Abstract: The sorting installation (1) of the invention includes sorting outlets (2) aligned along a sorting conveyor (3), each outlet being provided with a recess (4) for receiving a tray (5) in which sorted mailpieces (6) are stored. The installation also includes a tray conveyor (8) that extends in a certain conveying direction (F2) under the sorting outlets for the purpose of transporting trays filled with sorted mailpieces from the sorting outlets to a feed inlet (7) of the sorting conveyor. The installation further includes a shuttle robot (9) suitable for traveling on the floor (S1) in autonomous manner along the sorting outlets, the robot including handling means (12) suitable for extracting a tray from a recess of a sorting outlet and for placing it lengthwise on the tray conveyor.

Abstract: The sorting installation (1) of the invention includes sorting outlets (2) aligned along a sorting conveyor (3), each outlet being provided with a recess (4) for receiving a tray (5) in which sorted mailpieces (6) are stored. The installation also includes a tray conveyor (8) that extends in a certain conveying direction (F2) under the sorting outlets for the purpose of transporting trays filled with sorted mailpieces from the sorting outlets to a feed inlet (7) of the sorting conveyor. The installation further includes a shuttle robot (9) suitable for traveling on the floor (S1) in autonomous manner along the sorting outlets, the robot including handling means (12) suitable for extracting a tray from a recess of a sorting outlet and for placing it lengthwise on the tray conveyor.

Abstract: A method of processing mailpieces in a sorting installation including a feed inlet magazine (4) in which the mailpieces (1) for sorting are placed in a stack and on edge so as to be put in series in a sorting conveyor (5), the mailpieces (1) in series and on edge in the sorting conveyor being directed towards sorting outlets having respective stackers (6). The mailpieces (1) for sorting that arrive at the feed inlet magazine while stored in a tray (3) are taken in handfuls from the storage tray to be positioned in a stack and on edge in order to be put into series. The mailpieces (1) sorted into a stacker of a sorting outlet (6) are also transferred in handfuls from the stacker towards a storage tray (3) for the purpose of being recycled to the feed inlet magazine (4) from the sorting outlet (6) having a stacker.

Abstract: An installation (1) for sorting mailpieces (2) includes an unstacker having an unstacking plate (3) suitable for separating a mailpiece at the head of a stack of mailpieces so as to feed a sorting conveyor (4) in which the mailpieces (1), as put into series, are moved in series and on edge. The installation (1) also includes: a feed inlet magazine (6) upstream from the unstacking plate with a motor-driven floor (8) designed to receive a stack of mailpieces (2) on edge; and a retaining paddle (9) that is mounted to move along the magazine and that is suitable for being placed behind the stack to keep it on edge while it is moving on the motor-driven floor towards the unstacking plate.

Abstract: An installation for sorting mailpieces (A) includes a sorting conveyor with sorting outlets (2) and storage trays (3), and further includes a tray conveyor (4) disposed along the sorting conveyor under the sorting outlets, and a shuttle robot (5) suitable for being controlled by a monitoring and control unit (6) for automatically taking hold of a tray in a sorting outlet and for placing it below on the tray conveyor, the shuttle robot also being provided with a safety system arranged to detect the presence of an obstacle being approached in the direction in which the robot is traveling while at a certain safety distance away, and arranged to respond to such detection by reducing the speed of movement of the shuttle robot.

Abstract: A connecting rod for an aeronautical actuator system, having one shaft transmitting forces applied in tension and/or compression along a longitudinal axis of the rod. When the connecting rod is in service, an elastically deformable element connected to the shaft is configured to react to the forces applied to the shaft, and displays elastic deformation when effected by these forces. The deformable element has a peripheral part rigidly connected to a member of the rod in which the shaft is slidably mounted. Measurement means associated with the deformable element determine the forces. The measurement means is partially housed in the deformable element. The deformable element includes a central part elongated along the longitudinal axis, which is rigidly connected to the shaft and in which the measurement means are at least partially housed. An intermediate part runs transversally to the central part and connects the central part and the peripheral part.

Abstract: A flight unit control system having at least one instrumented fastening bolt connecting an aircraft carrier structure and a load path, the instrumented bolt having at least one measurement area for detecting that the load path is under load and including a fastener for locking the instrumented bolt in a position relative to the aircraft carrier structure and load path and wherein the measurement area has two cavities and at least one strain gauge and wherein the fastener includes a plate which is positioned at a threaded end of the instrumented bolt which bears against one of the aircraft carrier structure and the load path and which extends perpendicularly to an axis of the bolt and a nut which is placed at the threaded end of the instrumented bolt to immobilize the instrumented bolt relative to the aircraft structure or the load path.

Abstract: A connecting rod for an aeronautical actuator system, having one shaft transmitting forces applied in tension and/or compression along a longitudinal axis of the rod. When the connecting rod is in service, an elastically deformable element connected to the shaft is configured to react to the forces applied to the shaft, and displays elastic deformation when effected by these forces. The deformable element has a peripheral part rigidly connected to a member of the rod in which the shaft is slidably mounted. Measurement means associated with the deformable element determine the forces. The measurement means is partially housed in the deformable element. The deformable element includes a central part elongated along the longitudinal axis, which is rigidly connected to the shaft and in which the measurement means are at least partially housed. An intermediate part runs transversally to the central part and connects the central part and the peripheral part.

Abstract: The present invention relates to a flight unit control system (S), comprising at least one instrumented fastening bolt (6) connecting an aircraft carrier structure (34) and a load path (36a, 36b), the instrumented bolt having at least one measurement area (61; 62) for detecting that the load path in under load. The system comprises fastening means (4, 11) capable of locking the instrumented bolt (6) in a position relative to the aircraft carrier structure (34) and to the load path (36). The or each measurement area (61; 62) of the instrumented bolt (6) comprises two cavities and at least one strain gauge.

Abstract: A control method for a motor driven linear drive device is provided in which: a device control unit receives information representative of measured speed of said device; on receiving a start-up command, start-up of the motor is not initiated if the measured speed is zero; information representative of the speed of the drive devices is monitored; and a control sequence which brings about rotation of the motor in accordance with a pre-programmed acceleration profile is initiated when rotation of the device caused by an external action is detected.