GAS TURBINE ENGINE BLOWER ROTOR, GAS TURBINE ENGINE WITH SUCH ROTOR AND ROTOR BLADE ROOT RING Russian patent published in 2013 - IPC F01D5/32 

Abstract RU 2488697 C2

FIELD: engines and pumps.

SUBSTANCE: blower rotor comprises disc furnished with blades with roots fitted in slots arranged along disc edges and rings, each being fitted between disc slot bottom and blade root. Front end of every end thrusts against retaining flange attached to disc and comprises ledge extending radially outward to retain blade root front end. Ledge of every ring comprises thrust rear surface for blade root front end to thrust against at overload. Note here that said thrust rear surface is inclined relative to rotational axis of rotor. Other invention of this set relate to gas turbine engine with above described blower rotor and to blade root ring.

EFFECT: decreased weight of gas turbine engine blower rotor.

15 cl, 3 dwg

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RU 2 488 697 C2

Authors

Miller Ksav'E Lui Bartelemi

Servan Rezhi Ehzhen Anri

Verso Filipp

Dates

2013-07-27Published

2009-03-27Filed