DEVICE TO BRAKE TURBINE OF GAS TURBINE ENGINE IN COLLAPSE OF TURBINE SHAFT, AND DOUBLE-STEP GAS TURBINE ENGINE Russian patent published in 2012 - IPC F01D21/04 

Abstract RU 2469194 C2

FIELD: engines and pumps.

SUBSTANCE: turbine brake comprises rotor with at least one disc with rim. Said rotor drives the shaft and can revolve relative to stator in the case of shaft collapse. Besides, said rotor comprises first and second braking elements. Said first braking element is rigidly engaged with rim and incorporates, at least, one cutting element. Said second braking element is rigidly engaged with stator downstream of said rim to comprise ring-shape element. Said ring is made from material that can be cut by aforesaid cutting element. Both braking elements get in contact due to rotor axial displacement caused by shaft collapse to allow cutting element to cut said ring-shape element of second braking element.

EFFECT: turbine braking in collapse of its shaft.

8 cl, 2 dwg

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RU 2 469 194 C2

Authors

Bar Zhak

Ehskjur Dad'E

Mon Klod

Russelehn Stefan

Dates

2012-12-10Published

2008-05-23Filed