FIELD: mechanical engineering; turbines.
SUBSTANCE: proposed device for locking blades in peripheral groove of turbine wheel disk is made for its driving into mounting port and is provided with lock member arranged in aperture dividing two roots of blades. Blades are provided with hammer-type roots made in groove through mounting port and held with possibility of fitting in groove through engagement with its side walls. Lock member is made for lifting under action of radial lifting screw into lock seat made in side walls of groove. Head of lifting screw thrusts against bottom of groove. Radial clearance is provided between bottom of grove and lower part of blade root. Head of screw is held radially outside by two adjacent roots of blades.
EFFECT: provision of locking device which can be set in confined round space.
7 cl, 12 dwg
Title | Year | Author | Number |
---|---|---|---|
SHIM FOR TURBINE BLADE, TURBINE ROTOR STRUCTURE AND TURBINE | 2008 |
|
RU2472945C2 |
ROTOR DISK BALANCING MECHANISM, DISK EQUIPPED WITH SUCH MECHANISM AND ROTOR INCORPORATING SAID MECHANISM | 2005 |
|
RU2362028C2 |
GAS TURBINE RING FASTENING DEVICE, ASSEMBLY COMPRISING TURBINE RING AND DEVICE FOR ITS FASTENING, TURBINE AND TURBOMOTOR | 2010 |
|
RU2538988C2 |
TURBINE IMPELLER AND GAS-TURBINE ENGINE | 2010 |
|
RU2550226C2 |
DEVICE FOR LOCKING BLADES ON DISK BY HAMMER-LIKE FASTENERS | 2001 |
|
RU2222700C2 |
DEVICE TO CONTROL POSITION OF BLADES WITH ADJUSTABLE ANGLE OF SETTING | 2001 |
|
RU2272913C2 |
TURBINE UNIT ROTOR AND TURBINE UNIT WITH SAID ROTOR | 2007 |
|
RU2446287C2 |
TURBOJET ENGINE BLOWER ROTOR, BLOWER AND AIRCRAFT TURBOJET ENGINE | 2006 |
|
RU2396470C2 |
GAS-TURBINE ENGINE FAN | 2008 |
|
RU2459120C2 |
TURBINE RUNNER AND TURBOMACHINE CONTAINING SUCH RUNNER | 2009 |
|
RU2511915C2 |
Authors
Dates
2004-10-27—Published
2002-11-21—Filed