Invention Grant
- Patent Title: Device for masking a turbomachine rotor
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Application No.: US16382059Application Date: 2019-04-11
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Publication No.: US11261743B2Publication Date: 2022-03-01
- Inventor: Nicolas Léon Jean-Baptiste Besnard , Romain Jean-François Guerit , Laurent Miguel Sanchez
- 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: FR1853193 20180412
- Main IPC: F01D5/28
- IPC: F01D5/28 ; F01D11/00 ; F01D25/00

Abstract:
A device for masking the inner periphery of a disc of a turbine engine generally includes a lower element, an upper element, and an elastic annular seal. The lower element, the upper element, and the elastic annular seal are coaxial, the elastic annular seal arranged longitudinally between the lower element and the upper element. The seal generally includes a lower annular part bearing radially and internally against the lower element, and an upper annular part bearing radially and internally against the upper element. The lower part and the upper part are connected to one another by an annular central part forming a return element. The elastic annular seal is configured to bear longitudinally, radially, and externally against each longitudinal end of said inner periphery of the disc to mask said inner periphery, and a clamping system capable of clamping the seal between the lower element and the upper element.
Public/Granted literature
- US20190316476A1 DEVICE FOR MASKING A TURBOMACHINE ROTOR Public/Granted day:2019-10-17
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