Invention Grant
- Patent Title: Gas turbine engine with a geared turbofan arrangement
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Application No.: US15961014Application Date: 2018-04-24
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Publication No.: US10823082B2Publication Date: 2020-11-03
- Inventor: Dominic Boniface
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Blankenfelde-Mahlow
- Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee: Rolls-Royce Deutschland Ltd & Co KG
- Current Assignee Address: DE Blankenfelde-Mahlow
- Agency: Shuttleworth & Ingersoll, PLC
- Agent Timothy Klima
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@6f70176a com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@701769e0
- Main IPC: F16D41/12
- IPC: F16D41/12 ; F02C7/36 ; F01D21/00 ; F02K3/06

Abstract:
A gas turbine engine with a geared turbofan arrangement with a gearbox in a drive train driven by a turbine, a driving side of the gearbox being driveably connected with a propulsive fan, with at least one torque transmission device positioned in the drive train, the torque transmission device having an asymmetric torque transmission characteristic, so that torque is transmittable by the torque transmission device under a nominal rotational direction and no torque is transmittable by the torque transmission device in a non-nominal rotational direction.
Public/Granted literature
- US20180313275A1 GAS TURBINE ENGINE WITH A GEARED TURBOFAN ARRANGEMENT Public/Granted day:2018-11-01
Information query
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