SEALING GASKET OF PLATFORM IN TURBOMACHINE ROTOR Russian patent published in 2014 - IPC F01D11/00 

Abstract RU 2511897 C2

FIELD: engines and pumps.

SUBSTANCE: object of this invention is sealing gasket of intermediate platform between two adjacent blades in prolonged turbomachine rotor with inlet and outlet ends containing transversally in width direction a contact part, a fastening part and a flexible part between the fastening part and the contact part. It differs by the fact that its transverse section has a form changing between its two ends, at that the flexible part is narrower than the contact part.

EFFECT: higher tightness between blades and platforms of turbomachine rotor.

9 cl, 5 dwg

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RU 2 511 897 C2

Authors

Forg Zhan-Bernar

Regezza Patrik Zhan-Lui

Stoshmil' Karol'

Dates

2014-04-10Published

2009-12-10Filed