Method of identifying the balancing configuration installed on a turbine engine rotor
A method of identifying the balancing configuration installed on a turbine engine rotor using a plurality of screws forming balance weights that are mounted on the rotor at different angular positions of the rotor is provided. Each screw possesses a predetermined weight and each screw is associated with an element for identifying its weight and for identifying its angular position on the rotor. The method includes contactless scanning of all of the screws mounted on the rotor by an identification appliance capable of recognizing the elements for identifying the weight and the angular position associated with each screw.
1. A method of identifying a balancing configuration installed on a turbine engine rotor by:
mounting a plurality of screws forming balance weights on the turbine engine rotor at different angular positions of the turbine engine rotor, each screw of the plurality of screws possessing a predetermined weight, and each screw of the plurality of screws being associated with an element for identifying its weight and another element for identifying its angular position on the turbine engine rotor, and
contactless scanning of the plurality of screws mounted on the turbine engine rotor by an identification appliance capable of recognizing the element for identifying the weight and the element for identifying the angular position associated with each screw of the plurality of screws.
2. The method according to claim 1 , wherein the identification appliance is a digital camera associated with image processing software.
3. The method according to claim 2 , wherein the turbine engine rotor further comprises holes which present an element visually identifying the angular position of each screw mounted therein on the turbine engine rotor, and each screw of the plurality of screws has a screw head comprising a visual characteristic, said visual characteristic associated with the weight of each screw on which each screw head is provided.
4. The method according to claim 3 , wherein the element visually identifying the angular position on the turbine engine rotor of each screw is a visual mark applied in a vicinity of each hole in the turbine engine rotor and associated with a determined angular position on the turbine engine rotor.
5. The method according to claim 4 , wherein the visual mark applied in the vicinity of each hole of the turbine engine rotor is a number.
6. The method according to claim 3 , wherein each visual characteristic of each screw head includes a particular shape and/or color.
7. The method according to claim 1 , wherein the identification appliance is an RFID tag reader associated with data processing software.
8. The method according to claim 7 , wherein each screw of the plurality of screws is mounted in a hole of the turbine engine rotor by a nut, each screw of the plurality of screws having an RFID tag with an electronic chip containing an element for identifying the weight of each screw on which the RFID tag is provided, and each nut having an RFID tag with an electronic chip containing an element identifying the angular position of each screw on which the RFID tag is provided, on the turbine engine rotor.
9. The method according to claim 1 , including a prior step of establishing a table listing each of the elements for identifying the weight and the angular position of each screw.
10. The method according to claim 1 , further including automatically storing and transmitting the identified balancing configuration to an avionics system.
11. The method according to claim 4 , wherein the visual characteristic of each screw head includes particular shapes and/or colors.
12. The method according to claim 5 , wherein the visual characteristic of each screw head includes particular shapes and/or colors.