Invention Grant
- Patent Title: Modular calibration rotor for a horizontal balancer
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Application No.: US15578204Application Date: 2016-06-29
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Publication No.: US10197467B2Publication Date: 2019-02-05
- Inventor: Alain Roland Luinaud , Alain Decocq , Christophe Guengant
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1556355 20150706
- International Application: PCT/FR2016/051622 WO 20160629
- International Announcement: WO2017/006016 WO 20170112
- Main IPC: G01M1/04
- IPC: G01M1/04 ; G01M1/02 ; G01M1/06

Abstract:
A calibration rotor for a horizontal balancer, configured to be driven by a driver. The calibration rotor includes a main barrel that has a longitudinal axis and the periphery of which includes points for attaching balance weights that are evenly distributed in an axial and angular manner about the axis. A rotation guide is arranged at each end of the main barrel. The rotor is modular, and the rotation guide includes adapters (40, 42) which are capable of being configured to be attached to the ends of the barrel. The guide is of a first type, suitable for rotatably guiding the barrel on rollers, or of a second type, suitable for rotatably guiding the half-shell barrel. Each type of adapter has the same predetermined moment of inertia and is interchangeable on the barrel.
Public/Granted literature
- US20180149544A1 MODULAR CALIBRATION ROTOR FOR A HORIZONTAL BALANCER Public/Granted day:2018-05-31
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