VORTEX GENERATORS AT INLET OF COMPRESSOR BLADE SYSTEM Russian patent published in 2016 - IPC F04D29/68 F04D29/54 

Abstract RU 2583190 C2

FIELD: machine building.

SUBSTANCE: present invention relates to an assembly (2) with blades (1), in particular of straightening unit for turbomachine compressor. Assembly (2) with blades (1) contains multiple individual devices (14A) acting on a flow, which are formed so as to generate swirling (16). Each of said individual devices (14A) is provided at inlet of said unit (2) with blades (1) so as to simultaneously affect main flow (E) and recirculation flow (G).

EFFECT: reduced tearing obtained due to present invention allows to improve efficiency of compressor (3) and widens range of stability.

12 cl, 8 dwg

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RU 2 583 190 C2

Authors

Domerk Olive Stefan

Perro Vensan Pol Gabriel

Pestej Anes

Dates

2016-05-10Published

2011-05-25Filed