Invention Grant
- Patent Title: Turbine overspeed disengagement device for a turbine engine
-
Application No.: US17791829Application Date: 2021-01-08
-
Publication No.: US11761345B2Publication Date: 2023-09-19
- Inventor: Antoine Hervé Dos Santos , Joao Antonio Amorim , Pascal Grégory Casaliggi , Nicolas Xavier Trappier
- 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: FR 00227 2020.01.10
- International Application: PCT/FR2021/050021 2021.01.08
- International Announcement: WO2021/140301A 2021.07.15
- Date entered country: 2022-07-08
- Main IPC: F01D21/04
- IPC: F01D21/04 ; F01D5/02

Abstract:
An assembly for a turbine engine turbine includes a turbine rotor disc centered on a longitudinal axis and a turbine shaft centered on the longitudinal axis and driven in rotation by the rotor disc. Torque from the rotor disc is transmitted to the shaft, wherein the rotor disc is locked in translation relative to the shaft in the direction of the longitudinal axis by a screwed member on the shaft. Torque from the rotor disc is transmitted from the rotor disc to the screwed member when the torque ceases being transmitted from the rotor disc to the shaft. The screwed member has an unscrewing direction identical to the direction of rotation of the rotor disc in operation.
Public/Granted literature
- US20230033362A1 TURBINE OVERSPEED DISENGAGEMENT DEVICE FOR A TURBINE ENGINE Public/Granted day:2023-02-02
Information query