FIELD: machine building.
SUBSTANCE: rotor blade having a platform, a body part, connected to the platform, and a surface finished at the end part and having an aerodynamic shape in the cross section. The thickness of the rotor blade varies depending on its height according to three different linear functions: Tmax=-0.8646*h+1.1087, Tmax=-1.0209*h+1.2058, Tmax=-0.7618*h+0.9985, where h is the percentage of the blade height. The blade thickness can be put in compliance with the operation characteristics of the turbine unit.
EFFECT: characteristics optimisation.
10 cl, 1 tbl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| RADIAL DIFFUSER BLADE FOR CENTRIFUGAL COMPRESSORS | 2010 |
|
RU2581686C2 |
| TURBINE BLADE AND TURBINE WHEEL WITH SAID BLADES | 2010 |
|
RU2518767C2 |
| COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PRESET PROFILE PART, COMPRESSOR BLADE, WHICH HAS AERODYNAMIC PART WITH THE SIDE OF LOW-PRESSURE PRESET PROFILE AND COMPRESSOR | 2013 |
|
RU2614423C2 |
| PLATFORM COOLING DEVICE INTENDED FOR TURBINE ROTARY BLADE AND ITS MANUFACTURING METHOD | 2012 |
|
RU2605791C2 |
| TURBOMACHINE ROTOR BLADE, DISC WITH BLADES, ROTOR AND TURBOMACHINE | 2016 |
|
RU2727823C2 |
| LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
| COMPRESSOR BLADE OF AXIAL TURBOMACHINE WITH BRANCHES AT BASE AND ON BLADE TOP AND TURBOMACHINE COMPRISING SAID BLADE | 2015 |
|
RU2693548C2 |
| BLADE WITH NARROW MIDDLE PART | 2000 |
|
RU2219377C2 |
| DOUBLE ALLOY BLADE | 2016 |
|
RU2680169C1 |
| TURBOMACHINE OVERROTOR DEVICE | 2001 |
|
RU2199680C2 |
