TURBOFAN JET ENGINE WITH LEVER OF AUXILIARY JOINT AND LEVER OF AUXILIARY JOINT Russian patent published in 2009 - IPC F02K3/04 

Abstract RU 2358137 C2

FIELD: engines and pumps.

SUBSTANCE: turbofan jet engine includes external body, which is connected by radial levers with annular internal device, downstream of which shell is installed opposite to external body, and shell forms fairing, auxiliary parts on external side of external body and auxiliary parts on internal side of shell. The present invention is characterised by the fact that turbofan jet engine includes at least one single-block lever, which is installed parallel to radial lever for connection of auxiliary parts between external side of external body and internal side of shell.

EFFECT: increased efficiency factor.

11 cl, 8 dwg

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RU 2 358 137 C2

Authors

Gan'E P'Er

Lefrank Lionel' Zhan Leon

Letash Zhonni

Taglialavor Zhozef

Dates

2009-06-10Published

2005-09-26Filed