Invention Grant
- Patent Title: Shim for a turbojet blade
- Patent Title (中): Shim用于涡轮喷气发动机叶片
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Application No.: US11519015Application Date: 2006-09-12
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Publication No.: US07938626B2Publication Date: 2011-05-10
- Inventor: Jean-Bernard Forgue , Jack-Pierre Lauvergnat , Thierry Nitre , Patrick Jean-Louis Reghezza
- Applicant: Jean-Bernard Forgue , Jack-Pierre Lauvergnat , Thierry Nitre , Patrick Jean-Louis Reghezza
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0509420 20050915
- Main IPC: F01D5/32
- IPC: F01D5/32

Abstract:
A shim for a turbomachine blade is disclosed. The shim includes two branches which wrap around flanks of a blade root, and two tabs. Each of the tabs extend from one end of a respective one of the two branches. The tabs are folded towards each other and are interconnected in such a manner as to prevent them from unfolding. Advantageously, the shim includes a connection part which interconnects the tabs in such a manner as to prevent them from unfolding. The connection part is assembled to the tabs in such a manner as to allow the branches of the shim to spread apart. For example, the connection part can be suitable for stretching in the direction for spreading the branches apart.
Public/Granted literature
- US20100226777A1 Shim for a turbojet blade Public/Granted day:2010-09-09
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