TERTIARY LOCKING ASSEMBLY FOR A THRUST REVERSER

摘要

The invention relates to a so-called tertiary locking assembly for a thrust reverser with which a turbojet engine nacelle is provided, said locking assembly including at least one so-called tertiary lock associated with at least one primary control line (2) comprising at least one electromechanical control means (3), as well as a power supply (4) connected to said electromechanical control means, characterized in that it includes at least one secondary control line (20) comprising at least one electromechanical control means (30), as well as a power supply (40) which is connected to the electromechanical control means and which is separate from the electrical power supply of the primary control line, said secondary control line being further provided with at least one manually controlled switch (50).