Invention Application
- Patent Title: GAS TURBINE ENGINE TURNING SYSTEM
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Application No.: US16497951Application Date: 2018-03-23
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Publication No.: US20210108568A1Publication Date: 2021-04-15
- Inventor: Antonio Caimano , Paolo Altamura , Massimo Civardi , Giorgio Rivetto
- Applicant: GE Avio S.r.l.
- Applicant Address: IT Rivalta di Torino
- Assignee: GE Avio S.r.l.
- Current Assignee: GE Avio S.r.l.
- Current Assignee Address: IT Rivalta di Torino
- Priority: EP17425037.3 20170328
- International Application: PCT/EP2018/057480 WO 20180323
- Main IPC: F02C7/32
- IPC: F02C7/32 ; F02C7/06 ; F02C7/275 ; F01D21/14 ; F01D21/12 ; F01D25/36

Abstract:
A gas turbine engine (10) includes a compressor section, a turbine section, and an accessory gearbox (100). A turning unit (200) for the gas turbine engine includes an output assembly (204) configured to be mechanically coupled to the gas turbine engine, and an electric motor (202). The electric motor is operable to rotate, through the output assembly, one or more components of the compressor section or the turbine section at a rotational speed less than about fifty revolutions per minute during a shut-down condition of the gas turbine engine.
Public/Granted literature
- US11536202B2 Gas turbine engine turning system Public/Granted day:2022-12-27
Information query
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