Tool and method for frontal unscrewing of a link nut in a twin-spool turbine
View Patent ↗A method for unscrewing a link nut of an HP rotor of a twin-spool turbine, including a front fan, an intermediate casing, a HP module with a HP rotor, and a LP turbine module, the intermediate casing including a support bearing for the HP rotor, the rotor being retained in the bearing by the link nut, the method including: placing an unscrewing tool in front of the link nut after having removed the fan and released access to the nut from the front; with rotation of the HP rotor locked and the frontal unscrewing tool including a socket spanner including teeth having a shape that complements that of teeth of the link nut, attaching a mounting for the socket spanner to the intermediate casing, the socket spanner being rotatably mounted on the mounting, and applying an unscrewing torque to the socket spanner. An unscrewing tool implements the method.
1. A method for unscrewing a connecting nut of an HP rotor of a twin-spool gas turbine engine including, in order from a front of the gas turbine engine to a rear of the gas turbine engine, a front fan, an intermediate casing, an HP module including the HP rotor, and a LP turbine module, the intermediate casing including a bearing supporting the HP rotor, the HP rotor being retained in the bearing by the connecting nut, the method comprising:
removing the fan at the front of the gas turbine engine so to provide access to the connecting nut from a front side of the gas turbine engine;
placing a support in front of the connecting nut, the support including a cylindrical barrel and four branches radially extending from the barrel so as to present a star shape, the four branches being integrally connected to each other so as to form a single monolithic piece, a first end of each of the branches being connected to the barrel and a second end of each of the branches being free and presenting a thickness in an axial direction;
mounting removable shoes on the second free ends of the branches, the shoes and the second free ends of the branches including holes;
fastening the second free ends of the branches of the support to the intermediate casing via screws passing through the holes in the shoes and the second free ends of the branches so as to fix the support to the intermediate casing;
inserting a tubular wrench into the barrel of the support such that teeth at a first end of the tubular wrench are engaged with teeth of the connecting nut and the tubular wrench is locked axially with respect to the support, shapes of the teeth of the tubular wrench and the connecting nut being complementary to each other;
inserting an anti-rotation tool in the HP rotor to block the HP rotor against any rotational movement; and
applying an unscrewing torque to the tubular wrench;
wherein the removable shoes are selected based on a type of the gas turbine engine.
2. The method as claimed in claim 1 , further comprising removing the LP turbine module,
wherein the anti-rotation tool is a tubular element engaged in a space released by the LP module, a first end of the anti-rotation tool being fixed to a casing of the HP module and at a second end of the anti-rotation tool being secured in rotation with the HP rotor.
3. The method as claimed in claim 1 , wherein each of the shoes includes a protrusion.