Invention Application
- Patent Title: BLADE RETENTION FEATURES FOR TURBOMACHINES
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Application No.: US16987747Application Date: 2020-08-07
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Publication No.: US20210108522A1Publication Date: 2021-04-15
- Inventor: Andrea Depalma , Antonio Giuseppe D'Ettole , Matteo Renato Usseglio
- 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: IT102019000014724 20190813
- Main IPC: F01D5/30
- IPC: F01D5/30 ; F01D5/02

Abstract:
A turbomachine includes a rotatable annular outer drum rotor connected to a first plurality of blades. Each of the first plurality of blades includes a blade root portion secured to the rotatable annular outer drum rotor. Each of the blade root portions includes one or more structural radial retention features for radially retaining each of the blade root portions within the rotatable annular outer drum and one or more axial retention features for axially retaining each of the blade root portions within the rotatable annular outer drum.
Public/Granted literature
- US11156109B2 Blade retention features for turbomachines Public/Granted day:2021-10-26
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