FIELD: machine building.
SUBSTANCE: blades are installed in radial grooves of a wheel hub with tension. The blade ends bent at the angle of 90° are inserted in the longitudinal grooves of the pins which are installed with tension in the holes adjoining the hub grooves. The holes for the installation of pins are set at the same distance from the wheel centre.
EFFECT: invention provides for fast replacement of worn wheel blades, allows for the usage of simply manufactured parts.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOMACHINE WORKING WHEEL | 1990 |
|
RU2018037C1 |
GAS-TURBINE ENGINE BLADE STRUT INSERT AND ROTOR DISK UNIT | 2001 |
|
RU2281403C2 |
GAS-TURBINE ENGINE CONTAINING FAN AND COMPRESSOR | 2016 |
|
RU2625078C1 |
ROTOR DISK OF GAS-TURBINE ENGINE (VERSIONS) | 2001 |
|
RU2281420C2 |
PROPELLER-TYPE HYDRAULIC TURBINE WHEEL | 1996 |
|
RU2127827C1 |
FAN, IN PARTICULAR, FOR TURBINE ENGINE | 2014 |
|
RU2677769C1 |
FAN FOR TURBOMACHINE | 2014 |
|
RU2683343C1 |
METHOD OF COOLING AND REGULATING RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2732653C1 |
CONTROL METHOD OF RADIAL CLEARANCES OF TURBINE OF DOUBLE-FLOW GAS TURBINE ENGINE AND DEVICE FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2738523C1 |
CENTRIFUGAL COMPRESSOR | 2007 |
|
RU2345252C1 |
Authors
Dates
2014-10-10—Published
2013-02-28—Filed