FIELD: machine building.
SUBSTANCE: system to prevent wear of the tip airfoil shroud platform of the turbine blade comprises a turbine blade slot formed on the surface of the tip airfoil shroud platforms, and a rigid tube, mounted in the slot and has a durable outer surface. The tip airfoil shroud platform contacts the neighbour tip airfoil shroud platform when the turbine works at the contact surface. The contact surface has an interface that has a profile in the form of letter "Z". The tip airfoil shroud platform urther comprises a cut-off tooth, forming a ledge that runs along the middle of the upper surface of the tip airfoil shroud platform. The interface includes the middle surface of contact corresponding to the middle section of the profile in the form of letter "Z". The middle surface of contact has a substantially rectangular shape which substantially corresponds to the form of cross-section of a shearing tooth.
EFFECT: invention allows to improve wear resistance of the tip airfoil shroud platform of turbine blades, to increase its service life and to facilitate its maintenance.
9 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
AXLE COMPRESSOR BLISK AND ROTOR OF LOW-PRESSURE COMPRESSOR OF AIRCRAFT GAS TURBINE ENGINE | 2019 |
|
RU2740442C2 |
BLADE SYSTEM AND CORRESPONDING METHOD OF MANUFACTURING A BLADE SYSTEM | 2014 |
|
RU2647170C2 |
TURBOMACHINE ROTOR BLADE AND METHOD OF APPLYING WEAR-RESISTANT MATERIAL THEREON | 2014 |
|
RU2658451C2 |
TURBINE ROTOR, DEVICE AND METHOD TO PRODUCE IT | 2006 |
|
RU2375589C2 |
METHOD OF INSTALLING BLADES ON PERIPHERY OF DISC OF TURBINE ENGINE AND TOOL FOR MOUNTING BLADE | 2015 |
|
RU2701925C2 |
METHOD OF REPAIRING GAS TURBINE ENGINE BLADE LABYRINTH SEAL KNIFE EDGES | 2007 |
|
RU2354523C1 |
REPAIRMENT OF END PART OF TURBINE COMPONENT, USING COMPOSITE PRE-SINTERED MOLD OF BORON-DOPED BASE | 2019 |
|
RU2785029C1 |
PROTECTIVE MASK TO PROCESS TURBOMACHINE VANE SURFACES | 2004 |
|
RU2369443C2 |
HARD-FACING OF POWER PLANT BLADES | 2013 |
|
RU2545877C2 |
METHOD FOR RECONSTRUCTION OF PLATFORMS FOR COMPRESSOR BLADES IN GAS TURBINE ENGINES (GTE) | 2016 |
|
RU2627558C1 |
Authors
Dates
2012-07-20—Published
2007-12-13—Filed