Invention Grant
- Patent Title: Gas turbine architecture
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Application No.: US14865838Application Date: 2015-09-25
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Publication No.: US10202905B2Publication Date: 2019-02-12
- Inventor: Gideon Daniel Venter
- Applicant: Rolls-Royce Deutschland Ltd & Co KG
- Applicant Address: DE Dahlewitz
- Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
- Current Assignee Address: DE Dahlewitz
- Agency: Oliff PLC
- Priority: GB1417504.6 20141003
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F02C3/04 ; F01D15/12 ; F02C7/06 ; F02K3/04 ; F01D25/04 ; F16H57/08

Abstract:
A geared architecture for a gas turbine comprising an output shaft for connection with a fan, an input shaft and a gearbox connecting the input shaft with the output shaft. The gearbox has a forward planet carrier plate supported by a forward radially fixed bearing structure and a rearward planet carrier plate supported by a rearward radially fixed bearing structure. By supporting the carrier plates on radially fixed bearing structures the planet carriers can rotate about their own axis to lower vibration and mesh forces within the gearbox.
Public/Granted literature
- US20160097330A1 GAS TURBINE ARCHITECTURE Public/Granted day:2016-04-07
Information query
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