AIRCRAFT TURBOJET ENGINE FAN ROTOR Russian patent published in 2014 - IPC F01D5/32 F04D29/34 

Abstract RU 2525817 C2

FIELD: transport.

SUBSTANCE: fan rotor contains fan blades (15) attached to periphery of wheel (13). Each blade has blade tail engaged with groove in this wheel and held in it by main fixture (28). The main fixture is engaged with slots (34) formed adjacent to superposed end of corresponding groove and on each its side to counteract blade tail movement in axial direction. The main fixture (28) is connected with additional fixture differing from the main fixture. Additional fixture is spaced from the main fixture by predetermined distance. The additional fixture (32) is located between the main fixture and superposed end of blade tail engaged with groove. The additional fixture (32) preferably is thin wall.

EFFECT: invention allows fixture to dissipate impact energy and minimise damage to adjacent blades and parts while keeping structure simple and cheap.

6 cl, 6 dwg

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RU 2 525 817 C2

Authors

Bjuisson Ehrve

Goga Zhan-Ljuk

Dates

2014-08-20Published

2010-04-19Filed