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Tool for handling high pressure module of turbojet of aircraft, has fixing arms connected to vertical branches of support body by pivot joint, so as to allow rotation of high pressure module about horizontal rotation axis between branches
Tool for handling high pressure module of turbojet of aircraft, has fixing arms connected to vertical branches of support body by pivot joint, so as to allow rotation of high pressure module about horizontal rotation axis between branches
The tool has a support body (7) having an inverted U-shape and defining a horizontal beam (70) and two vertical branches (71, 72). Two fixing arms (81, 82) are attached to a high pressure module of a turbojet of an aircraft, where the fixing arms are connected to the vertical branches of the support body by a pivot joint (9), so as to allow rotation of the high pressure module about a horizontal rotation axis (V) between the branches of the support body. The socket body includes a fixing ring (73) for connection to a traction chain.
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