AIRCRAFT TURBOMACHINE COMPUTER

摘要

The invention concerns an aircraft turbomachine computer comprising a parallelepiped metal housing (10) containing an electronic circuit incorporating a control channel and a monitoring channel. The housing (10) of the invention comprises a first recess (14) in which a first electronic card (20) for managing the control channel is disposed, and a second recess, separate from the first recess, in which a second electronic card (21) for managing the monitoring channel is disposed, these electronic cards being disposed in two planes oriented at an angle of 90° relative to one another.