METHOD TO PRODUCE GAS TURBINE AXIAL COMPRESSOR DIFFUSER VANES Russian patent published in 2010 - IPC B23P15/02 B23H9/10 B23H7/02 F01D5/14 

Abstract RU 2383421 C1

FIELD: power engineering.

SUBSTANCE: vane comprises aerodynamically streamline bent airfoil portion with leading and trailing edges and shank portion. Lengthwise through starting hole is made on airfoil portion leading edge side. Said lengthwise starting hole is made by electric charge machining with the help of rotary discharge electrode. Thereafter, electric charge machining is further used along with discharge wire to cut out inner channel for working medium.

EFFECT: higher accuracy and reliability, reduced heat carrier leaks.

5 cl, 15 dwg, 1 ex

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Authors

Zjabrev Sergej Viktorovich

Andropov Valerij Sergeevich

Verst Viktor Gennad'Evich

Nikolaev Dmitrij Valerievich

Dates

2010-03-10Published

2008-07-10Filed