Aircraft engine module handling assembly
View Patent ↗An aircraft engine module handling assembly including a carriage, a pivoting portion at a top of the carriage, a module support tooling, and an additional mechanism for assembly of the tooling on the pivoting portion, such that the module can be rotated from an original vertical position, observed when it reaches an assembly shop in a crate, to a horizontal position suitable for its assembly with another module of an engine.
1. An aircraft engine module handling assembly, comprising:
a moving carriage; and
tooling positioned at an end of the module, wherein the tooling includes a mount and devices for attachment to the module;
wherein the carriage includes an upper structure set up on a support frame, and a pivot for pivoting the upper structure with respect to the support frame around a horizontal axis, and
wherein additional devices are provided on the upper structure and the tooling for securing the tooling to the upper structure in a position in which an axis of rotation of the module intersects the horizontal axis and can be pivoted from a vertical direction to a horizontal direction.
2. An aircraft engine module handling assembly according to claim 1 , wherein the additional devices include a groove limited by overhanging edges, wherein a skid sliding in the groove and attached to a projection of the tooling extends out of the groove, with a stop of the skid in the groove and means of immobilizing the skid at the stop in the groove.
3. An aircraft engine module handling assembly according to claim 1 , further comprising a device for raising the frame.
4. An aircraft engine module handling assembly according to claim 3 , wherein the device for raising the frame includes a table independent of the carriage, and on which the carriage can roll, and wherein immobilizing stops are provided between the table and the carriage.
5. An aircraft engine module handling assembly according to claim 1 , further comprising a lifting arm configured to be assembled at one end with the tooling and, at an opposite end, at a location of the module which is opposite the tooling.
6. An aircraft engine module handling assembly according to claim 1 , wherein the pivot is driven by a motor.
7. An aircraft engine module handling assembly according to claim 2 , wherein the groove is provided in a bracket disposed at a top of the upper structure, and the pivot is fitted in the bracket.