TURBOMACHINE ROTOR SECTION Russian patent published in 2014 - IPC F01D5/30 

Abstract RU 2518749 C2

FIELD: engines and pumps.

SUBSTANCE: turbomachine rotor section has working blade locating grooves extending axially. Every said groove receive working blade including contact surface directed radially inward. To force coolant over rotor end face surface, plate-like sealing elements are forced by centrifugal force to fit in contact surface. To lock sealing elements against circular shift, at least one sealing element has a bore for locking element. Said locking element is locked in said bore and seat aligned therewith and made in blade root. Locking element is locked in said seat by Z-shape plate with first end abutting between sealing element and blade root end face.

EFFECT: simplified assembly/disassembly of locking element.

5 cl, 9 dwg

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RU 2 518 749 C2

Authors

Akhaus Guido

Bushmann Aksel'

Dungs Sasha

Khell' Kharal'D

Kol'K Karsten

Milazar Mirko

Shreder Peter

Fajtsman Vjacheslav

Dates

2014-06-10Published

2010-01-27Filed