Invention Grant
- Patent Title: Deflector for a mechanical reduction gear of an aircraft turbine engine
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Application No.: US16691504Application Date: 2019-11-21
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Publication No.: US11339724B2Publication Date: 2022-05-24
- Inventor: Jean-Charles Michel Pierre Di Giovanni , Adrien Louis Simon
- Applicant: SAFRAN TRANSMISSION SYSTEMS
- Applicant Address: FR Colombes
- Assignee: SAFRAN TRANSMISSION SYSTEMS
- Current Assignee: SAFRAN TRANSMISSION SYSTEMS
- Current Assignee Address: FR Colombes
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: FR1871750 20181123
- Main IPC: F16H57/04
- IPC: F16H57/04 ; F02C7/36 ; F01D25/18 ; F16H57/08

Abstract:
A deflector for a mechanical reduction gear of a turbine engine, for example of an aircraft, is configured to be inserted between two adjacent planets of the reduction gear. The deflector includes a block having a first lateral surface that is cylindrical and concave and has a radius of curvature R1 measured from an axis G1. The block also has a second lateral surface, opposite the first lateral surface, that is cylindrical and concave and that has a radius of curvature R1 measured from an axis G2 that is parallel to G1. Each of the first and second surfaces has at least one protruding tab having a generally elongate shape about the respective axis G1, G2 of the surface considered and having an internal periphery that is concavely curved and a has radius of curvature R2 measured from the respective axis G1, G2, R2 being less than R1.
Public/Granted literature
- US20200166118A1 DEFLECTOR FOR A MECHANICAL REDUCTION GEAR OF AN AIRCRAFT TURBINE ENGINE Public/Granted day:2020-05-28
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