a so-called tertiary locking assembly for a thrust reverser, manually controlled switch for a locking assembly, thrust reverser for a turbojet engine nacelle and turbojet engine nacelle

摘要

a so-called tertiary locking assembly for a thrust reverser, manually controlled switch for a locking assembly, thrust reverser for a turbojet engine nacelle and turbojet engine nacelle The invention relates to a so-called tertiary locking assembly for a thrust reverser thrust reverser, with which a turbojet engine nacelle is provided, said locking assembly including at least one so-called tertiary closure associated with at least one primary control line (2) comprising at least one electromechanical control means (3). ), as well as a power source (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 primary control line, said secondary control line being additionally provided with at least one manually controlled switch (50).