Invention Grant
- Patent Title: Method of identifying the balancing configuration installed on a turbine engine rotor
-
Application No.: US15111414Application Date: 2015-01-05
-
Publication No.: US10598017B2Publication Date: 2020-03-24
- Inventor: Valerio Gerez , Francois Prost
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1450250 20140113
- International Application: PCT/FR2015/050007 WO 20150105
- International Announcement: WO2015/104488 WO 20150716
- Main IPC: F01D5/02
- IPC: F01D5/02

Abstract:
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.
Public/Granted literature
- US20160333695A1 METHOD OF IDENTIFYING THE BALANCING CONFIGURATION INSTALLED ON A TURBINE ENGINE ROTOR Public/Granted day:2016-11-17
Information query