following events:

FPC control unit limits BLDC motor speed under following events:

Monitoring and archiving functions

FPC control unit performs monitoring and recording of several emergency states:

Technical specification

Nominal voltage supply: 28.0V DC
Operational voltage supply: 22V až 30,3V DC
Marginal voltage supply: 18.0V až 32,2V DC
Maximum continuous BLDC motor power consumption: 200W
Weight: 250g

FPC control unit is designed in accordance with aviation standards RTCA/DO-160D, RTCA/DO-178B, RTCA/DO-254, FAA AC 23.1309-1C, and FAR 23. HW criticality according to RTCA/DO-254 and SW criticality according to RTCA/DO-178B are at level C - major.

FPC control unit applications

FPC control unit is intended for control of LUN 6282.XX in-tank booster fuel pump manufactured by Jihostroj, a.s., Velešín, Czech Republic.

This in-tank booster fuel pump is, together with FPC control unit, used in civil transport aircraft Ae270 (manufactured by Ibis Aerospace Ltd.), or in multipurpose twin-engine amphibian aircraft Be-103 (manufactured by Beriev).

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Available documents:

# FPC datasheet (459.32 kB)

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