A tool for removing an annular part mounted around a shaft of a turbomachine, includes a holder configured to cooperate with a lifting system, a system for coupling and holding the annular part, the coupling and holding system being secured to the holder, the system for coupling and holding having an opening designed to receive the shaft of the turbomachine during the removal of the annular part, the coupling and holding system being rotatable with respect to the holder between a first position and a second position by a rotation system for tilting the annular part with respect to the holder when the coupling and holding system is fastened to the annular part.

A fender mounted hoist has a frame having lifting points for receiving one or more ratchets. The frame is mounted over a fender well. The fender well includes a right fender well and a left fender well. The right fender well includes a right fender well inside frame, a right fender well base, and a right fender well wall. The left fender well includes a left fender well inside frame, a left fender well base, and a left fender well wall. A main beam has a left end of the main beam and a right end of the main beam. The main beam of the frame is horizontally oriented. A left leg is connected to the frame at the left end of the main beam, and a right leg is connected to the frame at the right end of the main beam.

An engine hoist attachment assembly for hoisting a vehicle component includes a tube, a bar, and a pair of rods. The tube has a first end that is configured to slidably insert a terminus of a boom of an engine hoist to removably couple the tube to the boom. The bar has a back face that is coupled to and extends bidirectionally and perpendicularly from a second end of the tube so that the bar is substantially parallel to a surface upon which the engine hoist is positioned. The pair of rods is coupled to and extends in parallel from a front face of the bar. The rods are configured to position under a vehicle component, positioning a user to utilize the engine hoist to selectively lift and lower the vehicle component.

An end effector includes an elongated body that is non-circular in cross section. A guide rail is mounted on a top surface of the elongated body. A hook carriage includes a linear motion guide that moves linearly along the guide rail to position a hook member. A locking mechanism locks the hook carriage at a preselected position along a length of the guide rail.

A method for transporting a turbine engine held by a transport kit by a carriage. The transport kit connected to a connection member hoists the engine to connect to an aircraft fuselage. The transport kit is a structure which includes a hoisting interface (328) arranged on a rigid hoisting arm (318) which extends over the turbine engine and is connected to a rigid transport arm (316) which extends over a lateral side of the turbine engine. The transport arm is connected to at least two engine mounts (340) solid with the turbine engine. The transport arm (316), or one of the engine mounts connected to the transport arm, includes a transport interface (324) that can be supported by a bearing element (332) of a truck (326) used for transporting the turbine engine.

A hoist for removing an object to enable an individual to work on the object includes a first substantially vertical support mounted on a floor surface. A second substantially vertical support mounted on the floor surface and being spaced a predetermined distance away from the first substantially vertical support. The first and second substantially vertical supports include an upper surface. A substantially horizontal member extending across the upper surfaces of the first and second substantially vertical supports. A first vertical lift is operatively positioned within the first substantially vertical support. A second vertical lift is operatively positioned within the second substantially vertical support. The first and second vertical lifts selectively raising the member relative to the floor surface. A winch is operatively mounted on the substantially horizontal member for lifting the object relative to the member for enabling an individual to work on the object.

The invention relates to the field of support interfaces, and in particular to such a support interface (30a, 30b) for an engine casing (90) and comprising a coupling part (50), a first plurality of bolts (80), and a plurality of pegs (70). The coupling part (50) has an outer face (52) presenting a cavity (42) suitable for receiving a support arm (20a, 20b), and an inner face (51) suitable for being mounted on an outer face (93) of the engine casing (90), together with a first plurality of orifices (53) between the outer face (52) and the inner face (51) of the coupling part (50). Each bolt (80) has a threaded shank (82) received in an orifice (53) of the first plurality of orifices (53), and a head (81) suitable for bearing against the outer face (52) of the coupling part (50). Each peg (70) has a threaded orifice (71) in which the threaded shank (82) of one of the bolts (80) of the first plurality of bolts (80) is engaged through a first end of the peg (70), each peg having a second end that is enlarged and suitable for bearing against an inner face (92) of the engine casing (90).

An end effector includes a body having a cavity located therein. The body partially encloses the cavity and includes an opening through the body to the cavity that is sized to receive a hanger hook. A hooking structure is located within the cavity. A latch is movably received by the body. The latch has a closed position that reduces the size of the opening and an open position that increases the size of the opening.

A rotary assembly for a hoist includes at least one of a rotary union and a slip ring. A bearing is positioned radially outward of the rotary union and/or slip ring with respect to a central axis. A first plurality of axially extending support columns are radially outward of the rotary union and/or slip ring and fixed to the bearing. A second plurality of axially extending support columns are radially outward of the rotary union and/or slip ring and fixed to the bearing. The second plurality of axially extending support columns is axially opposite the bearing from the first plurality of axially extending support columns.

A jacking assembly for a rotor of a turbine includes an arc-shaped saddle which extends around and supports a lower portion of a rotor. A lifting beam extends over the rotor transversely to an axial direction of the rotor. The lifting beam is axially aligned with the arc-shaped saddle. Two connectors are disposed on respective lateral sides of the rotor, each connector extending between and being coupled to the lifting beam and the arc-shaped saddle such that the saddle is configured to lift the rotor vertically when the lifting beam is displaced vertically.